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	<id>https://www.astro-init.top/api.php?action=feedcontributions&amp;feedformat=atom&amp;user=Quan787</id>
	<title>astro-init - 用户贡献 [zh-cn]</title>
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	<updated>2026-05-05T10:49:16Z</updated>
	<subtitle>用户贡献</subtitle>
	<generator>MediaWiki 1.32.2</generator>
	<entry>
		<id>https://www.astro-init.top/index.php?title=%E6%A8%A1%E6%9D%BF:%E9%A6%96%E9%A1%B5%E5%BD%A9%E8%9B%8B&amp;diff=2847</id>
		<title>模板:首页彩蛋</title>
		<link rel="alternate" type="text/html" href="https://www.astro-init.top/index.php?title=%E6%A8%A1%E6%9D%BF:%E9%A6%96%E9%A1%B5%E5%BD%A9%E8%9B%8B&amp;diff=2847"/>
		<updated>2025-10-16T09:08:10Z</updated>

		<summary type="html">&lt;p&gt;Quan787：&lt;/p&gt;
&lt;hr /&gt;
&lt;div&gt; 如何区分AI与BR？&lt;br /&gt;
 AI：20.6万&lt;br /&gt;
 BR：2！0！6！2！6！5！&lt;br /&gt;
 [[模板:首页彩蛋|查看更多&amp;gt;&amp;gt;]] | [[模板讨论:首页彩蛋|投稿&amp;gt;&amp;gt;]]&lt;br /&gt;
&lt;br /&gt;
&amp;lt;noinclude&amp;gt;&lt;br /&gt;
== 往期彩蛋 ==&lt;br /&gt;
&lt;br /&gt;
 闲着无聊，不如[[未名题集-第一期|做题]]。&lt;br /&gt;
&lt;br /&gt;
 让我康康是谁还没有学习！&lt;br /&gt;
&lt;br /&gt;
 新年快乐，龙年大吉～&lt;br /&gt;
 是谁过年了还在astro-init学习，原来是聪慧的你。&lt;br /&gt;
&lt;br /&gt;
 天文学中只有两种颜色，红和蓝；也只有两种非金属元素，氢和氦，剩下的都是金属。&lt;br /&gt;
&lt;br /&gt;
&lt;br /&gt;
&lt;br /&gt;
 一位同学使用手机拍下了如下照片。图片上的两个天体确实是太阳和月亮。但很显然，根据常识，太阳和月亮不可能存在这样的位置关系。请问这个同学采用了什么光学把戏拍下了这张照片？&lt;br /&gt;
 [[文件:太阳和月亮.png|无框]]&lt;br /&gt;
&lt;br /&gt;
&lt;br /&gt;
&lt;br /&gt;
&lt;br /&gt;
 一群外星天文学家居住在一颗恒星附近的行星上。这颗恒星在地球上看黄纬是5度。&lt;br /&gt;
 1）这群天文学家能否通过观测木星凌太阳的方式发现太阳系？&lt;br /&gt;
 2）如果不能，在什么情况下就可以发现了？&lt;br /&gt;
&lt;br /&gt;
&lt;br /&gt;
 aw太像话了&lt;br /&gt;
 不存在的&lt;br /&gt;
 今年aw我女装&lt;br /&gt;
 你们可以截图了&lt;br /&gt;
&lt;br /&gt;
&lt;br /&gt;
 国家天文台门口有一座正确放置的日晷。一个同学路过时，读出日晷上的时间是下午16时35分。一个月后，这个同学在与上次一样的'''地方恒星时'''去读数，读到的时间居然与上一次完全一样是16时35分。请解释这一现象。&lt;br /&gt;
&amp;lt;/noinclude&amp;gt;&lt;/div&gt;</summary>
		<author><name>Quan787</name></author>
		
	</entry>
	<entry>
		<id>https://www.astro-init.top/index.php?title=%E6%A8%A1%E6%9D%BF:%E6%9C%AC%E5%91%A8%E5%85%B3%E6%B3%A8&amp;diff=2839</id>
		<title>模板:本周关注</title>
		<link rel="alternate" type="text/html" href="https://www.astro-init.top/index.php?title=%E6%A8%A1%E6%9D%BF:%E6%9C%AC%E5%91%A8%E5%85%B3%E6%B3%A8&amp;diff=2839"/>
		<updated>2025-07-23T06:03:13Z</updated>

		<summary type="html">&lt;p&gt;Quan787：&lt;/p&gt;
&lt;hr /&gt;
&lt;div&gt;&amp;lt;table class=&amp;quot;wikitable&amp;quot; width=&amp;quot;100%&amp;quot;&amp;gt;&lt;br /&gt;
&amp;lt;tr&amp;gt;&amp;lt;td&amp;gt;&lt;br /&gt;
&amp;lt;big&amp;gt;[[CNAO2025]]&lt;br /&gt;
&lt;br /&gt;
2024-2025学年全国中学生天文知识竞赛决赛于5月12月至5月16日在汕头举行。&amp;lt;/big&amp;gt;&lt;br /&gt;
&lt;br /&gt;
题目已经更新&amp;gt;&amp;gt;[[CNAO2025]]&lt;br /&gt;
&lt;br /&gt;
----&lt;br /&gt;
&lt;br /&gt;
&amp;lt;big&amp;gt;[[IOAA2024]]&lt;br /&gt;
&lt;br /&gt;
第17届国际天文与天体物理奥林匹克竞赛将于2024年8月17日至26日在巴西举行&amp;lt;/big&amp;gt;&lt;br /&gt;
&lt;br /&gt;
[http://www.bjp.org.cn/qgzxstwzsjs/asry/4028c1367d4415d3017d46802f65001f.shtml 北京天文馆带队参加国际天文与天体物理奥林匹克竞赛获佳绩]&lt;br /&gt;
----&lt;br /&gt;
&lt;br /&gt;
IOAA2021题目正在更新，敬请期待。&lt;br /&gt;
&amp;lt;/td&amp;gt;&amp;lt;/tr&amp;gt;&lt;br /&gt;
&amp;lt;/table&amp;gt;&lt;/div&gt;</summary>
		<author><name>Quan787</name></author>
		
	</entry>
	<entry>
		<id>https://www.astro-init.top/index.php?title=%E6%A8%A1%E6%9D%BF:%E8%B5%9B%E4%BA%8B%E5%88%97%E8%A1%A8&amp;diff=2838</id>
		<title>模板:赛事列表</title>
		<link rel="alternate" type="text/html" href="https://www.astro-init.top/index.php?title=%E6%A8%A1%E6%9D%BF:%E8%B5%9B%E4%BA%8B%E5%88%97%E8%A1%A8&amp;diff=2838"/>
		<updated>2025-07-23T05:59:36Z</updated>

		<summary type="html">&lt;p&gt;Quan787：&lt;/p&gt;
&lt;hr /&gt;
&lt;div&gt;&amp;lt;table class=&amp;quot;wikitable&amp;quot; width=&amp;quot;100%&amp;quot; border=&amp;quot;1&amp;quot;&amp;gt;&lt;br /&gt;
&amp;lt;tr&amp;gt;&lt;br /&gt;
&amp;lt;th width=&amp;quot;50%&amp;quot; bgcolor=&amp;quot;DeepSkyBlue &amp;quot;&amp;gt;[[CNAO]]&amp;lt;/th&amp;gt;&lt;br /&gt;
&amp;lt;th width=&amp;quot;50%&amp;quot; bgcolor=&amp;quot;DeepSkyBlue &amp;quot;&amp;gt;[[IOAA]]&amp;lt;/th&amp;gt;&lt;br /&gt;
&amp;lt;/tr&amp;gt;&lt;br /&gt;
&amp;lt;tr&amp;gt;&lt;br /&gt;
&amp;lt;td&amp;gt;&lt;br /&gt;
*[[CNAO2025]]&lt;br /&gt;
*[[CNAO2024]]&lt;br /&gt;
*[[CNAO2023]]&lt;br /&gt;
*[[CNAO2022]]&lt;br /&gt;
&amp;lt;/td&amp;gt;&lt;br /&gt;
&amp;lt;td&amp;gt;&lt;br /&gt;
*[[IOAA2024]]&lt;br /&gt;
*[[IOAA2021]]&lt;br /&gt;
*[[GeCAA2020]]&lt;br /&gt;
*[[IOAA2019]]&lt;br /&gt;
&amp;lt;/td&amp;gt;&lt;br /&gt;
&amp;lt;/tr&amp;gt;&lt;br /&gt;
&amp;lt;tr&amp;gt;&lt;br /&gt;
&amp;lt;th width=&amp;quot;50%&amp;quot; bgcolor=&amp;quot;DeepSkyBlue &amp;quot;&amp;gt;[[IAO]]&amp;lt;/th&amp;gt;&lt;br /&gt;
&amp;lt;th width=&amp;quot;50%&amp;quot; bgcolor=&amp;quot;DeepSkyBlue &amp;quot;&amp;gt;[[APAO]]&amp;lt;/th&amp;gt;&lt;br /&gt;
&amp;lt;/tr&amp;gt;&lt;br /&gt;
&amp;lt;tr&amp;gt;&lt;br /&gt;
&amp;lt;td&amp;gt;&lt;br /&gt;
*[[IRAO2021]]&lt;br /&gt;
*[[IAO2019]]&lt;br /&gt;
*[[IAO2018]]&lt;br /&gt;
*[[IAO2017]]&lt;br /&gt;
&amp;lt;/td&amp;gt;&lt;br /&gt;
&amp;lt;td&amp;gt;&lt;br /&gt;
*[[APAO2018]]&lt;br /&gt;
*[[APAO2017]]&lt;br /&gt;
*[[APAO2016]]&lt;br /&gt;
&amp;lt;/td&amp;gt;&lt;br /&gt;
&amp;lt;/tr&amp;gt;&lt;br /&gt;
&amp;lt;/table&amp;gt;&lt;/div&gt;</summary>
		<author><name>Quan787</name></author>
		
	</entry>
	<entry>
		<id>https://www.astro-init.top/index.php?title=2023-2024%E5%AD%A6%E5%B9%B4CNAO%E5%86%B3%E8%B5%9B%E9%80%89%E6%8B%A9%E9%A2%98&amp;diff=2771</id>
		<title>2023-2024学年CNAO决赛选择题</title>
		<link rel="alternate" type="text/html" href="https://www.astro-init.top/index.php?title=2023-2024%E5%AD%A6%E5%B9%B4CNAO%E5%86%B3%E8%B5%9B%E9%80%89%E6%8B%A9%E9%A2%98&amp;diff=2771"/>
		<updated>2025-04-12T13:37:42Z</updated>

		<summary type="html">&lt;p&gt;Quan787：第8题“平方根”&lt;/p&gt;
&lt;hr /&gt;
&lt;div&gt;==题目==&lt;br /&gt;
1.（仅低年组）目前天文学研究的热点集中在以下哪个分支学科（　　　）？&lt;br /&gt;
&lt;br /&gt;
（A）天体测量学　　（B）天体力学　　（C）天体物理学　　（D）天体化学&lt;br /&gt;
&lt;br /&gt;
2.（仅低年组）以下四座城市的地方时哪个更接近“北京时间”（　　　）？&lt;br /&gt;
&lt;br /&gt;
（A）西安　  　　　（B）北京　　　　（C）上海　　　　（D）杭州&lt;br /&gt;
&lt;br /&gt;
3. 以下那个天体距离我们最近（　　　）？[[文件:CNAO2024决赛图1.jpg|缩略图|图1]]（A）M20　　　　（B）M31　　　（C）M81　　　（D）M101&lt;br /&gt;
&lt;br /&gt;
4. 全天看上去最亮的恒星位于（　　　）。&lt;br /&gt;
&lt;br /&gt;
（A）船底座　　　　（B）天琴座　　　（C）小熊座　　　（D）大犬座&lt;br /&gt;
&lt;br /&gt;
5. 图1箭头指的是哪种太阳活动（　　　）？&lt;br /&gt;
&lt;br /&gt;
（A）黑子　　　　（B）暗条　　　　（C）针状体　　　　（D）耀斑&lt;br /&gt;
&lt;br /&gt;
6. 夏至的时候，如果你在北京（166°E，40°N），可以看到太阳于（      ）方升起。&lt;br /&gt;
&lt;br /&gt;
（A）东北　　　　（B）正东　　　　（C）东南　　　　（D）西北&lt;br /&gt;
&lt;br /&gt;
7. 以下我国古代天文学家按年代先后顺序排序正确的是（      ）。&lt;br /&gt;
&lt;br /&gt;
①祖冲之 ②郭守敬 ③张衡 ④徐光启 ⑤沈括&lt;br /&gt;
&lt;br /&gt;
（A）①②④③⑤　　　  （B）③①⑤②④　　　&lt;br /&gt;
&lt;br /&gt;
（C）③①②⑤④　　　　（D）③⑤①②④&lt;br /&gt;
&lt;br /&gt;
8. 当我们观测遥远的恒星时，如果中间有其它恒星或行星（透镜天体）穿过，由于引力的光汇聚作用，观测的背景恒星亮度增加，即微引力透镜效应。利用微引力透镜寻找系外行星，有一个非常重要的时标参数τ，可以大致描述信号的长短，它与透镜天体质量的平方根成正比。一般来说，恒星质量的透镜天体引发的微引力透镜时标一般在一个月左右，那么木星质量的透镜天体导致的事件时标为（      ）左右。&lt;br /&gt;
&lt;br /&gt;
（A）1年　　　（B）1月　　　（C）1天　　　（D）1小时&lt;br /&gt;
&lt;br /&gt;
9. 若想从太阳系外某颗黄纬为0的恒星处，观察到因为地球带来的视向速度变化，则光谱仪的分辨率应道至少约为（　　　）。&lt;br /&gt;
&lt;br /&gt;
（A）3×10&amp;lt;sup&amp;gt;5&amp;lt;/sup&amp;gt;　　　（B）3×10&amp;lt;sup&amp;gt;7&amp;lt;/sup&amp;gt;　　　（C）3×10&amp;lt;sup&amp;gt;9&amp;lt;/sup&amp;gt;　　　（D）3×10&amp;lt;sup&amp;gt;11&amp;lt;/sup&amp;gt;&lt;br /&gt;
&lt;br /&gt;
10. 今年5月3日，（　　　）由长征五号火箭从海南文昌发射中心成功发射。&lt;br /&gt;
&lt;br /&gt;
（A）嫦娥六号　　　（B）神舟十八号　　　（C）天问二号　　　（D）中国巡天空间望远镜（CSST）&lt;br /&gt;
&lt;br /&gt;
11.（仅高年组）我们认为现在地球围绕太阳的轨道半径为1au的圆轨道。如果现在地球的轨道速度突然变为原先的1.2倍，则新轨道的偏心率为（　　　）。&lt;br /&gt;
&lt;br /&gt;
（A）0.2　　　（B）0.4　　　（C）0.6　　　（D）0.8&lt;br /&gt;
&lt;br /&gt;
12.（仅高年组）在宇宙学中，对同一个天体的距离有不同的定义方式。一般常用的有共动距离、光度距离、角直径距离。如果观测到一个红移z=5的天体，这三个数值从小到大排序是（　　　）。&lt;br /&gt;
&lt;br /&gt;
（A）角直径距离、共动距离、光度距离　　&lt;br /&gt;
&lt;br /&gt;
（B）共动距离、光度距离、角直径距离　　&lt;br /&gt;
&lt;br /&gt;
（C）光度距离、角直径距离、共动距离　　&lt;br /&gt;
&lt;br /&gt;
（D）差距不大，实际计算时可忽略&lt;br /&gt;
&lt;br /&gt;
==答案==&lt;br /&gt;
CDADB ABCCA BA&lt;br /&gt;
&lt;br /&gt;
==计算题解答==&lt;br /&gt;
&lt;br /&gt;
[[2024CNAO决赛选择题第9题解答]]&lt;br /&gt;
&lt;br /&gt;
&amp;lt;br /&amp;gt;&lt;/div&gt;</summary>
		<author><name>Quan787</name></author>
		
	</entry>
	<entry>
		<id>https://www.astro-init.top/index.php?title=2024%E5%B9%B4IOAA%E7%90%86%E8%AE%BA%E7%AC%AC10%E9%A2%98-%E6%9C%80%E5%A4%A7%E6%97%A5%E9%A3%9F&amp;diff=2750</id>
		<title>2024年IOAA理论第10题-最大日食</title>
		<link rel="alternate" type="text/html" href="https://www.astro-init.top/index.php?title=2024%E5%B9%B4IOAA%E7%90%86%E8%AE%BA%E7%AC%AC10%E9%A2%98-%E6%9C%80%E5%A4%A7%E6%97%A5%E9%A3%9F&amp;diff=2750"/>
		<updated>2025-03-08T15:08:35Z</updated>

		<summary type="html">&lt;p&gt;Quan787：&lt;/p&gt;
&lt;hr /&gt;
&lt;div&gt;{{由ai生成}}&lt;br /&gt;
&lt;br /&gt;
==英文题目==&lt;br /&gt;
&lt;br /&gt;
'''T10. Greatest Eclipse (75 points)'''&lt;br /&gt;
&lt;br /&gt;
The greatest eclipse is defined as the instant when the axis of the Moon's shadow cone gets closest to the centre of the Earth in a solar eclipse. This problem explores the geometry of this phenomenon, using the solar eclipse of 29\(^\text{th}\) May 1919 as an example, as it has great historical significance for being the first time astronomers were able to observationally verify general relativity. One of the scientific expeditions to observe this eclipse took place in the Brazilian city of Sobral.&lt;br /&gt;
&lt;br /&gt;
The two following tables show the Cartesian and spherical coordinates of the Sun and the Moon at the time of the greatest eclipse. The system used for these coordinates is right-handed and has the origin at the centre of the Earth, the positive \(x\)-axis pointing towards the Greenwich meridian, and the positive \(z\)-axis pointing towards the North Pole. For the rest of this problem, this will be referred to as System I.&lt;br /&gt;
&lt;br /&gt;
'''Spherical Coordinates:'''&lt;br /&gt;
&lt;br /&gt;
{| class=&amp;quot;wikitable&amp;quot;&lt;br /&gt;
|-&lt;br /&gt;
! !! Centre of the Sun !! Centre of the Moon&lt;br /&gt;
|-&lt;br /&gt;
| Radial Distance (\(r\)) || \(1.516 \times 10^{11}\) m || \(3.589 \times 10^8\) m&lt;br /&gt;
|-&lt;br /&gt;
| Polar Angle (\(\theta\)) || \(68^{\circ}29'44.1''\) || \(68^{\circ}47'41.6''\)&lt;br /&gt;
|-&lt;br /&gt;
| Azimuthal Angle (\(\varphi\)) || \(-1^h11^{m}28.2^s\) || \(-1^h11^{m}22.9^s\)&lt;br /&gt;
|}&lt;br /&gt;
&lt;br /&gt;
'''Cartesian Coordinates:'''&lt;br /&gt;
&lt;br /&gt;
{| class=&amp;quot;wikitable&amp;quot;&lt;br /&gt;
|-&lt;br /&gt;
! !! Centre of the Sun !! Centre of the Moon&lt;br /&gt;
|-&lt;br /&gt;
| \(x\) || \(1.342 \times 10^{11}\) m || \(3.185 \times 10^8\) m&lt;br /&gt;
|-&lt;br /&gt;
| \(y\) || \(-4.327 \times 10^{10}\) m || \(-1.025 \times 10^8\) m&lt;br /&gt;
|-&lt;br /&gt;
| \(z\) || \(5.557 \times 10^{10}\) m || \(1.298 \times 10^8\) m&lt;br /&gt;
|}&lt;br /&gt;
&lt;br /&gt;
For this problem, assume that the Earth is a perfect sphere.&lt;br /&gt;
&lt;br /&gt;
'''Note:''' The spherical coordinates of a point \(P\) are defined as follows:&lt;br /&gt;
&lt;br /&gt;
- Radial distance (\(r\)): distance between the origin (\(O\)) and \(P\) (range: \(r \geq 0\)).&lt;br /&gt;
- Polar angle (\(\theta\)): angle between the positive \(z\)-axis and the line segment \(OP\) (range: \(0^{\circ} \leq \theta \leq 180^{\circ}\)).&lt;br /&gt;
- Azimuthal angle (\(\varphi\)): angle between the positive \(x\)-axis and the projection of the line segment \(OP\) onto the \(xy\)-plane (range: \(-12^h \leq \varphi &amp;lt; 12^h\)).&lt;br /&gt;
&lt;br /&gt;
=== Part I: Geographic Coordinates (25 points) ===&lt;br /&gt;
&lt;br /&gt;
(a) (3 points) Determine the declination of the Sun and the Moon during the greatest eclipse for a geocentric observer.&lt;br /&gt;
&lt;br /&gt;
(b) (3 points) Determine the right ascension of the Sun and the Moon at the time of the greatest eclipse for a geocentric observer. The local sidereal time at Greenwich at that same moment was \(5^h32^m35.5^s\).&lt;br /&gt;
&lt;br /&gt;
(c) (4 points) Find a unit vector that indicates the direction of the axis of the Moon’s shadow cone. This vector should point from the Moon to the vicinity of the centre of the Earth.&lt;br /&gt;
&lt;br /&gt;
(d) (15 points) Determine the latitude and the longitude of the point where the axis of the Moon's shadow cone crosses the surface of the Earth during the greatest eclipse.&lt;br /&gt;
&lt;br /&gt;
=== Part II: Duration of the Totality (50 points) ===&lt;br /&gt;
&lt;br /&gt;
Precisely determining the duration of totality of a solar eclipse involves complex calculations that would be beyond the scope of this problem. However, it is possible to obtain a reasonable approximation for this value using the two following assumptions:&lt;br /&gt;
&lt;br /&gt;
- The size of the umbra on the surface of the Earth remains roughly constant throughout totality at a given location.&lt;br /&gt;
- The velocity of the umbra on the surface of the Earth remains roughly constant throughout totality at a given location.&lt;br /&gt;
&lt;br /&gt;
(e) (10 points) Estimate the radius of the umbra during the greatest eclipse. In order to simplify the calculations, assume that the umbra is small enough that it can be considered approximately flat and that the axis of the Moon's shadow cone is extremely close to the centre of the Earth during the greatest eclipse.&lt;br /&gt;
&lt;br /&gt;
(f) (3 points) Calculate the velocity of the Earth's rotation at the latitude of the centre of the umbra.&lt;br /&gt;
&lt;br /&gt;
(g) (4 points) Determine the orbital velocity of the Moon at the instant of the greatest eclipse. Neglect the changes in the semi-major axis of the Moon’s orbit.&lt;br /&gt;
&lt;br /&gt;
For the remaining items of this problem, assume that the tangential velocity of the Moon is roughly the same as the orbital velocity and neglect its radial component.&lt;br /&gt;
&lt;br /&gt;
(h) (14 points) Using System II, determine the velocity vector of the Moon during the greatest eclipse. Note that the intersection between the Celestial Equator and the lunar orbit that is closer to the position of the eclipse has a right ascension of \(23^{h}07^{m}59.2^s\).&lt;br /&gt;
&lt;br /&gt;
(i) (10 points) Write the velocity vector of the Moon in System III. Note that in System I, the azimuthal angle difference between the positions of the origins OII and OIII is negligible, so you should only take into account the difference in the polar angles.&lt;br /&gt;
&lt;br /&gt;
(j) (6 points) Calculate the speed of the centre of the umbra along the surface of the Earth at the instant of the greatest eclipse.&lt;br /&gt;
&lt;br /&gt;
(k) (3 points) Estimate the duration of the totality of the eclipse at the location with the coordinates found in part (d).&lt;br /&gt;
&lt;br /&gt;
==中文翻译==&lt;br /&gt;
&lt;br /&gt;
'''T10. 最大食分（75分）'''&lt;br /&gt;
&lt;br /&gt;
最大食分定义为月球本影锥轴最接近地球中心的时刻。本题将探讨这一现象的几何原理，并以1919年5月29日日全食为例（该次日食具有重大历史意义，是天文学家首次通过观测验证广义相对论的契机）。其中一支科学考察队就是在巴西索布拉尔市进行观测的。&lt;br /&gt;
&lt;br /&gt;
以下两个表格分别给出了最大食分时刻太阳和月球的球面坐标与笛卡尔坐标。该坐标系为右手坐标系，原点在地球中心，x轴正方向指向格林尼治子午线，z轴正方向指向北极点。在下文中称为&amp;quot;系统I&amp;quot;。&lt;br /&gt;
&lt;br /&gt;
'''球面坐标：'''&lt;br /&gt;
&lt;br /&gt;
{| class=&amp;quot;wikitable&amp;quot;&lt;br /&gt;
|-&lt;br /&gt;
! !! 太阳中心 !! 月球中心&lt;br /&gt;
|-&lt;br /&gt;
| 径向距离 (\(r\)) || \(1.516 \times 10^{11}\) m || \(3.589 \times 10^8\) m&lt;br /&gt;
|-&lt;br /&gt;
| 极角 (\(\theta\)) || \(68^{\circ}29'44.1''\) || \(68^{\circ}47'41.6''\)&lt;br /&gt;
|-&lt;br /&gt;
| 方位角 (\(\varphi\)) || \(-1^h11^{m}28.2^s\) || \(-1^h11^{m}22.9^s\)&lt;br /&gt;
|}&lt;br /&gt;
&lt;br /&gt;
'''笛卡尔坐标：'''&lt;br /&gt;
&lt;br /&gt;
{| class=&amp;quot;wikitable&amp;quot;&lt;br /&gt;
|-&lt;br /&gt;
! !! 太阳中心 !! 月球中心&lt;br /&gt;
|-&lt;br /&gt;
| \(x\) || \(1.342 \times 10^{11}\) m || \(3.185 \times 10^8\) m&lt;br /&gt;
|-&lt;br /&gt;
| \(y\) || \(-4.327 \times 10^{10}\) m || \(-1.025 \times 10^8\) m&lt;br /&gt;
|-&lt;br /&gt;
| \(z\) || \(5.557 \times 10^{10}\) m || \(1.298 \times 10^8\) m&lt;br /&gt;
|}&lt;br /&gt;
&lt;br /&gt;
'''注意：'''点\(P\)的球面坐标定义如下：&lt;br /&gt;
&lt;br /&gt;
- 径向距离 (\(r\))：原点\(O\)到\(P\)的距离（范围：\(r \geq 0\)）&lt;br /&gt;
&lt;br /&gt;
- 极角 (\(\theta\))：z轴正方向与线段\(OP\)的夹角（范围：\(0^{\circ} \leq \theta \leq 180^{\circ}\)）&lt;br /&gt;
&lt;br /&gt;
- 方位角 (\(\varphi\))：x轴正方向与线段\(OP\)在xy平面投影的夹角（范围：\(-12^h \leq \varphi &amp;lt; 12^h\)）&lt;br /&gt;
&lt;br /&gt;
=== 第一部分：地理坐标（25分） ===&lt;br /&gt;
&lt;br /&gt;
(a)（3分）确定地心观测者所见的最大食分时刻太阳和月球的赤纬。&lt;br /&gt;
&lt;br /&gt;
(b)（3分）确定地心观测者所见的最大食分时刻太阳和月球的赤经。此时格林尼治的本地恒星时为\(5^h32^m35.5^s\)。&lt;br /&gt;
&lt;br /&gt;
(c)（4分）求表示月球本影锥轴方向的单位向量。该向量应从月球指向地球中心附近。&lt;br /&gt;
&lt;br /&gt;
(d)（15分）确定月球本影锥轴在最大食分时刻与地球表面的交点经纬度。&lt;br /&gt;
&lt;br /&gt;
=== 第二部分：全食持续时间（50分） ===&lt;br /&gt;
&lt;br /&gt;
精确计算日全食持续时间涉及复杂运算，超出本题范围。但通过以下两个假设可获得合理近似值：&lt;br /&gt;
&lt;br /&gt;
- 在特定位置，地球表面本影尺寸在全食期间大致保持不变&lt;br /&gt;
&lt;br /&gt;
- 在特定位置，地球表面本影移动速度在全食期间大致保持不变&lt;br /&gt;
&lt;br /&gt;
(e)（10分）估算最大食分时刻本影半径。为简化计算，可假设本影足够小可视为平面，且此时月球本影锥轴极度接近地球中心。&lt;br /&gt;
&lt;br /&gt;
(f)（3分）计算本影中心所在纬度处的地球自转线速度。&lt;br /&gt;
&lt;br /&gt;
(g)（4分）确定最大食分时刻月球的轨道速度。忽略月球轨道半长轴的变化。&lt;br /&gt;
&lt;br /&gt;
以下问题中，假设月球的切向速度大致等于轨道速度，并忽略其径向分量。&lt;br /&gt;
&lt;br /&gt;
(h)（14分）使用系统II确定月球在最大食分时刻的速度向量。已知月球轨道与天赤道交点中较接近食分位置的那个点赤经为\(23^h07^m59.2^s\)。&lt;br /&gt;
&lt;br /&gt;
(i)（10分）写出系统III中月球的速度向量。注意在系统I中，原点OII与OIII的方位角差异可忽略，只需考虑极角差异。&lt;br /&gt;
&lt;br /&gt;
(j)（6分）计算最大食分时刻本影中心沿地球表面的移动速率。&lt;br /&gt;
&lt;br /&gt;
(k)（3分）估算(d)中坐标位置的全食持续时间。&lt;br /&gt;
&lt;br /&gt;
&lt;br /&gt;
==官方解答==&lt;br /&gt;
&lt;br /&gt;
=== 第一部分：地理坐标解答 ===&lt;br /&gt;
&lt;br /&gt;
(a) 赤纬计算：&lt;br /&gt;
&lt;br /&gt;
$$ \delta = 90^\circ - \theta $$&lt;br /&gt;
&lt;br /&gt;
太阳赤纬：&lt;br /&gt;
&lt;br /&gt;
$$ \delta_\odot = 90^\circ - 68^\circ29'44.1'' = 21^\circ30'15.9'' $$&lt;br /&gt;
&lt;br /&gt;
月球赤纬：&lt;br /&gt;
&lt;br /&gt;
$$ \delta_{\text{Moon}} = 90^\circ - 68^\circ47'41.6'' = 21^\circ12'18.4'' $$&lt;br /&gt;
&lt;br /&gt;
(b) 赤经计算：&lt;br /&gt;
&lt;br /&gt;
$$ \alpha = \varphi + \text{LST}_{\text{Greenwich}} $$&lt;br /&gt;
&lt;br /&gt;
太阳赤经：&lt;br /&gt;
&lt;br /&gt;
$$ \alpha_\odot = -1^h11^m28.2^s + 5^h32^m35.5^s = 4^h21^m7.3^s $$&lt;br /&gt;
&lt;br /&gt;
月球赤经：&lt;br /&gt;
&lt;br /&gt;
$$ \alpha_{\text{Moon}} = -1^h11^m22.9^s + 5^h32^m35.5^s = 4^h21^m12.6^s $$&lt;br /&gt;
&lt;br /&gt;
(c) 本影轴单位向量：&lt;br /&gt;
&lt;br /&gt;
$$ \vec{u} = \frac{\vec{M}_{\text{Moon}} - \vec{M}_\odot}{|\vec{M}_{\text{Moon}} - \vec{M}_\odot|} $$&lt;br /&gt;
&lt;br /&gt;
计算结果：&lt;br /&gt;
&lt;br /&gt;
$$ \vec{u} = \left\langle -0.8855, 0.2855, -0.3666 \right\rangle $$&lt;br /&gt;
&lt;br /&gt;
(d) 地表交点坐标：&lt;br /&gt;
&lt;br /&gt;
1. 建立方程：&lt;br /&gt;
&lt;br /&gt;
$$ |\vec{M}_{\text{Moon}} + k\vec{u}|^2 = R_\oplus^2 $$&lt;br /&gt;
&lt;br /&gt;
2. 解得缩放因子：&lt;br /&gt;
&lt;br /&gt;
$$ k = 3.528 \times 10^8 $$&lt;br /&gt;
&lt;br /&gt;
3. 转换球面坐标：&lt;br /&gt;
&lt;br /&gt;
$$ \theta = \arccos\left(\frac{z}{r}\right) = 85^\circ38' $$&lt;br /&gt;
&lt;br /&gt;
$$ \varphi = \arctan\left(\frac{y}{x}\right) = -16^\circ42' $$&lt;br /&gt;
&lt;br /&gt;
最终坐标：&lt;br /&gt;
&lt;br /&gt;
$$ 4^\circ22'N, 16^\circ42'W $$&lt;br /&gt;
&lt;br /&gt;
=== 第二部分：全食持续时间解答 ===&lt;br /&gt;
&lt;br /&gt;
(e) 本影半径估算：&lt;br /&gt;
&lt;br /&gt;
$$ \beta = \arccos\left(\frac{R_\odot - R_{\text{Moon}}}{d_\odot - d_{\text{Moon}}}\right) = 89.74^\circ $$&lt;br /&gt;
&lt;br /&gt;
$$ r_{\text{umbra}} = \frac{R_{\text{Moon}} - (d_{\text{Moon}} - R_\odot)\cos\beta}{\sin\beta} = 1.196 \times 10^5 \text{ m} $$&lt;br /&gt;
&lt;br /&gt;
(f) 地球自转线速度：&lt;br /&gt;
&lt;br /&gt;
$$ v_{\text{rot}} = \frac{2\pi R_\oplus \cos\phi}{T_{\text{sidereal}}} = 463.7 \text{ m/s} $$&lt;br /&gt;
&lt;br /&gt;
(g) 月球轨道速度：&lt;br /&gt;
&lt;br /&gt;
$$ v_{\text{Moon}} = \sqrt{GM_\oplus\left(\frac{2}{d_{\text{Moon}}} - \frac{1}{a_{\text{Moon}}}\right)} = 1088 \text{ m/s} $$&lt;br /&gt;
&lt;br /&gt;
(h) 系统II速度向量：&lt;br /&gt;
&lt;br /&gt;
$$ \kappa = \arctan\left(\frac{\sin\delta_{\text{Moon}}}{\tan(\alpha_{\text{Moon}} - \alpha_{\text{intersection}})}\right) = 4^\circ17' $$&lt;br /&gt;
&lt;br /&gt;
$$ \vec{v}_{\text{II}} = \begin{bmatrix} 1085\cos\kappa \\ 1085\sin\kappa \\ 0 \end{bmatrix} = \begin{bmatrix} 1085 \\ 81.25 \\ 0 \end{bmatrix} \text{ m/s} $$&lt;br /&gt;
&lt;br /&gt;
(i) 系统III速度向量：&lt;br /&gt;
&lt;br /&gt;
$$ \vec{v}_{\text{III}} = \begin{bmatrix} v_x \\ v_y\cos\Delta\theta \\ -v_y\sin\Delta\theta \end{bmatrix} = \begin{bmatrix} 1085 \\ 77.76 \\ -23.54 \end{bmatrix} \text{ m/s} $$&lt;br /&gt;
&lt;br /&gt;
(j) 本影移动速率合成：&lt;br /&gt;
&lt;br /&gt;
$$ \vec{v}_{\text{umbra}} = \sqrt{(v_x - v_{\text{rot}})^2 + v_y^2} = 626.3 \text{ m/s} $$&lt;br /&gt;
&lt;br /&gt;
(k) 全食持续时间：&lt;br /&gt;
&lt;br /&gt;
$$ \Delta t = \frac{2r_{\text{umbra}}}{v_{\text{umbra}}} = 6\text{分}21.4\text{秒} $$&lt;br /&gt;
&lt;br /&gt;
[[分类:日月食]]&lt;br /&gt;
[[分类:球面三角]]&lt;br /&gt;
[[分类:由ai生成]]&lt;/div&gt;</summary>
		<author><name>Quan787</name></author>
		
	</entry>
	<entry>
		<id>https://www.astro-init.top/index.php?title=2024%E5%B9%B4IOAA%E7%90%86%E8%AE%BA%E7%AC%AC10%E9%A2%98-%E6%9C%80%E5%A4%A7%E6%97%A5%E9%A3%9F&amp;diff=2749</id>
		<title>2024年IOAA理论第10题-最大日食</title>
		<link rel="alternate" type="text/html" href="https://www.astro-init.top/index.php?title=2024%E5%B9%B4IOAA%E7%90%86%E8%AE%BA%E7%AC%AC10%E9%A2%98-%E6%9C%80%E5%A4%A7%E6%97%A5%E9%A3%9F&amp;diff=2749"/>
		<updated>2025-03-08T15:02:05Z</updated>

		<summary type="html">&lt;p&gt;Quan787：&lt;/p&gt;
&lt;hr /&gt;
&lt;div&gt;{{由ai生成}}&lt;br /&gt;
&lt;br /&gt;
==英文题目==&lt;br /&gt;
&lt;br /&gt;
'''T10. Greatest Eclipse (75 points)'''&lt;br /&gt;
&lt;br /&gt;
The greatest eclipse is defined as the instant when the axis of the Moon's shadow cone gets closest to the centre of the Earth in a solar eclipse. This problem explores the geometry of this phenomenon, using the solar eclipse of 29\(^\text{th}\) May 1919 as an example, as it has great historical significance for being the first time astronomers were able to observationally verify general relativity. One of the scientific expeditions to observe this eclipse took place in the Brazilian city of Sobral.&lt;br /&gt;
&lt;br /&gt;
The two following tables show the Cartesian and spherical coordinates of the Sun and the Moon at the time of the greatest eclipse. The system used for these coordinates is right-handed and has the origin at the centre of the Earth, the positive \(x\)-axis pointing towards the Greenwich meridian, and the positive \(z\)-axis pointing towards the North Pole. For the rest of this problem, this will be referred to as System I.&lt;br /&gt;
&lt;br /&gt;
'''Spherical Coordinates:'''&lt;br /&gt;
&lt;br /&gt;
{| class=&amp;quot;wikitable&amp;quot;&lt;br /&gt;
|-&lt;br /&gt;
! !! Centre of the Sun !! Centre of the Moon&lt;br /&gt;
|-&lt;br /&gt;
| Radial Distance (\(r\)) || \(1.516 \times 10^{11}\) m || \(3.589 \times 10^8\) m&lt;br /&gt;
|-&lt;br /&gt;
| Polar Angle (\(\theta\)) || \(68^{\circ}29'44.1''\) || \(68^{\circ}47'41.6''\)&lt;br /&gt;
|-&lt;br /&gt;
| Azimuthal Angle (\(\varphi\)) || \(-1^h11^{m}28.2^s\) || \(-1^h11^{m}22.9^s\)&lt;br /&gt;
|}&lt;br /&gt;
&lt;br /&gt;
'''Cartesian Coordinates:'''&lt;br /&gt;
&lt;br /&gt;
{| class=&amp;quot;wikitable&amp;quot;&lt;br /&gt;
|-&lt;br /&gt;
! !! Centre of the Sun !! Centre of the Moon&lt;br /&gt;
|-&lt;br /&gt;
| \(x\) || \(1.342 \times 10^{11}\) m || \(3.185 \times 10^8\) m&lt;br /&gt;
|-&lt;br /&gt;
| \(y\) || \(-4.327 \times 10^{10}\) m || \(-1.025 \times 10^8\) m&lt;br /&gt;
|-&lt;br /&gt;
| \(z\) || \(5.557 \times 10^{10}\) m || \(1.298 \times 10^8\) m&lt;br /&gt;
|}&lt;br /&gt;
&lt;br /&gt;
For this problem, assume that the Earth is a perfect sphere.&lt;br /&gt;
&lt;br /&gt;
'''Note:''' The spherical coordinates of a point \(P\) are defined as follows:&lt;br /&gt;
&lt;br /&gt;
- Radial distance (\(r\)): distance between the origin (\(O\)) and \(P\) (range: \(r \geq 0\)).&lt;br /&gt;
- Polar angle (\(\theta\)): angle between the positive \(z\)-axis and the line segment \(OP\) (range: \(0^{\circ} \leq \theta \leq 180^{\circ}\)).&lt;br /&gt;
- Azimuthal angle (\(\varphi\)): angle between the positive \(x\)-axis and the projection of the line segment \(OP\) onto the \(xy\)-plane (range: \(-12^h \leq \varphi &amp;lt; 12^h\)).&lt;br /&gt;
&lt;br /&gt;
=== Part I: Geographic Coordinates (25 points) ===&lt;br /&gt;
&lt;br /&gt;
(a) (3 points) Determine the declination of the Sun and the Moon during the greatest eclipse for a geocentric observer.&lt;br /&gt;
&lt;br /&gt;
(b) (3 points) Determine the right ascension of the Sun and the Moon at the time of the greatest eclipse for a geocentric observer. The local sidereal time at Greenwich at that same moment was \(5^h32^m35.5^s\).&lt;br /&gt;
&lt;br /&gt;
(c) (4 points) Find a unit vector that indicates the direction of the axis of the Moon’s shadow cone. This vector should point from the Moon to the vicinity of the centre of the Earth.&lt;br /&gt;
&lt;br /&gt;
(d) (15 points) Determine the latitude and the longitude of the point where the axis of the Moon's shadow cone crosses the surface of the Earth during the greatest eclipse.&lt;br /&gt;
&lt;br /&gt;
=== Part II: Duration of the Totality (50 points) ===&lt;br /&gt;
&lt;br /&gt;
Precisely determining the duration of totality of a solar eclipse involves complex calculations that would be beyond the scope of this problem. However, it is possible to obtain a reasonable approximation for this value using the two following assumptions:&lt;br /&gt;
&lt;br /&gt;
- The size of the umbra on the surface of the Earth remains roughly constant throughout totality at a given location.&lt;br /&gt;
- The velocity of the umbra on the surface of the Earth remains roughly constant throughout totality at a given location.&lt;br /&gt;
&lt;br /&gt;
(e) (10 points) Estimate the radius of the umbra during the greatest eclipse. In order to simplify the calculations, assume that the umbra is small enough that it can be considered approximately flat and that the axis of the Moon's shadow cone is extremely close to the centre of the Earth during the greatest eclipse.&lt;br /&gt;
&lt;br /&gt;
(f) (3 points) Calculate the velocity of the Earth's rotation at the latitude of the centre of the umbra.&lt;br /&gt;
&lt;br /&gt;
(g) (4 points) Determine the orbital velocity of the Moon at the instant of the greatest eclipse. Neglect the changes in the semi-major axis of the Moon’s orbit.&lt;br /&gt;
&lt;br /&gt;
For the remaining items of this problem, assume that the tangential velocity of the Moon is roughly the same as the orbital velocity and neglect its radial component.&lt;br /&gt;
&lt;br /&gt;
(h) (14 points) Using System II, determine the velocity vector of the Moon during the greatest eclipse. Note that the intersection between the Celestial Equator and the lunar orbit that is closer to the position of the eclipse has a right ascension of \(23^{h}07^{m}59.2^s\).&lt;br /&gt;
&lt;br /&gt;
(i) (10 points) Write the velocity vector of the Moon in System III. Note that in System I, the azimuthal angle difference between the positions of the origins OII and OIII is negligible, so you should only take into account the difference in the polar angles.&lt;br /&gt;
&lt;br /&gt;
(j) (6 points) Calculate the speed of the centre of the umbra along the surface of the Earth at the instant of the greatest eclipse.&lt;br /&gt;
&lt;br /&gt;
(k) (3 points) Estimate the duration of the totality of the eclipse at the location with the coordinates found in part (d).&lt;br /&gt;
&lt;br /&gt;
==中文翻译==&lt;br /&gt;
&lt;br /&gt;
'''T10. 最大食分（75分）'''&lt;br /&gt;
&lt;br /&gt;
最大食分定义为月球本影锥轴最接近地球中心的时刻。本题将探讨这一现象的几何原理，并以1919年5月29日日全食为例（该次日食具有重大历史意义，是天文学家首次通过观测验证广义相对论的契机）。其中一支科学考察队就是在巴西索布拉尔市进行观测的。&lt;br /&gt;
&lt;br /&gt;
以下两个表格分别给出了最大食分时刻太阳和月球的球面坐标与笛卡尔坐标。该坐标系为右手坐标系，原点在地球中心，x轴正方向指向格林尼治子午线，z轴正方向指向北极点。在下文中称为&amp;quot;系统I&amp;quot;。&lt;br /&gt;
&lt;br /&gt;
'''球面坐标：'''&lt;br /&gt;
&lt;br /&gt;
{| class=&amp;quot;wikitable&amp;quot;&lt;br /&gt;
|-&lt;br /&gt;
! !! 太阳中心 !! 月球中心&lt;br /&gt;
|-&lt;br /&gt;
| 径向距离 (\(r\)) || \(1.516 \times 10^{11}\) m || \(3.589 \times 10^8\) m&lt;br /&gt;
|-&lt;br /&gt;
| 极角 (\(\theta\)) || \(68^{\circ}29'44.1''\) || \(68^{\circ}47'41.6''\)&lt;br /&gt;
|-&lt;br /&gt;
| 方位角 (\(\varphi\)) || \(-1^h11^{m}28.2^s\) || \(-1^h11^{m}22.9^s\)&lt;br /&gt;
|}&lt;br /&gt;
&lt;br /&gt;
'''笛卡尔坐标：'''&lt;br /&gt;
&lt;br /&gt;
{| class=&amp;quot;wikitable&amp;quot;&lt;br /&gt;
|-&lt;br /&gt;
! !! 太阳中心 !! 月球中心&lt;br /&gt;
|-&lt;br /&gt;
| \(x\) || \(1.342 \times 10^{11}\) m || \(3.185 \times 10^8\) m&lt;br /&gt;
|-&lt;br /&gt;
| \(y\) || \(-4.327 \times 10^{10}\) m || \(-1.025 \times 10^8\) m&lt;br /&gt;
|-&lt;br /&gt;
| \(z\) || \(5.557 \times 10^{10}\) m || \(1.298 \times 10^8\) m&lt;br /&gt;
|}&lt;br /&gt;
&lt;br /&gt;
'''注意：'''点\(P\)的球面坐标定义如下：&lt;br /&gt;
&lt;br /&gt;
- 径向距离 (\(r\))：原点\(O\)到\(P\)的距离（范围：\(r \geq 0\)）&lt;br /&gt;
&lt;br /&gt;
- 极角 (\(\theta\))：z轴正方向与线段\(OP\)的夹角（范围：\(0^{\circ} \leq \theta \leq 180^{\circ}\)）&lt;br /&gt;
&lt;br /&gt;
- 方位角 (\(\varphi\))：x轴正方向与线段\(OP\)在xy平面投影的夹角（范围：\(-12^h \leq \varphi &amp;lt; 12^h\)）&lt;br /&gt;
&lt;br /&gt;
=== 第一部分：地理坐标（25分） ===&lt;br /&gt;
&lt;br /&gt;
(a)（3分）确定地心观测者所见的最大食分时刻太阳和月球的赤纬。&lt;br /&gt;
&lt;br /&gt;
(b)（3分）确定地心观测者所见的最大食分时刻太阳和月球的赤经。此时格林尼治的本地恒星时为\(5^h32^m35.5^s\)。&lt;br /&gt;
&lt;br /&gt;
(c)（4分）求表示月球本影锥轴方向的单位向量。该向量应从月球指向地球中心附近。&lt;br /&gt;
&lt;br /&gt;
(d)（15分）确定月球本影锥轴在最大食分时刻与地球表面的交点经纬度。&lt;br /&gt;
&lt;br /&gt;
=== 第二部分：全食持续时间（50分） ===&lt;br /&gt;
&lt;br /&gt;
精确计算日全食持续时间涉及复杂运算，超出本题范围。但通过以下两个假设可获得合理近似值：&lt;br /&gt;
&lt;br /&gt;
- 在特定位置，地球表面本影尺寸在全食期间大致保持不变&lt;br /&gt;
&lt;br /&gt;
- 在特定位置，地球表面本影移动速度在全食期间大致保持不变&lt;br /&gt;
&lt;br /&gt;
(e)（10分）估算最大食分时刻本影半径。为简化计算，可假设本影足够小可视为平面，且此时月球本影锥轴极度接近地球中心。&lt;br /&gt;
&lt;br /&gt;
(f)（3分）计算本影中心所在纬度处的地球自转线速度。&lt;br /&gt;
&lt;br /&gt;
(g)（4分）确定最大食分时刻月球的轨道速度。忽略月球轨道半长轴的变化。&lt;br /&gt;
&lt;br /&gt;
以下问题中，假设月球的切向速度大致等于轨道速度，并忽略其径向分量。&lt;br /&gt;
&lt;br /&gt;
(h)（14分）使用系统II确定月球在最大食分时刻的速度向量。已知月球轨道与天赤道交点中较接近食分位置的那个点赤经为\(23^h07^m59.2^s\)。&lt;br /&gt;
&lt;br /&gt;
(i)（10分）写出系统III中月球的速度向量。注意在系统I中，原点OII与OIII的方位角差异可忽略，只需考虑极角差异。&lt;br /&gt;
&lt;br /&gt;
(j)（6分）计算最大食分时刻本影中心沿地球表面的移动速率。&lt;br /&gt;
&lt;br /&gt;
(k)（3分）估算(d)中坐标位置的全食持续时间。&lt;br /&gt;
&lt;br /&gt;
&lt;br /&gt;
==官方解答==&lt;br /&gt;
&lt;br /&gt;
=== Part I: 地理坐标 ===&lt;br /&gt;
(a) 太阳和月球的赤纬：&lt;br /&gt;
$$$\delta = 90^\circ - \theta$$$&lt;br /&gt;
$$$\delta_\odot = 21^\circ30'15.9''$$$&lt;br /&gt;
$$$\delta_{Moon} = 21^\circ12'18.4''$$$&lt;br /&gt;
&lt;br /&gt;
(b) 太阳和月球的赤经（格林尼治恒星时为$5^h32^m35.5^s$）：&lt;br /&gt;
$$$\alpha = \varphi + LST_{Greenwich}$$$&lt;br /&gt;
$$$\alpha_\odot = 4^h21^m7.3^s$$$&lt;br /&gt;
$$$\alpha_{Moon} = 4^h21^m12.6^s$$$&lt;br /&gt;
&lt;br /&gt;
(c) 月球本影轴方向单位向量：&lt;br /&gt;
$$$\vec{u} = \left\langle -0.8855, 0.2855, -0.3666 \right\rangle$$$&lt;br /&gt;
&lt;br /&gt;
(d) 本影轴与地球表面交点坐标：&lt;br /&gt;
通过方程$$|\vec{M} + k\vec{u}| = R_\oplus$$解得：&lt;br /&gt;
$$$\phi = 4^\circ22'N$$$&lt;br /&gt;
$$$\lambda = 16^\circ42'W$$$&lt;br /&gt;
&lt;br /&gt;
=== Part II: 全食持续时间 ===&lt;br /&gt;
(e) 本影半径估算：&lt;br /&gt;
$$$r_{umbra} = 1.196 \times 10^5 \, \text{m}$$$&lt;br /&gt;
&lt;br /&gt;
(f) 地球自转线速度：&lt;br /&gt;
$$$v_{rot} = 463.7 \, \text{m/s}$$$&lt;br /&gt;
&lt;br /&gt;
(g) 月球轨道速度（忽略半长轴变化）：&lt;br /&gt;
$$$v_{Moon} = 1088 \, \text{m/s}$$$&lt;br /&gt;
&lt;br /&gt;
(h) 系统II中月球速度向量：&lt;br /&gt;
$$$\mathbf{v_{II}} = \begin{bmatrix} 1085 \, \text{m/s} \\ 81.25 \, \text{m/s} \\ 0 \end{bmatrix}$$$&lt;br /&gt;
&lt;br /&gt;
(i) 系统III中月球速度向量：&lt;br /&gt;
$$$\mathbf{v_{III}} = \begin{bmatrix} 1085 \, \text{m/s} \\ 77.76 \, \text{m/s} \\ -23.54 \, \text{m/s} \end{bmatrix}$$$&lt;br /&gt;
&lt;br /&gt;
(j) 本影中心地表移动速度：&lt;br /&gt;
$$$v_{umbra} = \sqrt{621.4^2 + 77.76^2} = 626.3 \, \text{m/s}$$$&lt;br /&gt;
&lt;br /&gt;
(k) 全食持续时间：&lt;br /&gt;
$$$\Delta t = \frac{2r_{umbra}}{v_{umbra}} = 6\,\text{分钟}\,21.4\,\text{秒}$$$&lt;br /&gt;
&lt;br /&gt;
[[分类:日月食]]&lt;br /&gt;
[[分类:球面三角]]&lt;br /&gt;
[[分类:由ai生成]]&lt;/div&gt;</summary>
		<author><name>Quan787</name></author>
		
	</entry>
	<entry>
		<id>https://www.astro-init.top/index.php?title=2024%E5%B9%B4IOAA%E7%90%86%E8%AE%BA%E7%AC%AC10%E9%A2%98-%E6%9C%80%E5%A4%A7%E6%97%A5%E9%A3%9F&amp;diff=2748</id>
		<title>2024年IOAA理论第10题-最大日食</title>
		<link rel="alternate" type="text/html" href="https://www.astro-init.top/index.php?title=2024%E5%B9%B4IOAA%E7%90%86%E8%AE%BA%E7%AC%AC10%E9%A2%98-%E6%9C%80%E5%A4%A7%E6%97%A5%E9%A3%9F&amp;diff=2748"/>
		<updated>2025-03-08T13:34:40Z</updated>

		<summary type="html">&lt;p&gt;Quan787：&lt;/p&gt;
&lt;hr /&gt;
&lt;div&gt;{{由ai生成}}&lt;br /&gt;
&lt;br /&gt;
==英文题目==&lt;br /&gt;
&lt;br /&gt;
'''T10. Greatest Eclipse (75 points)'''&lt;br /&gt;
&lt;br /&gt;
The greatest eclipse is defined as the instant when the axis of the Moon's shadow cone gets closest to the centre of the Earth in a solar eclipse. This problem explores the geometry of this phenomenon, using the solar eclipse of 29\(^\text{th}\) May 1919 as an example, as it has great historical significance for being the first time astronomers were able to observationally verify general relativity. One of the scientific expeditions to observe this eclipse took place in the Brazilian city of Sobral.&lt;br /&gt;
&lt;br /&gt;
The two following tables show the Cartesian and spherical coordinates of the Sun and the Moon at the time of the greatest eclipse. The system used for these coordinates is right-handed and has the origin at the centre of the Earth, the positive \(x\)-axis pointing towards the Greenwich meridian, and the positive \(z\)-axis pointing towards the North Pole. For the rest of this problem, this will be referred to as System I.&lt;br /&gt;
&lt;br /&gt;
'''Spherical Coordinates:'''&lt;br /&gt;
&lt;br /&gt;
{| class=&amp;quot;wikitable&amp;quot;&lt;br /&gt;
|-&lt;br /&gt;
! !! Centre of the Sun !! Centre of the Moon&lt;br /&gt;
|-&lt;br /&gt;
| Radial Distance (\(r\)) || \(1.516 \times 10^{11}\) m || \(3.589 \times 10^8\) m&lt;br /&gt;
|-&lt;br /&gt;
| Polar Angle (\(\theta\)) || \(68^{\circ}29'44.1''\) || \(68^{\circ}47'41.6''\)&lt;br /&gt;
|-&lt;br /&gt;
| Azimuthal Angle (\(\varphi\)) || \(-1^h11^{m}28.2^s\) || \(-1^h11^{m}22.9^s\)&lt;br /&gt;
|}&lt;br /&gt;
&lt;br /&gt;
'''Cartesian Coordinates:'''&lt;br /&gt;
&lt;br /&gt;
{| class=&amp;quot;wikitable&amp;quot;&lt;br /&gt;
|-&lt;br /&gt;
! !! Centre of the Sun !! Centre of the Moon&lt;br /&gt;
|-&lt;br /&gt;
| \(x\) || \(1.342 \times 10^{11}\) m || \(3.185 \times 10^8\) m&lt;br /&gt;
|-&lt;br /&gt;
| \(y\) || \(-4.327 \times 10^{10}\) m || \(-1.025 \times 10^8\) m&lt;br /&gt;
|-&lt;br /&gt;
| \(z\) || \(5.557 \times 10^{10}\) m || \(1.298 \times 10^8\) m&lt;br /&gt;
|}&lt;br /&gt;
&lt;br /&gt;
For this problem, assume that the Earth is a perfect sphere.&lt;br /&gt;
&lt;br /&gt;
'''Note:''' The spherical coordinates of a point \(P\) are defined as follows:&lt;br /&gt;
&lt;br /&gt;
- Radial distance (\(r\)): distance between the origin (\(O\)) and \(P\) (range: \(r \geq 0\)).&lt;br /&gt;
- Polar angle (\(\theta\)): angle between the positive \(z\)-axis and the line segment \(OP\) (range: \(0^{\circ} \leq \theta \leq 180^{\circ}\)).&lt;br /&gt;
- Azimuthal angle (\(\varphi\)): angle between the positive \(x\)-axis and the projection of the line segment \(OP\) onto the \(xy\)-plane (range: \(-12^h \leq \varphi &amp;lt; 12^h\)).&lt;br /&gt;
&lt;br /&gt;
=== Part I: Geographic Coordinates (25 points) ===&lt;br /&gt;
&lt;br /&gt;
(a) (3 points) Determine the declination of the Sun and the Moon during the greatest eclipse for a geocentric observer.&lt;br /&gt;
&lt;br /&gt;
(b) (3 points) Determine the right ascension of the Sun and the Moon at the time of the greatest eclipse for a geocentric observer. The local sidereal time at Greenwich at that same moment was \(5^h32^m35.5^s\).&lt;br /&gt;
&lt;br /&gt;
(c) (4 points) Find a unit vector that indicates the direction of the axis of the Moon’s shadow cone. This vector should point from the Moon to the vicinity of the centre of the Earth.&lt;br /&gt;
&lt;br /&gt;
(d) (15 points) Determine the latitude and the longitude of the point where the axis of the Moon's shadow cone crosses the surface of the Earth during the greatest eclipse.&lt;br /&gt;
&lt;br /&gt;
=== Part II: Duration of the Totality (50 points) ===&lt;br /&gt;
&lt;br /&gt;
Precisely determining the duration of totality of a solar eclipse involves complex calculations that would be beyond the scope of this problem. However, it is possible to obtain a reasonable approximation for this value using the two following assumptions:&lt;br /&gt;
&lt;br /&gt;
- The size of the umbra on the surface of the Earth remains roughly constant throughout totality at a given location.&lt;br /&gt;
- The velocity of the umbra on the surface of the Earth remains roughly constant throughout totality at a given location.&lt;br /&gt;
&lt;br /&gt;
(e) (10 points) Estimate the radius of the umbra during the greatest eclipse. In order to simplify the calculations, assume that the umbra is small enough that it can be considered approximately flat and that the axis of the Moon's shadow cone is extremely close to the centre of the Earth during the greatest eclipse.&lt;br /&gt;
&lt;br /&gt;
(f) (3 points) Calculate the velocity of the Earth's rotation at the latitude of the centre of the umbra.&lt;br /&gt;
&lt;br /&gt;
(g) (4 points) Determine the orbital velocity of the Moon at the instant of the greatest eclipse. Neglect the changes in the semi-major axis of the Moon’s orbit.&lt;br /&gt;
&lt;br /&gt;
For the remaining items of this problem, assume that the tangential velocity of the Moon is roughly the same as the orbital velocity and neglect its radial component.&lt;br /&gt;
&lt;br /&gt;
(h) (14 points) Using System II, determine the velocity vector of the Moon during the greatest eclipse. Note that the intersection between the Celestial Equator and the lunar orbit that is closer to the position of the eclipse has a right ascension of \(23^{h}07^{m}59.2^s\).&lt;br /&gt;
&lt;br /&gt;
(i) (10 points) Write the velocity vector of the Moon in System III. Note that in System I, the azimuthal angle difference between the positions of the origins OII and OIII is negligible, so you should only take into account the difference in the polar angles.&lt;br /&gt;
&lt;br /&gt;
(j) (6 points) Calculate the speed of the centre of the umbra along the surface of the Earth at the instant of the greatest eclipse.&lt;br /&gt;
&lt;br /&gt;
(k) (3 points) Estimate the duration of the totality of the eclipse at the location with the coordinates found in part (d).&lt;br /&gt;
&lt;br /&gt;
==中文翻译==&lt;br /&gt;
&lt;br /&gt;
'''T10. 最大食分（75分）'''&lt;br /&gt;
&lt;br /&gt;
最大食分定义为月球本影锥轴最接近地球中心的时刻。本问题以1919年5月29日日食为例探讨该现象的几何学，此次日食因首次通过观测验证广义相对论而具有重大历史意义。科学考察队之一在巴西索布拉尔市观测了此次日食。&lt;br /&gt;
&lt;br /&gt;
下表展示了最大食分时刻太阳和月球的球面坐标与笛卡尔坐标。坐标系为右手系，原点在地球中心，$x$轴正向指向格林尼治子午线，$z$轴正向指向北极点。下文中称此坐标系为**系统I**。&lt;br /&gt;
&lt;br /&gt;
'''球面坐标系：'''&lt;br /&gt;
{| class=&amp;quot;wikitable&amp;quot;&lt;br /&gt;
|-&lt;br /&gt;
! !! 太阳中心 !! 月球中心&lt;br /&gt;
|-&lt;br /&gt;
! 径向距离（$r$）&lt;br /&gt;
| $1.516 \times 10^{11}$ 米 || $3.589 \times 10^{8}$ 米&lt;br /&gt;
|-&lt;br /&gt;
! 极角（$\theta$）&lt;br /&gt;
| $68^\circ29'44.1''$ || $68^\circ47'41.6''$&lt;br /&gt;
|-&lt;br /&gt;
! 方位角（$\varphi$）&lt;br /&gt;
| $-1^h11^m28.2^s$ || $-1^h11^m22.9^s$&lt;br /&gt;
|}&lt;br /&gt;
&lt;br /&gt;
'''笛卡尔坐标系：'''&lt;br /&gt;
{| class=&amp;quot;wikitable&amp;quot;&lt;br /&gt;
|-&lt;br /&gt;
! !! 太阳中心 !! 月球中心&lt;br /&gt;
|-&lt;br /&gt;
! $x$&lt;br /&gt;
| $1.342 \times 10^{11}$ 米 || $3.185 \times 10^{8}$ 米&lt;br /&gt;
|-&lt;br /&gt;
! $y$&lt;br /&gt;
| $-4.327 \times 10^{10}$ 米 || $-1.025 \times 10^{8}$ 米&lt;br /&gt;
|-&lt;br /&gt;
! $z$&lt;br /&gt;
| $5.557 \times 10^{10}$ 米 || $1.298 \times 10^{8}$ 米&lt;br /&gt;
|}&lt;br /&gt;
&lt;br /&gt;
==官方解答==&lt;br /&gt;
&lt;br /&gt;
=== Part I: 地理坐标 ===&lt;br /&gt;
(a) 太阳和月球的赤纬：&lt;br /&gt;
$$$\delta = 90^\circ - \theta$$$&lt;br /&gt;
$$$\delta_\odot = 21^\circ30'15.9''$$$&lt;br /&gt;
$$$\delta_{Moon} = 21^\circ12'18.4''$$$&lt;br /&gt;
&lt;br /&gt;
(b) 太阳和月球的赤经（格林尼治恒星时为$5^h32^m35.5^s$）：&lt;br /&gt;
$$$\alpha = \varphi + LST_{Greenwich}$$$&lt;br /&gt;
$$$\alpha_\odot = 4^h21^m7.3^s$$$&lt;br /&gt;
$$$\alpha_{Moon} = 4^h21^m12.6^s$$$&lt;br /&gt;
&lt;br /&gt;
(c) 月球本影轴方向单位向量：&lt;br /&gt;
$$$\vec{u} = \left\langle -0.8855, 0.2855, -0.3666 \right\rangle$$$&lt;br /&gt;
&lt;br /&gt;
(d) 本影轴与地球表面交点坐标：&lt;br /&gt;
通过方程$$|\vec{M} + k\vec{u}| = R_\oplus$$解得：&lt;br /&gt;
$$$\phi = 4^\circ22'N$$$&lt;br /&gt;
$$$\lambda = 16^\circ42'W$$$&lt;br /&gt;
&lt;br /&gt;
=== Part II: 全食持续时间 ===&lt;br /&gt;
(e) 本影半径估算：&lt;br /&gt;
$$$r_{umbra} = 1.196 \times 10^5 \, \text{m}$$$&lt;br /&gt;
&lt;br /&gt;
(f) 地球自转线速度：&lt;br /&gt;
$$$v_{rot} = 463.7 \, \text{m/s}$$$&lt;br /&gt;
&lt;br /&gt;
(g) 月球轨道速度（忽略半长轴变化）：&lt;br /&gt;
$$$v_{Moon} = 1088 \, \text{m/s}$$$&lt;br /&gt;
&lt;br /&gt;
(h) 系统II中月球速度向量：&lt;br /&gt;
$$$\mathbf{v_{II}} = \begin{bmatrix} 1085 \, \text{m/s} \\ 81.25 \, \text{m/s} \\ 0 \end{bmatrix}$$$&lt;br /&gt;
&lt;br /&gt;
(i) 系统III中月球速度向量：&lt;br /&gt;
$$$\mathbf{v_{III}} = \begin{bmatrix} 1085 \, \text{m/s} \\ 77.76 \, \text{m/s} \\ -23.54 \, \text{m/s} \end{bmatrix}$$$&lt;br /&gt;
&lt;br /&gt;
(j) 本影中心地表移动速度：&lt;br /&gt;
$$$v_{umbra} = \sqrt{621.4^2 + 77.76^2} = 626.3 \, \text{m/s}$$$&lt;br /&gt;
&lt;br /&gt;
(k) 全食持续时间：&lt;br /&gt;
$$$\Delta t = \frac{2r_{umbra}}{v_{umbra}} = 6\,\text{分钟}\,21.4\,\text{秒}$$$&lt;br /&gt;
&lt;br /&gt;
[[分类:日月食]]&lt;br /&gt;
[[分类:球面三角]]&lt;br /&gt;
[[分类:由ai生成]]&lt;/div&gt;</summary>
		<author><name>Quan787</name></author>
		
	</entry>
	<entry>
		<id>https://www.astro-init.top/index.php?title=2024%E5%B9%B4IOAA%E7%90%86%E8%AE%BA%E7%AC%AC10%E9%A2%98-%E6%9C%80%E5%A4%A7%E6%97%A5%E9%A3%9F&amp;diff=2747</id>
		<title>2024年IOAA理论第10题-最大日食</title>
		<link rel="alternate" type="text/html" href="https://www.astro-init.top/index.php?title=2024%E5%B9%B4IOAA%E7%90%86%E8%AE%BA%E7%AC%AC10%E9%A2%98-%E6%9C%80%E5%A4%A7%E6%97%A5%E9%A3%9F&amp;diff=2747"/>
		<updated>2025-03-08T13:30:20Z</updated>

		<summary type="html">&lt;p&gt;Quan787：&lt;/p&gt;
&lt;hr /&gt;
&lt;div&gt;{{由ai生成}}&lt;br /&gt;
==英文题目==&lt;br /&gt;
&lt;br /&gt;
'''T10. Greatest Eclipse (75 points)'''&lt;br /&gt;
&lt;br /&gt;
The greatest eclipse is defined as the instant when the axis of the Moon's shadow cone gets closest to the centre of the Earth in a solar eclipse. This problem explores the geometry of this phenomenon, using the solar eclipse of 29\(^\text{th}\) May 1919 as an example, as it has great historical significance for being the first time astronomers were able to observationally verify general relativity. One of the scientific expeditions to observe this eclipse took place in the Brazilian city of Sobral.&lt;br /&gt;
&lt;br /&gt;
The two following tables show the Cartesian and spherical coordinates of the Sun and the Moon at the time of the greatest eclipse. The system used for these coordinates is right-handed and has the origin at the centre of the Earth, the positive \(x\)-axis pointing towards the Greenwich meridian, and the positive \(z\)-axis pointing towards the North Pole. For the rest of this problem, this will be referred to as System I.&lt;br /&gt;
&lt;br /&gt;
Spherical Coordinates:&lt;br /&gt;
&lt;br /&gt;
|    | Centre of the Sun    | Centre of the Moon    |&lt;br /&gt;
|---|---|---|&lt;br /&gt;
| Radial Distance (\(r\))   | \(1.516 \times 10^{11}\) m    | \(3.589 \times 10^8\) m    |&lt;br /&gt;
| Polar Angle (\(\theta\))   | \(68^{\circ}29'44.1''\)    | \(68^{\circ}47'41.6''\)    |&lt;br /&gt;
| Azimuthal Angle (\(\varphi\)) | \(-1^h11^{m}28.2^s\)    | \(-1^h11^{m}22.9^s\)    |&lt;br /&gt;
&lt;br /&gt;
Cartesian Coordinates:&lt;br /&gt;
&lt;br /&gt;
|    | Centre of the Sun    | Centre of the Moon    |&lt;br /&gt;
|---|---|---|&lt;br /&gt;
| \(x\)    | \(1.342 \times 10^{11}\) m    | \(3.185 \times 10^8\) m    |&lt;br /&gt;
| \(y\)    | \(-4.327 \times 10^{10}\) m    | \(-1.025 \times 10^8\) m    |&lt;br /&gt;
| \(z\)    | \(5.557 \times 10^{10}\) m    | \(1.298 \times 10^8\) m    |&lt;br /&gt;
&lt;br /&gt;
For this problem, assume that the Earth is a perfect sphere.&lt;br /&gt;
&lt;br /&gt;
Note: The spherical coordinates of a point \(P\) are defined as follows:&lt;br /&gt;
- Radial distance (\(r\)): distance between the origin (\(O\)) and \(P\) (range: \(r \geq 0\)).&lt;br /&gt;
- Polar angle (\(\theta\)): angle between the positive \(z\)-axis and the line segment \(OP\) (range: \(0^{\circ} \leq \theta \leq 180^{\circ}\)).&lt;br /&gt;
- Azimuthal angle (\(\varphi\)): angle between the positive \(x\)-axis and the projection of the line segment \(OP\) onto the \(xy\)-plane (range: \(-12^h \leq \varphi &amp;lt; 12^h\)).&lt;br /&gt;
&lt;br /&gt;
===== Part I: Geographic Coordinates (25 points) =====&lt;br /&gt;
&lt;br /&gt;
(a) (3 points) Determine the declination of the Sun and the Moon during the greatest eclipse for a geocentric observer.&lt;br /&gt;
&lt;br /&gt;
(b) (3 points) Determine the right ascension of the Sun and the Moon at the time of the greatest eclipse for a geocentric observer. The local sidereal time at Greenwich at that same moment was \(5^h32^m35.5^s\).&lt;br /&gt;
&lt;br /&gt;
(c) (4 points) Find a unit vector that indicates the direction of the axis of the Moon’s shadow cone. This vector should point from the Moon to the vicinity of the centre of the Earth.&lt;br /&gt;
&lt;br /&gt;
(d) (15 points) Determine the latitude and the longitude of the point where the axis of the Moon's shadow cone crosses the surface of the Earth during the greatest eclipse.&lt;br /&gt;
&lt;br /&gt;
===== Part II: Duration of the Totality (50 points) =====&lt;br /&gt;
&lt;br /&gt;
Precisely determining the duration of totality of a solar eclipse involves complex calculations that would be beyond the scope of this problem. However, it is possible to obtain a reasonable approximation for this value using the two following assumptions:&lt;br /&gt;
- The size of the umbra on the surface of the Earth remains roughly constant throughout totality at a given location.&lt;br /&gt;
- The velocity of the umbra on the surface of the Earth remains roughly constant throughout totality at a given location.&lt;br /&gt;
&lt;br /&gt;
(e) (10 points) Estimate the radius of the umbra during the greatest eclipse. In order to simplify the calculations, assume that the umbra is small enough that it can be considered approximately flat and that the axis of the Moon's shadow cone is extremely close to the centre of the Earth during the greatest eclipse.&lt;br /&gt;
&lt;br /&gt;
(f) (3 points) Calculate the velocity of the Earth's rotation at the latitude of the centre of the umbra.&lt;br /&gt;
&lt;br /&gt;
(g) (4 points) Determine the orbital velocity of the Moon at the instant of the greatest eclipse. Neglect the changes in the semi-major axis of the Moon’s orbit.&lt;br /&gt;
&lt;br /&gt;
For the remaining items of this problem, assume that the tangential velocity of the Moon is roughly the same as the orbital velocity and neglect its radial component.&lt;br /&gt;
&lt;br /&gt;
(h) (14 points) Using System II, determine the velocity vector of the Moon during the greatest eclipse. Note that the intersection between the Celestial Equator and the lunar orbit that is closer to the position of the eclipse has a right ascension of \(23^{h}07^{m}59.2^s\).&lt;br /&gt;
&lt;br /&gt;
(i) (10 points) Write the velocity vector of the Moon in System III. Note that in System I, the azimuthal angle difference between the positions of the origins \(O_{\text{II}}\) and \(O_{\text{III}}\) is negligible, so you should only take into account the difference in the polar angles.&lt;br /&gt;
&lt;br /&gt;
(j) (6 points) Calculate the speed of the centre of the umbra along the surface of the Earth at the instant of the greatest eclipse.&lt;br /&gt;
&lt;br /&gt;
(k) (3 points) Estimate the duration of the totality of the eclipse at the location with the coordinates found in part (d).&lt;br /&gt;
&lt;br /&gt;
[[分类:日月食]]&lt;br /&gt;
[[分类:天体力学]]&lt;br /&gt;
[[分类:由ai生成]]&lt;br /&gt;
&lt;br /&gt;
==中文翻译==&lt;br /&gt;
&lt;br /&gt;
'''T10. 最大食分（75分）'''&lt;br /&gt;
&lt;br /&gt;
最大食分定义为月球本影锥轴最接近地球中心的时刻。本问题以1919年5月29日日食为例探讨该现象的几何学，此次日食因首次通过观测验证广义相对论而具有重大历史意义。科学考察队之一在巴西索布拉尔市观测了此次日食。&lt;br /&gt;
&lt;br /&gt;
下表展示了最大食分时刻太阳和月球的球面坐标与笛卡尔坐标。坐标系为右手系，原点在地球中心，$x$轴正向指向格林尼治子午线，$z$轴正向指向北极点。下文中称此坐标系为**系统I**。&lt;br /&gt;
&lt;br /&gt;
'''球面坐标系：'''&lt;br /&gt;
{| class=&amp;quot;wikitable&amp;quot;&lt;br /&gt;
|-&lt;br /&gt;
! !! 太阳中心 !! 月球中心&lt;br /&gt;
|-&lt;br /&gt;
! 径向距离（$r$）&lt;br /&gt;
| $1.516 \times 10^{11}$ 米 || $3.589 \times 10^{8}$ 米&lt;br /&gt;
|-&lt;br /&gt;
! 极角（$\theta$）&lt;br /&gt;
| $68^\circ29'44.1''$ || $68^\circ47'41.6''$&lt;br /&gt;
|-&lt;br /&gt;
! 方位角（$\varphi$）&lt;br /&gt;
| $-1^h11^m28.2^s$ || $-1^h11^m22.9^s$&lt;br /&gt;
|}&lt;br /&gt;
&lt;br /&gt;
'''笛卡尔坐标系：'''&lt;br /&gt;
{| class=&amp;quot;wikitable&amp;quot;&lt;br /&gt;
|-&lt;br /&gt;
! !! 太阳中心 !! 月球中心&lt;br /&gt;
|-&lt;br /&gt;
! $x$&lt;br /&gt;
| $1.342 \times 10^{11}$ 米 || $3.185 \times 10^{8}$ 米&lt;br /&gt;
|-&lt;br /&gt;
! $y$&lt;br /&gt;
| $-4.327 \times 10^{10}$ 米 || $-1.025 \times 10^{8}$ 米&lt;br /&gt;
|-&lt;br /&gt;
! $z$&lt;br /&gt;
| $5.557 \times 10^{10}$ 米 || $1.298 \times 10^{8}$ 米&lt;br /&gt;
|}&lt;br /&gt;
&lt;br /&gt;
==官方解答==&lt;br /&gt;
&lt;br /&gt;
=== Part I: 地理坐标 ===&lt;br /&gt;
(a) 太阳和月球的赤纬：&lt;br /&gt;
$$$\delta = 90^\circ - \theta$$$&lt;br /&gt;
$$$\delta_\odot = 21^\circ30'15.9''$$$&lt;br /&gt;
$$$\delta_{Moon} = 21^\circ12'18.4''$$$&lt;br /&gt;
&lt;br /&gt;
(b) 太阳和月球的赤经（格林尼治恒星时为$5^h32^m35.5^s$）：&lt;br /&gt;
$$$\alpha = \varphi + LST_{Greenwich}$$$&lt;br /&gt;
$$$\alpha_\odot = 4^h21^m7.3^s$$$&lt;br /&gt;
$$$\alpha_{Moon} = 4^h21^m12.6^s$$$&lt;br /&gt;
&lt;br /&gt;
(c) 月球本影轴方向单位向量：&lt;br /&gt;
$$$\vec{u} = \left\langle -0.8855, 0.2855, -0.3666 \right\rangle$$$&lt;br /&gt;
&lt;br /&gt;
(d) 本影轴与地球表面交点坐标：&lt;br /&gt;
通过方程$$|\vec{M} + k\vec{u}| = R_\oplus$$解得：&lt;br /&gt;
$$$\phi = 4^\circ22'N$$$&lt;br /&gt;
$$$\lambda = 16^\circ42'W$$$&lt;br /&gt;
&lt;br /&gt;
=== Part II: 全食持续时间 ===&lt;br /&gt;
(e) 本影半径估算：&lt;br /&gt;
$$$r_{umbra} = 1.196 \times 10^5 \, \text{m}$$$&lt;br /&gt;
&lt;br /&gt;
(f) 地球自转线速度：&lt;br /&gt;
$$$v_{rot} = 463.7 \, \text{m/s}$$$&lt;br /&gt;
&lt;br /&gt;
(g) 月球轨道速度（忽略半长轴变化）：&lt;br /&gt;
$$$v_{Moon} = 1088 \, \text{m/s}$$$&lt;br /&gt;
&lt;br /&gt;
(h) 系统II中月球速度向量：&lt;br /&gt;
$$$\mathbf{v_{II}} = \begin{bmatrix} 1085 \, \text{m/s} \\ 81.25 \, \text{m/s} \\ 0 \end{bmatrix}$$$&lt;br /&gt;
&lt;br /&gt;
(i) 系统III中月球速度向量：&lt;br /&gt;
$$$\mathbf{v_{III}} = \begin{bmatrix} 1085 \, \text{m/s} \\ 77.76 \, \text{m/s} \\ -23.54 \, \text{m/s} \end{bmatrix}$$$&lt;br /&gt;
&lt;br /&gt;
(j) 本影中心地表移动速度：&lt;br /&gt;
$$$v_{umbra} = \sqrt{621.4^2 + 77.76^2} = 626.3 \, \text{m/s}$$$&lt;br /&gt;
&lt;br /&gt;
(k) 全食持续时间：&lt;br /&gt;
$$$\Delta t = \frac{2r_{umbra}}{v_{umbra}} = 6\,\text{分钟}\,21.4\,\text{秒}$$$&lt;br /&gt;
&lt;br /&gt;
[[分类:日月食]]&lt;br /&gt;
[[分类:球面三角]]&lt;br /&gt;
[[分类:由ai生成]]&lt;/div&gt;</summary>
		<author><name>Quan787</name></author>
		
	</entry>
	<entry>
		<id>https://www.astro-init.top/index.php?title=2024%E5%B9%B4IOAA%E7%90%86%E8%AE%BA%E7%AC%AC10%E9%A2%98-%E6%9C%80%E5%A4%A7%E6%97%A5%E9%A3%9F&amp;diff=2746</id>
		<title>2024年IOAA理论第10题-最大日食</title>
		<link rel="alternate" type="text/html" href="https://www.astro-init.top/index.php?title=2024%E5%B9%B4IOAA%E7%90%86%E8%AE%BA%E7%AC%AC10%E9%A2%98-%E6%9C%80%E5%A4%A7%E6%97%A5%E9%A3%9F&amp;diff=2746"/>
		<updated>2025-03-08T13:29:30Z</updated>

		<summary type="html">&lt;p&gt;Quan787：&lt;/p&gt;
&lt;hr /&gt;
&lt;div&gt;{{由ai生成}}&lt;br /&gt;
==英文题目==&lt;br /&gt;
&lt;br /&gt;
'''T10. Greatest Eclipse (75 points)'''&lt;br /&gt;
&lt;br /&gt;
The greatest eclipse is defined as the instant when the axis of the Moon's shadow cone gets closest to the centre of the Earth in a solar eclipse. This problem explores the geometry of this phenomenon, using the solar eclipse of 29\(^\text{th}\) May 1919 as an example, as it has great historical significance for being the first time astronomers were able to observationally verify general relativity. One of the scientific expeditions to observe this eclipse took place in the Brazilian city of Sobral.&lt;br /&gt;
&lt;br /&gt;
The two following tables show the Cartesian and spherical coordinates of the Sun and the Moon at the time of the greatest eclipse. The system used for these coordinates is right-handed and has the origin at the centre of the Earth, the positive \(x\)-axis pointing towards the Greenwich meridian, and the positive \(z\)-axis pointing towards the North Pole. For the rest of this problem, this will be referred to as System I.&lt;br /&gt;
&lt;br /&gt;
Spherical Coordinates:&lt;br /&gt;
{| class=&amp;quot;wikitable&amp;quot;&lt;br /&gt;
|    | Centre of the Sun    | Centre of the Moon    |&lt;br /&gt;
|---|---|---|&lt;br /&gt;
| Radial Distance (\(r\))   | \(1.516 \times 10^{11}\) m    | \(3.589 \times 10^8\) m    |&lt;br /&gt;
| Polar Angle (\(\theta\))   | \(68^{\circ}29'44.1''\)    | \(68^{\circ}47'41.6''\)    |&lt;br /&gt;
| Azimuthal Angle (\(\varphi\)) | \(-1^h11^{m}28.2^s\)    | \(-1^h11^{m}22.9^s\)    |}&lt;br /&gt;
&lt;br /&gt;
Cartesian Coordinates:&lt;br /&gt;
&lt;br /&gt;
{| class=&amp;quot;wikitable&amp;quot;|    | Centre of the Sun    | Centre of the Moon    |&lt;br /&gt;
|---|---|---|&lt;br /&gt;
| \(x\)    | \(1.342 \times 10^{11}\) m    | \(3.185 \times 10^8\) m    |&lt;br /&gt;
| \(y\)    | \(-4.327 \times 10^{10}\) m    | \(-1.025 \times 10^8\) m    |&lt;br /&gt;
| \(z\)    | \(5.557 \times 10^{10}\) m    | \(1.298 \times 10^8\) m    |}&lt;br /&gt;
&lt;br /&gt;
For this problem, assume that the Earth is a perfect sphere.&lt;br /&gt;
&lt;br /&gt;
Note: The spherical coordinates of a point \(P\) are defined as follows:&lt;br /&gt;
- Radial distance (\(r\)): distance between the origin (\(O\)) and \(P\) (range: \(r \geq 0\)).&lt;br /&gt;
- Polar angle (\(\theta\)): angle between the positive \(z\)-axis and the line segment \(OP\) (range: \(0^{\circ} \leq \theta \leq 180^{\circ}\)).&lt;br /&gt;
- Azimuthal angle (\(\varphi\)): angle between the positive \(x\)-axis and the projection of the line segment \(OP\) onto the \(xy\)-plane (range: \(-12^h \leq \varphi &amp;lt; 12^h\)).&lt;br /&gt;
&lt;br /&gt;
===== Part I: Geographic Coordinates (25 points) =====&lt;br /&gt;
&lt;br /&gt;
(a) (3 points) Determine the declination of the Sun and the Moon during the greatest eclipse for a geocentric observer.&lt;br /&gt;
&lt;br /&gt;
(b) (3 points) Determine the right ascension of the Sun and the Moon at the time of the greatest eclipse for a geocentric observer. The local sidereal time at Greenwich at that same moment was \(5^h32^m35.5^s\).&lt;br /&gt;
&lt;br /&gt;
(c) (4 points) Find a unit vector that indicates the direction of the axis of the Moon’s shadow cone. This vector should point from the Moon to the vicinity of the centre of the Earth.&lt;br /&gt;
&lt;br /&gt;
(d) (15 points) Determine the latitude and the longitude of the point where the axis of the Moon's shadow cone crosses the surface of the Earth during the greatest eclipse.&lt;br /&gt;
&lt;br /&gt;
===== Part II: Duration of the Totality (50 points) =====&lt;br /&gt;
&lt;br /&gt;
Precisely determining the duration of totality of a solar eclipse involves complex calculations that would be beyond the scope of this problem. However, it is possible to obtain a reasonable approximation for this value using the two following assumptions:&lt;br /&gt;
- The size of the umbra on the surface of the Earth remains roughly constant throughout totality at a given location.&lt;br /&gt;
- The velocity of the umbra on the surface of the Earth remains roughly constant throughout totality at a given location.&lt;br /&gt;
&lt;br /&gt;
(e) (10 points) Estimate the radius of the umbra during the greatest eclipse. In order to simplify the calculations, assume that the umbra is small enough that it can be considered approximately flat and that the axis of the Moon's shadow cone is extremely close to the centre of the Earth during the greatest eclipse.&lt;br /&gt;
&lt;br /&gt;
(f) (3 points) Calculate the velocity of the Earth's rotation at the latitude of the centre of the umbra.&lt;br /&gt;
&lt;br /&gt;
(g) (4 points) Determine the orbital velocity of the Moon at the instant of the greatest eclipse. Neglect the changes in the semi-major axis of the Moon’s orbit.&lt;br /&gt;
&lt;br /&gt;
For the remaining items of this problem, assume that the tangential velocity of the Moon is roughly the same as the orbital velocity and neglect its radial component.&lt;br /&gt;
&lt;br /&gt;
(h) (14 points) Using System II, determine the velocity vector of the Moon during the greatest eclipse. Note that the intersection between the Celestial Equator and the lunar orbit that is closer to the position of the eclipse has a right ascension of \(23^{h}07^{m}59.2^s\).&lt;br /&gt;
&lt;br /&gt;
(i) (10 points) Write the velocity vector of the Moon in System III. Note that in System I, the azimuthal angle difference between the positions of the origins \(O_{\text{II}}\) and \(O_{\text{III}}\) is negligible, so you should only take into account the difference in the polar angles.&lt;br /&gt;
&lt;br /&gt;
(j) (6 points) Calculate the speed of the centre of the umbra along the surface of the Earth at the instant of the greatest eclipse.&lt;br /&gt;
&lt;br /&gt;
(k) (3 points) Estimate the duration of the totality of the eclipse at the location with the coordinates found in part (d).&lt;br /&gt;
&lt;br /&gt;
[[分类:日月食]]&lt;br /&gt;
[[分类:天体力学]]&lt;br /&gt;
[[分类:由ai生成]]&lt;br /&gt;
&lt;br /&gt;
==中文翻译==&lt;br /&gt;
&lt;br /&gt;
'''T10. 最大食分（75分）'''&lt;br /&gt;
&lt;br /&gt;
最大食分定义为月球本影锥轴最接近地球中心的时刻。本问题以1919年5月29日日食为例探讨该现象的几何学，此次日食因首次通过观测验证广义相对论而具有重大历史意义。科学考察队之一在巴西索布拉尔市观测了此次日食。&lt;br /&gt;
&lt;br /&gt;
下表展示了最大食分时刻太阳和月球的球面坐标与笛卡尔坐标。坐标系为右手系，原点在地球中心，$x$轴正向指向格林尼治子午线，$z$轴正向指向北极点。下文中称此坐标系为**系统I**。&lt;br /&gt;
&lt;br /&gt;
'''球面坐标系：'''&lt;br /&gt;
{| class=&amp;quot;wikitable&amp;quot;&lt;br /&gt;
|-&lt;br /&gt;
! !! 太阳中心 !! 月球中心&lt;br /&gt;
|-&lt;br /&gt;
! 径向距离（$r$）&lt;br /&gt;
| $1.516 \times 10^{11}$ 米 || $3.589 \times 10^{8}$ 米&lt;br /&gt;
|-&lt;br /&gt;
! 极角（$\theta$）&lt;br /&gt;
| $68^\circ29'44.1''$ || $68^\circ47'41.6''$&lt;br /&gt;
|-&lt;br /&gt;
! 方位角（$\varphi$）&lt;br /&gt;
| $-1^h11^m28.2^s$ || $-1^h11^m22.9^s$&lt;br /&gt;
|}&lt;br /&gt;
&lt;br /&gt;
'''笛卡尔坐标系：'''&lt;br /&gt;
{| class=&amp;quot;wikitable&amp;quot;&lt;br /&gt;
|-&lt;br /&gt;
! !! 太阳中心 !! 月球中心&lt;br /&gt;
|-&lt;br /&gt;
! $x$&lt;br /&gt;
| $1.342 \times 10^{11}$ 米 || $3.185 \times 10^{8}$ 米&lt;br /&gt;
|-&lt;br /&gt;
! $y$&lt;br /&gt;
| $-4.327 \times 10^{10}$ 米 || $-1.025 \times 10^{8}$ 米&lt;br /&gt;
|-&lt;br /&gt;
! $z$&lt;br /&gt;
| $5.557 \times 10^{10}$ 米 || $1.298 \times 10^{8}$ 米&lt;br /&gt;
|}&lt;br /&gt;
&lt;br /&gt;
==官方解答==&lt;br /&gt;
&lt;br /&gt;
=== Part I: 地理坐标 ===&lt;br /&gt;
(a) 太阳和月球的赤纬：&lt;br /&gt;
$$$\delta = 90^\circ - \theta$$$&lt;br /&gt;
$$$\delta_\odot = 21^\circ30'15.9''$$$&lt;br /&gt;
$$$\delta_{Moon} = 21^\circ12'18.4''$$$&lt;br /&gt;
&lt;br /&gt;
(b) 太阳和月球的赤经（格林尼治恒星时为$5^h32^m35.5^s$）：&lt;br /&gt;
$$$\alpha = \varphi + LST_{Greenwich}$$$&lt;br /&gt;
$$$\alpha_\odot = 4^h21^m7.3^s$$$&lt;br /&gt;
$$$\alpha_{Moon} = 4^h21^m12.6^s$$$&lt;br /&gt;
&lt;br /&gt;
(c) 月球本影轴方向单位向量：&lt;br /&gt;
$$$\vec{u} = \left\langle -0.8855, 0.2855, -0.3666 \right\rangle$$$&lt;br /&gt;
&lt;br /&gt;
(d) 本影轴与地球表面交点坐标：&lt;br /&gt;
通过方程$$|\vec{M} + k\vec{u}| = R_\oplus$$解得：&lt;br /&gt;
$$$\phi = 4^\circ22'N$$$&lt;br /&gt;
$$$\lambda = 16^\circ42'W$$$&lt;br /&gt;
&lt;br /&gt;
=== Part II: 全食持续时间 ===&lt;br /&gt;
(e) 本影半径估算：&lt;br /&gt;
$$$r_{umbra} = 1.196 \times 10^5 \, \text{m}$$$&lt;br /&gt;
&lt;br /&gt;
(f) 地球自转线速度：&lt;br /&gt;
$$$v_{rot} = 463.7 \, \text{m/s}$$$&lt;br /&gt;
&lt;br /&gt;
(g) 月球轨道速度（忽略半长轴变化）：&lt;br /&gt;
$$$v_{Moon} = 1088 \, \text{m/s}$$$&lt;br /&gt;
&lt;br /&gt;
(h) 系统II中月球速度向量：&lt;br /&gt;
$$$\mathbf{v_{II}} = \begin{bmatrix} 1085 \, \text{m/s} \\ 81.25 \, \text{m/s} \\ 0 \end{bmatrix}$$$&lt;br /&gt;
&lt;br /&gt;
(i) 系统III中月球速度向量：&lt;br /&gt;
$$$\mathbf{v_{III}} = \begin{bmatrix} 1085 \, \text{m/s} \\ 77.76 \, \text{m/s} \\ -23.54 \, \text{m/s} \end{bmatrix}$$$&lt;br /&gt;
&lt;br /&gt;
(j) 本影中心地表移动速度：&lt;br /&gt;
$$$v_{umbra} = \sqrt{621.4^2 + 77.76^2} = 626.3 \, \text{m/s}$$$&lt;br /&gt;
&lt;br /&gt;
(k) 全食持续时间：&lt;br /&gt;
$$$\Delta t = \frac{2r_{umbra}}{v_{umbra}} = 6\,\text{分钟}\,21.4\,\text{秒}$$$&lt;br /&gt;
&lt;br /&gt;
[[分类:日月食]]&lt;br /&gt;
[[分类:球面三角]]&lt;br /&gt;
[[分类:由ai生成]]&lt;/div&gt;</summary>
		<author><name>Quan787</name></author>
		
	</entry>
	<entry>
		<id>https://www.astro-init.top/index.php?title=2024%E5%B9%B4IOAA%E7%90%86%E8%AE%BA%E7%AC%AC10%E9%A2%98-%E6%9C%80%E5%A4%A7%E6%97%A5%E9%A3%9F&amp;diff=2745</id>
		<title>2024年IOAA理论第10题-最大日食</title>
		<link rel="alternate" type="text/html" href="https://www.astro-init.top/index.php?title=2024%E5%B9%B4IOAA%E7%90%86%E8%AE%BA%E7%AC%AC10%E9%A2%98-%E6%9C%80%E5%A4%A7%E6%97%A5%E9%A3%9F&amp;diff=2745"/>
		<updated>2025-03-08T13:28:49Z</updated>

		<summary type="html">&lt;p&gt;Quan787：&lt;/p&gt;
&lt;hr /&gt;
&lt;div&gt;{{由ai生成}}&lt;br /&gt;
==英文题目==&lt;br /&gt;
&lt;br /&gt;
'''T10. Greatest Eclipse (75 points)'''&lt;br /&gt;
&lt;br /&gt;
The greatest eclipse is defined as the instant when the axis of the Moon's shadow cone gets closest to the centre of the Earth in a solar eclipse. This problem explores the geometry of this phenomenon, using the solar eclipse of 29\(^\text{th}\) May 1919 as an example, as it has great historical significance for being the first time astronomers were able to observationally verify general relativity. One of the scientific expeditions to observe this eclipse took place in the Brazilian city of Sobral.&lt;br /&gt;
&lt;br /&gt;
The two following tables show the Cartesian and spherical coordinates of the Sun and the Moon at the time of the greatest eclipse. The system used for these coordinates is right-handed and has the origin at the centre of the Earth, the positive \(x\)-axis pointing towards the Greenwich meridian, and the positive \(z\)-axis pointing towards the North Pole. For the rest of this problem, this will be referred to as System I.&lt;br /&gt;
&lt;br /&gt;
Spherical Coordinates:&lt;br /&gt;
&lt;br /&gt;
|    | Centre of the Sun    | Centre of the Moon    |&lt;br /&gt;
|---|---|---|&lt;br /&gt;
| Radial Distance (\(r\))   | \(1.516 \times 10^{11}\) m    | \(3.589 \times 10^8\) m    |&lt;br /&gt;
| Polar Angle (\(\theta\))   | \(68^{\circ}29'44.1''\)    | \(68^{\circ}47'41.6''\)    |&lt;br /&gt;
| Azimuthal Angle (\(\varphi\)) | \(-1^h11^{m}28.2^s\)    | \(-1^h11^{m}22.9^s\)    |&lt;br /&gt;
&lt;br /&gt;
Cartesian Coordinates:&lt;br /&gt;
&lt;br /&gt;
|    | Centre of the Sun    | Centre of the Moon    |&lt;br /&gt;
|---|---|---|&lt;br /&gt;
| \(x\)    | \(1.342 \times 10^{11}\) m    | \(3.185 \times 10^8\) m    |&lt;br /&gt;
| \(y\)    | \(-4.327 \times 10^{10}\) m    | \(-1.025 \times 10^8\) m    |&lt;br /&gt;
| \(z\)    | \(5.557 \times 10^{10}\) m    | \(1.298 \times 10^8\) m    |&lt;br /&gt;
&lt;br /&gt;
For this problem, assume that the Earth is a perfect sphere.&lt;br /&gt;
&lt;br /&gt;
Note: The spherical coordinates of a point \(P\) are defined as follows:&lt;br /&gt;
- Radial distance (\(r\)): distance between the origin (\(O\)) and \(P\) (range: \(r \geq 0\)).&lt;br /&gt;
- Polar angle (\(\theta\)): angle between the positive \(z\)-axis and the line segment \(OP\) (range: \(0^{\circ} \leq \theta \leq 180^{\circ}\)).&lt;br /&gt;
- Azimuthal angle (\(\varphi\)): angle between the positive \(x\)-axis and the projection of the line segment \(OP\) onto the \(xy\)-plane (range: \(-12^h \leq \varphi &amp;lt; 12^h\)).&lt;br /&gt;
&lt;br /&gt;
===== Part I: Geographic Coordinates (25 points) =====&lt;br /&gt;
&lt;br /&gt;
(a) (3 points) Determine the declination of the Sun and the Moon during the greatest eclipse for a geocentric observer.&lt;br /&gt;
&lt;br /&gt;
(b) (3 points) Determine the right ascension of the Sun and the Moon at the time of the greatest eclipse for a geocentric observer. The local sidereal time at Greenwich at that same moment was \(5^h32^m35.5^s\).&lt;br /&gt;
&lt;br /&gt;
(c) (4 points) Find a unit vector that indicates the direction of the axis of the Moon’s shadow cone. This vector should point from the Moon to the vicinity of the centre of the Earth.&lt;br /&gt;
&lt;br /&gt;
(d) (15 points) Determine the latitude and the longitude of the point where the axis of the Moon's shadow cone crosses the surface of the Earth during the greatest eclipse.&lt;br /&gt;
&lt;br /&gt;
===== Part II: Duration of the Totality (50 points) =====&lt;br /&gt;
&lt;br /&gt;
Precisely determining the duration of totality of a solar eclipse involves complex calculations that would be beyond the scope of this problem. However, it is possible to obtain a reasonable approximation for this value using the two following assumptions:&lt;br /&gt;
- The size of the umbra on the surface of the Earth remains roughly constant throughout totality at a given location.&lt;br /&gt;
- The velocity of the umbra on the surface of the Earth remains roughly constant throughout totality at a given location.&lt;br /&gt;
&lt;br /&gt;
(e) (10 points) Estimate the radius of the umbra during the greatest eclipse. In order to simplify the calculations, assume that the umbra is small enough that it can be considered approximately flat and that the axis of the Moon's shadow cone is extremely close to the centre of the Earth during the greatest eclipse.&lt;br /&gt;
&lt;br /&gt;
(f) (3 points) Calculate the velocity of the Earth's rotation at the latitude of the centre of the umbra.&lt;br /&gt;
&lt;br /&gt;
(g) (4 points) Determine the orbital velocity of the Moon at the instant of the greatest eclipse. Neglect the changes in the semi-major axis of the Moon’s orbit.&lt;br /&gt;
&lt;br /&gt;
For the remaining items of this problem, assume that the tangential velocity of the Moon is roughly the same as the orbital velocity and neglect its radial component.&lt;br /&gt;
&lt;br /&gt;
(h) (14 points) Using System II, determine the velocity vector of the Moon during the greatest eclipse. Note that the intersection between the Celestial Equator and the lunar orbit that is closer to the position of the eclipse has a right ascension of \(23^{h}07^{m}59.2^s\).&lt;br /&gt;
&lt;br /&gt;
(i) (10 points) Write the velocity vector of the Moon in System III. Note that in System I, the azimuthal angle difference between the positions of the origins \(O_{\text{II}}\) and \(O_{\text{III}}\) is negligible, so you should only take into account the difference in the polar angles.&lt;br /&gt;
&lt;br /&gt;
(j) (6 points) Calculate the speed of the centre of the umbra along the surface of the Earth at the instant of the greatest eclipse.&lt;br /&gt;
&lt;br /&gt;
(k) (3 points) Estimate the duration of the totality of the eclipse at the location with the coordinates found in part (d).&lt;br /&gt;
&lt;br /&gt;
[[分类:日月食]]&lt;br /&gt;
[[分类:天体力学]]&lt;br /&gt;
[[分类:由ai生成]]&lt;br /&gt;
&lt;br /&gt;
==中文翻译==&lt;br /&gt;
&lt;br /&gt;
'''T10. 最大食分（75分）'''&lt;br /&gt;
&lt;br /&gt;
最大食分定义为月球本影锥轴最接近地球中心的时刻。本问题以1919年5月29日日食为例探讨该现象的几何学，此次日食因首次通过观测验证广义相对论而具有重大历史意义。科学考察队之一在巴西索布拉尔市观测了此次日食。&lt;br /&gt;
&lt;br /&gt;
下表展示了最大食分时刻太阳和月球的球面坐标与笛卡尔坐标。坐标系为右手系，原点在地球中心，$x$轴正向指向格林尼治子午线，$z$轴正向指向北极点。下文中称此坐标系为**系统I**。&lt;br /&gt;
&lt;br /&gt;
'''球面坐标系：'''&lt;br /&gt;
{| class=&amp;quot;wikitable&amp;quot;&lt;br /&gt;
|-&lt;br /&gt;
! !! 太阳中心 !! 月球中心&lt;br /&gt;
|-&lt;br /&gt;
! 径向距离（$r$）&lt;br /&gt;
| $1.516 \times 10^{11}$ 米 || $3.589 \times 10^{8}$ 米&lt;br /&gt;
|-&lt;br /&gt;
! 极角（$\theta$）&lt;br /&gt;
| $68^\circ29'44.1''$ || $68^\circ47'41.6''$&lt;br /&gt;
|-&lt;br /&gt;
! 方位角（$\varphi$）&lt;br /&gt;
| $-1^h11^m28.2^s$ || $-1^h11^m22.9^s$&lt;br /&gt;
|}&lt;br /&gt;
&lt;br /&gt;
'''笛卡尔坐标系：'''&lt;br /&gt;
{| class=&amp;quot;wikitable&amp;quot;&lt;br /&gt;
|-&lt;br /&gt;
! !! 太阳中心 !! 月球中心&lt;br /&gt;
|-&lt;br /&gt;
! $x$&lt;br /&gt;
| $1.342 \times 10^{11}$ 米 || $3.185 \times 10^{8}$ 米&lt;br /&gt;
|-&lt;br /&gt;
! $y$&lt;br /&gt;
| $-4.327 \times 10^{10}$ 米 || $-1.025 \times 10^{8}$ 米&lt;br /&gt;
|-&lt;br /&gt;
! $z$&lt;br /&gt;
| $5.557 \times 10^{10}$ 米 || $1.298 \times 10^{8}$ 米&lt;br /&gt;
|}&lt;br /&gt;
&lt;br /&gt;
==官方解答==&lt;br /&gt;
&lt;br /&gt;
=== Part I: 地理坐标 ===&lt;br /&gt;
(a) 太阳和月球的赤纬：&lt;br /&gt;
$$$\delta = 90^\circ - \theta$$$&lt;br /&gt;
$$$\delta_\odot = 21^\circ30'15.9''$$$&lt;br /&gt;
$$$\delta_{Moon} = 21^\circ12'18.4''$$$&lt;br /&gt;
&lt;br /&gt;
(b) 太阳和月球的赤经（格林尼治恒星时为$5^h32^m35.5^s$）：&lt;br /&gt;
$$$\alpha = \varphi + LST_{Greenwich}$$$&lt;br /&gt;
$$$\alpha_\odot = 4^h21^m7.3^s$$$&lt;br /&gt;
$$$\alpha_{Moon} = 4^h21^m12.6^s$$$&lt;br /&gt;
&lt;br /&gt;
(c) 月球本影轴方向单位向量：&lt;br /&gt;
$$$\vec{u} = \left\langle -0.8855, 0.2855, -0.3666 \right\rangle$$$&lt;br /&gt;
&lt;br /&gt;
(d) 本影轴与地球表面交点坐标：&lt;br /&gt;
通过方程$$|\vec{M} + k\vec{u}| = R_\oplus$$解得：&lt;br /&gt;
$$$\phi = 4^\circ22'N$$$&lt;br /&gt;
$$$\lambda = 16^\circ42'W$$$&lt;br /&gt;
&lt;br /&gt;
=== Part II: 全食持续时间 ===&lt;br /&gt;
(e) 本影半径估算：&lt;br /&gt;
$$$r_{umbra} = 1.196 \times 10^5 \, \text{m}$$$&lt;br /&gt;
&lt;br /&gt;
(f) 地球自转线速度：&lt;br /&gt;
$$$v_{rot} = 463.7 \, \text{m/s}$$$&lt;br /&gt;
&lt;br /&gt;
(g) 月球轨道速度（忽略半长轴变化）：&lt;br /&gt;
$$$v_{Moon} = 1088 \, \text{m/s}$$$&lt;br /&gt;
&lt;br /&gt;
(h) 系统II中月球速度向量：&lt;br /&gt;
$$$\mathbf{v_{II}} = \begin{bmatrix} 1085 \, \text{m/s} \\ 81.25 \, \text{m/s} \\ 0 \end{bmatrix}$$$&lt;br /&gt;
&lt;br /&gt;
(i) 系统III中月球速度向量：&lt;br /&gt;
$$$\mathbf{v_{III}} = \begin{bmatrix} 1085 \, \text{m/s} \\ 77.76 \, \text{m/s} \\ -23.54 \, \text{m/s} \end{bmatrix}$$$&lt;br /&gt;
&lt;br /&gt;
(j) 本影中心地表移动速度：&lt;br /&gt;
$$$v_{umbra} = \sqrt{621.4^2 + 77.76^2} = 626.3 \, \text{m/s}$$$&lt;br /&gt;
&lt;br /&gt;
(k) 全食持续时间：&lt;br /&gt;
$$$\Delta t = \frac{2r_{umbra}}{v_{umbra}} = 6\,\text{分钟}\,21.4\,\text{秒}$$$&lt;br /&gt;
&lt;br /&gt;
[[分类:日月食]]&lt;br /&gt;
[[分类:球面三角]]&lt;br /&gt;
[[分类:由ai生成]]&lt;/div&gt;</summary>
		<author><name>Quan787</name></author>
		
	</entry>
	<entry>
		<id>https://www.astro-init.top/index.php?title=2024%E5%B9%B4IOAA%E7%90%86%E8%AE%BA%E7%AC%AC10%E9%A2%98-%E6%9C%80%E5%A4%A7%E6%97%A5%E9%A3%9F&amp;diff=2744</id>
		<title>2024年IOAA理论第10题-最大日食</title>
		<link rel="alternate" type="text/html" href="https://www.astro-init.top/index.php?title=2024%E5%B9%B4IOAA%E7%90%86%E8%AE%BA%E7%AC%AC10%E9%A2%98-%E6%9C%80%E5%A4%A7%E6%97%A5%E9%A3%9F&amp;diff=2744"/>
		<updated>2025-03-08T11:10:25Z</updated>

		<summary type="html">&lt;p&gt;Quan787：创建页面，内容为“{{由ai生成}} ==英文题目==  '''T10. Greatest Eclipse (75 points)'''  The greatest eclipse is defined as the instant when the axis of the Moon's shadow cone get…”&lt;/p&gt;
&lt;hr /&gt;
&lt;div&gt;{{由ai生成}}&lt;br /&gt;
==英文题目==&lt;br /&gt;
&lt;br /&gt;
'''T10. Greatest Eclipse (75 points)'''&lt;br /&gt;
&lt;br /&gt;
The greatest eclipse is defined as the instant when the axis of the Moon's shadow cone gets closest to the centre of the Earth in a solar eclipse. This problem explores the geometry of this phenomenon, using the solar eclipse of 29$^\text{th}$ May 1919 as an example, as it has great historical significance for being the first time astronomers were able to observationally verify general relativity. One of the scientific expeditions to observe this eclipse took place in the Brazilian city of Sobral.&lt;br /&gt;
&lt;br /&gt;
The two following tables show the Cartesian and spherical coordinates of the Sun and the Moon at the time of the greatest eclipse. The system used for these coordinates is right-handed and has the origin at the centre of the Earth, the positive $x$-axis pointing towards the Greenwich meridian, and the positive $z$-axis pointing towards the North Pole. For the rest of this problem, this will be referred to as **System I**.&lt;br /&gt;
&lt;br /&gt;
'''Spherical Coordinates:'''&lt;br /&gt;
{| class=&amp;quot;wikitable&amp;quot;&lt;br /&gt;
|-&lt;br /&gt;
! !! Centre of the Sun !! Centre of the Moon&lt;br /&gt;
|-&lt;br /&gt;
! Radial Distance ($r$)&lt;br /&gt;
| $1.516 \times 10^{11}$ m || $3.589 \times 10^{8}$ m&lt;br /&gt;
|-&lt;br /&gt;
! Polar Angle ($\theta$)&lt;br /&gt;
| $68^\circ29'44.1''$ || $68^\circ47'41.6''$&lt;br /&gt;
|-&lt;br /&gt;
! Azimuthal Angle ($\varphi$)&lt;br /&gt;
| $-1^h11^m28.2^s$ || $-1^h11^m22.9^s$&lt;br /&gt;
|}&lt;br /&gt;
&lt;br /&gt;
'''Cartesian Coordinates:'''&lt;br /&gt;
{| class=&amp;quot;wikitable&amp;quot;&lt;br /&gt;
|-&lt;br /&gt;
! !! Centre of the Sun !! Centre of the Moon&lt;br /&gt;
|-&lt;br /&gt;
! $x$&lt;br /&gt;
| $1.342 \times 10^{11}$ m || $3.185 \times 10^{8}$ m&lt;br /&gt;
|-&lt;br /&gt;
! $y$&lt;br /&gt;
| $-4.327 \times 10^{10}$ m || $-1.025 \times 10^{8}$ m&lt;br /&gt;
|-&lt;br /&gt;
! $z$&lt;br /&gt;
| $5.557 \times 10^{10}$ m || $1.298 \times 10^{8}$ m&lt;br /&gt;
|}&lt;br /&gt;
&lt;br /&gt;
==中文翻译==&lt;br /&gt;
&lt;br /&gt;
'''T10. 最大食分（75分）'''&lt;br /&gt;
&lt;br /&gt;
最大食分定义为月球本影锥轴最接近地球中心的时刻。本问题以1919年5月29日日食为例探讨该现象的几何学，此次日食因首次通过观测验证广义相对论而具有重大历史意义。科学考察队之一在巴西索布拉尔市观测了此次日食。&lt;br /&gt;
&lt;br /&gt;
下表展示了最大食分时刻太阳和月球的球面坐标与笛卡尔坐标。坐标系为右手系，原点在地球中心，$x$轴正向指向格林尼治子午线，$z$轴正向指向北极点。下文中称此坐标系为**系统I**。&lt;br /&gt;
&lt;br /&gt;
'''球面坐标系：'''&lt;br /&gt;
{| class=&amp;quot;wikitable&amp;quot;&lt;br /&gt;
|-&lt;br /&gt;
! !! 太阳中心 !! 月球中心&lt;br /&gt;
|-&lt;br /&gt;
! 径向距离（$r$）&lt;br /&gt;
| $1.516 \times 10^{11}$ 米 || $3.589 \times 10^{8}$ 米&lt;br /&gt;
|-&lt;br /&gt;
! 极角（$\theta$）&lt;br /&gt;
| $68^\circ29'44.1''$ || $68^\circ47'41.6''$&lt;br /&gt;
|-&lt;br /&gt;
! 方位角（$\varphi$）&lt;br /&gt;
| $-1^h11^m28.2^s$ || $-1^h11^m22.9^s$&lt;br /&gt;
|}&lt;br /&gt;
&lt;br /&gt;
'''笛卡尔坐标系：'''&lt;br /&gt;
{| class=&amp;quot;wikitable&amp;quot;&lt;br /&gt;
|-&lt;br /&gt;
! !! 太阳中心 !! 月球中心&lt;br /&gt;
|-&lt;br /&gt;
! $x$&lt;br /&gt;
| $1.342 \times 10^{11}$ 米 || $3.185 \times 10^{8}$ 米&lt;br /&gt;
|-&lt;br /&gt;
! $y$&lt;br /&gt;
| $-4.327 \times 10^{10}$ 米 || $-1.025 \times 10^{8}$ 米&lt;br /&gt;
|-&lt;br /&gt;
! $z$&lt;br /&gt;
| $5.557 \times 10^{10}$ 米 || $1.298 \times 10^{8}$ 米&lt;br /&gt;
|}&lt;br /&gt;
&lt;br /&gt;
==官方解答==&lt;br /&gt;
&lt;br /&gt;
=== Part I: 地理坐标 ===&lt;br /&gt;
(a) 太阳和月球的赤纬：&lt;br /&gt;
$$$\delta = 90^\circ - \theta$$$&lt;br /&gt;
$$$\delta_\odot = 21^\circ30'15.9''$$$&lt;br /&gt;
$$$\delta_{Moon} = 21^\circ12'18.4''$$$&lt;br /&gt;
&lt;br /&gt;
(b) 太阳和月球的赤经（格林尼治恒星时为$5^h32^m35.5^s$）：&lt;br /&gt;
$$$\alpha = \varphi + LST_{Greenwich}$$$&lt;br /&gt;
$$$\alpha_\odot = 4^h21^m7.3^s$$$&lt;br /&gt;
$$$\alpha_{Moon} = 4^h21^m12.6^s$$$&lt;br /&gt;
&lt;br /&gt;
(c) 月球本影轴方向单位向量：&lt;br /&gt;
$$$\vec{u} = \left\langle -0.8855, 0.2855, -0.3666 \right\rangle$$$&lt;br /&gt;
&lt;br /&gt;
(d) 本影轴与地球表面交点坐标：&lt;br /&gt;
通过方程$$|\vec{M} + k\vec{u}| = R_\oplus$$解得：&lt;br /&gt;
$$$\phi = 4^\circ22'N$$$&lt;br /&gt;
$$$\lambda = 16^\circ42'W$$$&lt;br /&gt;
&lt;br /&gt;
=== Part II: 全食持续时间 ===&lt;br /&gt;
(e) 本影半径估算：&lt;br /&gt;
$$$r_{umbra} = 1.196 \times 10^5 \, \text{m}$$$&lt;br /&gt;
&lt;br /&gt;
(f) 地球自转线速度：&lt;br /&gt;
$$$v_{rot} = 463.7 \, \text{m/s}$$$&lt;br /&gt;
&lt;br /&gt;
(g) 月球轨道速度（忽略半长轴变化）：&lt;br /&gt;
$$$v_{Moon} = 1088 \, \text{m/s}$$$&lt;br /&gt;
&lt;br /&gt;
(h) 系统II中月球速度向量：&lt;br /&gt;
$$$\mathbf{v_{II}} = \begin{bmatrix} 1085 \, \text{m/s} \\ 81.25 \, \text{m/s} \\ 0 \end{bmatrix}$$$&lt;br /&gt;
&lt;br /&gt;
(i) 系统III中月球速度向量：&lt;br /&gt;
$$$\mathbf{v_{III}} = \begin{bmatrix} 1085 \, \text{m/s} \\ 77.76 \, \text{m/s} \\ -23.54 \, \text{m/s} \end{bmatrix}$$$&lt;br /&gt;
&lt;br /&gt;
(j) 本影中心地表移动速度：&lt;br /&gt;
$$$v_{umbra} = \sqrt{621.4^2 + 77.76^2} = 626.3 \, \text{m/s}$$$&lt;br /&gt;
&lt;br /&gt;
(k) 全食持续时间：&lt;br /&gt;
$$$\Delta t = \frac{2r_{umbra}}{v_{umbra}} = 6\,\text{分钟}\,21.4\,\text{秒}$$$&lt;br /&gt;
&lt;br /&gt;
[[分类:日月食]]&lt;br /&gt;
[[分类:球面三角]]&lt;br /&gt;
[[分类:由ai生成]]&lt;/div&gt;</summary>
		<author><name>Quan787</name></author>
		
	</entry>
	<entry>
		<id>https://www.astro-init.top/index.php?title=2024%E5%B9%B4IOAA%E7%90%86%E8%AE%BA%E7%AC%AC9%E9%A2%98-%E5%90%B8%E7%A7%AF%E7%89%A9%E7%90%86&amp;diff=2743</id>
		<title>2024年IOAA理论第9题-吸积物理</title>
		<link rel="alternate" type="text/html" href="https://www.astro-init.top/index.php?title=2024%E5%B9%B4IOAA%E7%90%86%E8%AE%BA%E7%AC%AC9%E9%A2%98-%E5%90%B8%E7%A7%AF%E7%89%A9%E7%90%86&amp;diff=2743"/>
		<updated>2025-03-08T10:55:14Z</updated>

		<summary type="html">&lt;p&gt;Quan787：&lt;/p&gt;
&lt;hr /&gt;
&lt;div&gt;{{由ai生成}}&lt;br /&gt;
==英文题目==&lt;br /&gt;
&lt;br /&gt;
'''T9. Physics of Accretion (35 points)'''&lt;br /&gt;
&lt;br /&gt;
The accretion of matter onto compact objects, such as neutron stars and black holes, is one of the most efficient ways to produce radiant energy in astrophysical systems. Consider an element of gas of mass $$\Delta m$$ in a stationary and geometrically thin disc of matter with a maximum radius of $$R_{max}$$ and minimum stable orbital radius of $$R_{min}$$ (with $$R_{min}/R_{max} \ll 1$$), in rotation around a compact object of mass $$M$$ and radius $$R$$.&lt;br /&gt;
&lt;br /&gt;
(a) (6 points) Assuming that an element of gas in the disc follows an approximately Keplerian circular orbit, find an expression for the total mechanical energy per unit mass $$\frac{\Delta E}{\Delta m}$$ released by this gas from when it starts orbiting at a radius $$R_{max}$$ until it reaches an orbital radius of $$r \ll R_{max}$$. This process occurs very slowly, transforming kinetic energy into internal energy of the gas disc through viscous dissipation. Note: Ignore the gravitational interaction between particles within the accretion disc and give your final answer in terms of $$G$$, $$M$$, and $$r$$.&lt;br /&gt;
&lt;br /&gt;
(b) (5 points) Considering that the disc receives mass at an average rate of $$\dot{M}$$, and assuming that all the mechanical energy lost is ultimately converted into radiation, find an expression for the total luminosity of the disc.&lt;br /&gt;
&lt;br /&gt;
(c) (8 points) Consider now the ring composed of all mass elements with radii between $$r$$ and $$r + \Delta r$$. In this scenario, find an expression for the luminosity generated by the disc over its small width $$\Delta r$$ at this radius; that is, find the expression for $$\frac{\Delta E}{\Delta t \Delta r}$$.&lt;br /&gt;
&lt;br /&gt;
(d) (10 points) Assuming that the gravitational energy released in this ring is locally emitted by the surface of the ring in the form of black-body radiation, find an expression for the surface temperature $$T$$ of the ring.&lt;br /&gt;
&lt;br /&gt;
(e) (3 points) Consider that the central object is a stellar black hole with a mass of $$3M_{\odot}$$ and a rate of accretion of $$\dot{M} = 10^{-9} M_{\odot} / \text{year}$$. Consider also that $$R_{min} = 3R_{sch}$$, where $$R_{sch}$$ is the Schwarzschild radius of the black hole. Determine the luminosity of the disc and the peak wavelength of emission of its innermost part. Ignore gravitational redshift effects and assume that the emission from the innermost part of the ring dominates the total emission.&lt;br /&gt;
&lt;br /&gt;
(f) (3 points) Now, considering another accretion system with $$\dot{M} = 1 \, M_{\odot}/$$ year and a peak emission wavelength of $$\lambda = 6 \times 10^{-8}$$ m, estimate the mass of this black hole.&lt;br /&gt;
&lt;br /&gt;
==中文翻译==&lt;br /&gt;
&lt;br /&gt;
'''T9. 吸积物理学（35分）'''&lt;br /&gt;
&lt;br /&gt;
物质向致密天体（如中子星和黑洞）的吸积是天体物理系统中产生辐射能最有效的方式之一。考虑一个质量为$$\Delta m$$的气体元素，其位于一个静止且几何学上薄的物质盘中，该盘的最大半径为$$R_{max}$$，最小稳定轨道半径为$$R_{min}$$（满足$$R_{min}/R_{max} \ll 1$$），围绕一个质量为$$M$$、半径为$$R$$的致密天体旋转。&lt;br /&gt;
&lt;br /&gt;
(a)（6分）假设盘中的气体元素遵循近似开普勒圆形轨道，求该气体从初始轨道半径$$R_{max}$$到达到轨道半径$$r \ll R_{max}$$的过程中，单位质量释放的总机械能$$\frac{\Delta E}{\Delta m}$$的表达式。此过程进行得非常缓慢，动能通过粘滞耗散转化为气体盘的内部能量。注意：忽略吸积盘内粒子间的引力相互作用，最终答案用$$G$$、$$M$$和$$r$$表示。&lt;br /&gt;
&lt;br /&gt;
(b)（5分）假设盘以平均速率$$\dot{M}$$接收质量，且所有损失的机械能最终转化为辐射，求盘的总光度表达式。&lt;br /&gt;
&lt;br /&gt;
(c)（8分）考虑由半径介于$$r$$和$$r + \Delta r$$之间的所有质量元素组成的环。在此情况下，求该半径处盘在微小宽度$$\Delta r$$上产生的光度表达式，即求$$\frac{\Delta E}{\Delta t \Delta r}$$的表达式。&lt;br /&gt;
&lt;br /&gt;
(d)（10分）假设此环中释放的引力能通过黑体辐射形式从环表面局部发射，求环的表面温度$$T$$的表达式。&lt;br /&gt;
&lt;br /&gt;
(e)（3分）设中心天体为质量$$3M_{\odot}$$的恒星黑洞，吸积率为$$\dot{M} = 10^{-9} M_{\odot} / \text{年}$$，且$$R_{min} = 3R_{sch}$$（其中$$R_{sch}$$为黑洞的史瓦西半径）。求盘的亮度及其最内层的峰值发射波长。忽略引力红移效应，并假设环最内层的发射主导总辐射。&lt;br /&gt;
&lt;br /&gt;
(f)（3分）考虑另一个吸积系统，其吸积率为$$\dot{M} = 1 \, M_{\odot}/$$年，峰值发射波长为$$\lambda = 6 \times 10^{-8}$$米，估算该黑洞的质量。&lt;br /&gt;
&lt;br /&gt;
==官方解答==&lt;br /&gt;
&lt;br /&gt;
'''解答：'''&lt;br /&gt;
&lt;br /&gt;
(a) 对于开普勒轨道：&lt;br /&gt;
&lt;br /&gt;
$$\frac{v_k^2}{r} = \frac{GM}{r^2} \Rightarrow v_k^2 = \frac{GM}{r}$$&lt;br /&gt;
&lt;br /&gt;
总机械能：&lt;br /&gt;
&lt;br /&gt;
$$E(r) = \frac{1}{2} \Delta m v_k^2 - \frac{GM \Delta m}{r} = -\frac{1}{2} \frac{GM \Delta m}{r}$$&lt;br /&gt;
&lt;br /&gt;
能量差：&lt;br /&gt;
&lt;br /&gt;
$$E(R_{max}) - E(r) = \frac{1}{2} GM \Delta m \left( \frac{1}{r} - \frac{1}{R_{max}} \right) \approx \frac{GM \Delta m}{2r}$$&lt;br /&gt;
&lt;br /&gt;
因此：&lt;br /&gt;
&lt;br /&gt;
$$\frac{\Delta E}{\Delta m} \approx \frac{GM}{2r}$$&lt;br /&gt;
&lt;br /&gt;
(b) 总光度：&lt;br /&gt;
&lt;br /&gt;
$$L_{Tot} = \frac{\Delta E_{Tot}}{\Delta t} = \frac{GM \dot{M}}{2R_{min}}$$&lt;br /&gt;
&lt;br /&gt;
(c) 考虑微小质量元素的能量变化：&lt;br /&gt;
&lt;br /&gt;
$$\frac{\Delta E}{\Delta m} \approx \frac{GM \Delta r}{2r^2}$$&lt;br /&gt;
&lt;br /&gt;
乘以质量流率：&lt;br /&gt;
&lt;br /&gt;
$$\frac{\Delta E}{\Delta t \Delta r} = \frac{GM \dot{M}}{2r^2}$$&lt;br /&gt;
&lt;br /&gt;
(d) 使用斯特藩-玻尔兹曼定律：&lt;br /&gt;
&lt;br /&gt;
$$4\pi r \Delta r \sigma T^4 = \frac{\Delta E}{\Delta t}$$&lt;br /&gt;
&lt;br /&gt;
代入得：&lt;br /&gt;
&lt;br /&gt;
$$T = \left( \frac{GM \dot{M}}{8\pi \sigma r^3} \right)^{1/4}$$&lt;br /&gt;
&lt;br /&gt;
(e) 史瓦西半径：&lt;br /&gt;
&lt;br /&gt;
$$R_{sch} = \frac{2GM}{c^2} \Rightarrow R_{min} = \frac{6GM}{c^2}$$&lt;br /&gt;
&lt;br /&gt;
总光度：&lt;br /&gt;
&lt;br /&gt;
$$L_{Tot} = \frac{\dot{M}c^2}{12} \approx 5 \times 10^{29} \, \text{W}$$&lt;br /&gt;
&lt;br /&gt;
表面温度：&lt;br /&gt;
&lt;br /&gt;
$$T = 5.5 \times 10^6 \, \text{K}$$&lt;br /&gt;
&lt;br /&gt;
峰值波长（维恩定律）：&lt;br /&gt;
&lt;br /&gt;
$$\lambda = \frac{b}{T} = 5 \times 10^{-10} \, \text{m}$$&lt;br /&gt;
&lt;br /&gt;
(f) 由维恩定律得温度：&lt;br /&gt;
&lt;br /&gt;
$$T = \frac{b}{\lambda} = 4.8 \times 10^4 \, \text{K}$$&lt;br /&gt;
&lt;br /&gt;
结合吸积公式估算质量：&lt;br /&gt;
&lt;br /&gt;
$$M \approx 1.3 \times 10^9 M_{\odot}$$&lt;br /&gt;
&lt;br /&gt;
[[分类:天体力学]]&lt;br /&gt;
[[分类:热学]]&lt;br /&gt;
[[分类:由ai生成]]&lt;/div&gt;</summary>
		<author><name>Quan787</name></author>
		
	</entry>
	<entry>
		<id>https://www.astro-init.top/index.php?title=2024%E5%B9%B4IOAA%E7%90%86%E8%AE%BA%E7%AC%AC9%E9%A2%98-%E5%90%B8%E7%A7%AF%E7%89%A9%E7%90%86&amp;diff=2742</id>
		<title>2024年IOAA理论第9题-吸积物理</title>
		<link rel="alternate" type="text/html" href="https://www.astro-init.top/index.php?title=2024%E5%B9%B4IOAA%E7%90%86%E8%AE%BA%E7%AC%AC9%E9%A2%98-%E5%90%B8%E7%A7%AF%E7%89%A9%E7%90%86&amp;diff=2742"/>
		<updated>2025-03-08T10:53:36Z</updated>

		<summary type="html">&lt;p&gt;Quan787：创建页面，内容为“{{由ai生成}} ==英文题目==  '''T9. Physics of Accretion (35 points)'''  The accretion of matter onto compact objects, such as neutron stars and black holes, is…”&lt;/p&gt;
&lt;hr /&gt;
&lt;div&gt;{{由ai生成}}&lt;br /&gt;
==英文题目==&lt;br /&gt;
&lt;br /&gt;
'''T9. Physics of Accretion (35 points)'''&lt;br /&gt;
&lt;br /&gt;
The accretion of matter onto compact objects, such as neutron stars and black holes, is one of the most efficient ways to produce radiant energy in astrophysical systems. Consider an element of gas of mass $$\Delta m$$ in a stationary and geometrically thin disc of matter with a maximum radius of $$R_{max}$$ and minimum stable orbital radius of $$R_{min}$$ (with $$R_{min}/R_{max} \ll 1$$), in rotation around a compact object of mass $$M$$ and radius $$R$$.&lt;br /&gt;
&lt;br /&gt;
(a) (6 points) Assuming that an element of gas in the disc follows an approximately Keplerian circular orbit, find an expression for the total mechanical energy per unit mass $$\frac{\Delta E}{\Delta m}$$ released by this gas from when it starts orbiting at a radius $$R_{max}$$ until it reaches an orbital radius of $$r \ll R_{max}$$. This process occurs very slowly, transforming kinetic energy into internal energy of the gas disc through viscous dissipation. Note: Ignore the gravitational interaction between particles within the accretion disc and give your final answer in terms of $$G$$, $$M$$, and $$r$$.&lt;br /&gt;
&lt;br /&gt;
(b) (5 points) Considering that the disc receives mass at an average rate of $$\dot{M}$$, and assuming that all the mechanical energy lost is ultimately converted into radiation, find an expression for the total luminosity of the disc.&lt;br /&gt;
&lt;br /&gt;
(c) (8 points) Consider now the ring composed of all mass elements with radii between $$r$$ and $$r + \Delta r$$. In this scenario, find an expression for the luminosity generated by the disc over its small width $$\Delta r$$ at this radius; that is, find the expression for $$\frac{\Delta E}{\Delta t \Delta r}$$.&lt;br /&gt;
&lt;br /&gt;
(d) (10 points) Assuming that the gravitational energy released in this ring is locally emitted by the surface of the ring in the form of black-body radiation, find an expression for the surface temperature $$T$$ of the ring.&lt;br /&gt;
&lt;br /&gt;
(e) (3 points) Consider that the central object is a stellar black hole with a mass of $$3M_{\odot}$$ and a rate of accretion of $$\dot{M} = 10^{-9} M_{\odot} / \text{year}$$. Consider also that $$R_{min} = 3R_{sch}$$, where $$R_{sch}$$ is the Schwarzschild radius of the black hole. Determine the luminosity of the disc and the peak wavelength of emission of its innermost part. Ignore gravitational redshift effects and assume that the emission from the innermost part of the ring dominates the total emission.&lt;br /&gt;
&lt;br /&gt;
(f) (3 points) Now, considering another accretion system with $$\dot{M} = 1 \, M_{\odot}/$$ year and a peak emission wavelength of $$\lambda = 6 \times 10^{-8}$$ m, estimate the mass of this black hole.&lt;br /&gt;
&lt;br /&gt;
==中文翻译==&lt;br /&gt;
&lt;br /&gt;
'''T9. 吸积物理学（35分）'''&lt;br /&gt;
&lt;br /&gt;
物质向致密天体（如中子星和黑洞）的吸积是天体物理系统中产生辐射能最有效的方式之一。考虑一个质量为$$\Delta m$$的气体元素，其位于一个静止且几何学上薄的物质盘中，该盘的最大半径为$$R_{max}$$，最小稳定轨道半径为$$R_{min}$$（满足$$R_{min}/R_{max} \ll 1$$），围绕一个质量为$$M$$、半径为$$R$$的致密天体旋转。&lt;br /&gt;
&lt;br /&gt;
(a)（6分）假设盘中的气体元素遵循近似开普勒圆形轨道，求该气体从初始轨道半径$$R_{max}$$到达到轨道半径$$r \ll R_{max}$$的过程中，单位质量释放的总机械能$$\frac{\Delta E}{\Delta m}$$的表达式。此过程进行得非常缓慢，动能通过粘滞耗散转化为气体盘的内部能量。注意：忽略吸积盘内粒子间的引力相互作用，最终答案用$$G$$、$$M$$和$$r$$表示。&lt;br /&gt;
&lt;br /&gt;
(b)（5分）假设盘以平均速率$$\dot{M}$$接收质量，且所有损失的机械能最终转化为辐射，求盘的总光度表达式。&lt;br /&gt;
&lt;br /&gt;
(c)（8分）考虑由半径介于$$r$$和$$r + \Delta r$$之间的所有质量元素组成的环。在此情况下，求该半径处盘在微小宽度$$\Delta r$$上产生的光度表达式，即求$$\frac{\Delta E}{\Delta t \Delta r}$$的表达式。&lt;br /&gt;
&lt;br /&gt;
(d)（10分）假设此环中释放的引力能通过黑体辐射形式从环表面局部发射，求环的表面温度$$T$$的表达式。&lt;br /&gt;
&lt;br /&gt;
(e)（3分）设中心天体为质量$$3M_{\odot}$$的恒星黑洞，吸积率为$$\dot{M} = 10^{-9} M_{\odot} / \text{年}$$，且$$R_{min} = 3R_{sch}$$（其中$$R_{sch}$$为黑洞的史瓦西半径）。求盘的亮度及其最内层的峰值发射波长。忽略引力红移效应，并假设环最内层的发射主导总辐射。&lt;br /&gt;
&lt;br /&gt;
(f)（3分）考虑另一个吸积系统，其吸积率为$$\dot{M} = 1 \, M_{\odot}/$$年，峰值发射波长为$$\lambda = 6 \times 10^{-8}$$米，估算该黑洞的质量。&lt;br /&gt;
&lt;br /&gt;
==官方解答==&lt;br /&gt;
&lt;br /&gt;
'''解答：'''&lt;br /&gt;
&lt;br /&gt;
(a) 对于开普勒轨道：&lt;br /&gt;
$$$\frac{v_k^2}{r} = \frac{GM}{r^2} \Rightarrow v_k^2 = \frac{GM}{r}$$$&lt;br /&gt;
&lt;br /&gt;
总机械能：&lt;br /&gt;
$$$E(r) = \frac{1}{2} \Delta m v_k^2 - \frac{GM \Delta m}{r} = -\frac{1}{2} \frac{GM \Delta m}{r}$$$&lt;br /&gt;
&lt;br /&gt;
能量差：&lt;br /&gt;
$$$E(R_{max}) - E(r) = \frac{1}{2} GM \Delta m \left( \frac{1}{r} - \frac{1}{R_{max}} \right) \approx \frac{GM \Delta m}{2r}$$$&lt;br /&gt;
&lt;br /&gt;
因此：&lt;br /&gt;
$$$\frac{\Delta E}{\Delta m} \approx \frac{GM}{2r}$$$&lt;br /&gt;
&lt;br /&gt;
(b) 总光度：&lt;br /&gt;
$$$L_{Tot} = \frac{\Delta E_{Tot}}{\Delta t} = \frac{GM \dot{M}}{2R_{min}}$$$&lt;br /&gt;
&lt;br /&gt;
(c) 考虑微小质量元素的能量变化：&lt;br /&gt;
$$$\frac{\Delta E}{\Delta m} \approx \frac{GM \Delta r}{2r^2}$$$&lt;br /&gt;
&lt;br /&gt;
乘以质量流率：&lt;br /&gt;
$$$\frac{\Delta E}{\Delta t \Delta r} = \frac{GM \dot{M}}{2r^2}$$$&lt;br /&gt;
&lt;br /&gt;
(d) 使用斯特藩-玻尔兹曼定律：&lt;br /&gt;
$$$4\pi r \Delta r \sigma T^4 = \frac{\Delta E}{\Delta t}$$$&lt;br /&gt;
&lt;br /&gt;
代入得：&lt;br /&gt;
$$$T = \left( \frac{GM \dot{M}}{8\pi \sigma r^3} \right)^{1/4}$$$&lt;br /&gt;
&lt;br /&gt;
(e) 史瓦西半径：&lt;br /&gt;
$$$R_{sch} = \frac{2GM}{c^2} \Rightarrow R_{min} = \frac{6GM}{c^2}$$$&lt;br /&gt;
&lt;br /&gt;
总光度：&lt;br /&gt;
$$$L_{Tot} = \frac{\dot{M}c^2}{12} \approx 5 \times 10^{29} \, \text{W}$$$&lt;br /&gt;
&lt;br /&gt;
表面温度：&lt;br /&gt;
$$$T = 5.5 \times 10^6 \, \text{K}$$$&lt;br /&gt;
&lt;br /&gt;
峰值波长（维恩定律）：&lt;br /&gt;
$$$\lambda = \frac{b}{T} = 5 \times 10^{-10} \, \text{m}$$$&lt;br /&gt;
&lt;br /&gt;
(f) 由维恩定律得温度：&lt;br /&gt;
$$$T = \frac{b}{\lambda} = 4.8 \times 10^4 \, \text{K}$$$&lt;br /&gt;
&lt;br /&gt;
结合吸积公式估算质量：&lt;br /&gt;
$$$M \approx 1.3 \times 10^9 M_{\odot}$$$&lt;br /&gt;
&lt;br /&gt;
[[分类:天体力学]]&lt;br /&gt;
[[分类:热学]]&lt;br /&gt;
[[分类:由ai生成]]&lt;/div&gt;</summary>
		<author><name>Quan787</name></author>
		
	</entry>
	<entry>
		<id>https://www.astro-init.top/index.php?title=2024%E5%B9%B4IOAA%E7%90%86%E8%AE%BA%E7%AC%AC8%E9%A2%98-%E5%8F%8C%E6%98%9F%E7%A1%AC%E5%8C%96&amp;diff=2741</id>
		<title>2024年IOAA理论第8题-双星硬化</title>
		<link rel="alternate" type="text/html" href="https://www.astro-init.top/index.php?title=2024%E5%B9%B4IOAA%E7%90%86%E8%AE%BA%E7%AC%AC8%E9%A2%98-%E5%8F%8C%E6%98%9F%E7%A1%AC%E5%8C%96&amp;diff=2741"/>
		<updated>2025-03-08T10:26:06Z</updated>

		<summary type="html">&lt;p&gt;Quan787：创建页面，内容为“{{由ai生成}} ==英文题目==  '''T8. Binary Hardening (25 points)'''  Consider a binary system of black holes, both of equal mass \(M\), separated by a distance…”&lt;/p&gt;
&lt;hr /&gt;
&lt;div&gt;{{由ai生成}}&lt;br /&gt;
==英文题目==&lt;br /&gt;
&lt;br /&gt;
'''T8. Binary Hardening (25 points)'''&lt;br /&gt;
&lt;br /&gt;
Consider a binary system of black holes, both of equal mass \(M\), separated by a distance \(a\), and revolving around their common centre of mass (CM) in circular orbits. This binary system moves against, and interacts with, a very large, uniform field of stars (each of mass \(m \ll M\)) with number density \(n\). Consider a star that approaches the system from infinity with speed \(v\) and impact parameter \(b\), in the reference frame of the CM (as shown in the figure below). Its closest approach distance to the CM is \(r_p \approx \frac{1}{2} a\). For tasks (a) and (c), you should make use of the fact that \(v^2 \ll \frac{GM}{a}\).&lt;br /&gt;
&lt;br /&gt;
(a) (5 points) Obtain an expression for \(b\), in terms of \(M\), \(a\), \(v\), and physical constants. In this task, assume that the star interacts with the binary as if its total mass was fixed at the CM.&lt;br /&gt;
&lt;br /&gt;
(b) (6 points) The star approaches the component with an initial speed negligible compared to the component's orbital speed, and both are moving directly towards each other. After interacting with the system, when the star is again far away from the black hole, we find that the direction of its velocity vector is reversed and the final speed is \(v_f\). Determine \(v_f\), in terms of \(M\), \(a\), and physical constants. Assume that linear momentum and mechanical energy are conserved during this interaction and that it takes place in a timescale much smaller than the binary's period. Recall that \(m \ll M\).&lt;br /&gt;
&lt;br /&gt;
(c) (14 points) Upon each encounter, part of the total energy of the binary is transferred to the kinetic energy of the star. Assume that the binary orbit remains circular. Knowing this, using your results from previous tasks, and taking into account only encounters with the stars within the specified range of impact parameters, show that the reciprocal of the binary's separation increases at a constant rate:&lt;br /&gt;
&lt;br /&gt;
$$&lt;br /&gt;
\frac{d}{dt} \left( \frac{1}{a} \right) = H \frac{G \rho}{v_0}&lt;br /&gt;
$$&lt;br /&gt;
&lt;br /&gt;
Here, \(\rho = nm\) is the mass density of the star field, and \(G\) is the universal gravitational constant. Find the dimensionless constant \(H\), which refers to hardening.&lt;br /&gt;
&lt;br /&gt;
==中文翻译==&lt;br /&gt;
&lt;br /&gt;
'''T8. 双星硬化（25分）'''&lt;br /&gt;
&lt;br /&gt;
考虑一个由两个质量均为\(M\)的黑洞组成的双星系统，间距为\(a\)，绕其共同质心（CM）做圆周运动。该系统在大量均匀分布的恒星场（每颗恒星质量\(m \ll M\)，数密度\(n\)）中运动并发生相互作用。假设一颗恒星从无穷远处以速度\(v\)和撞击参数\(b\)接近系统（参考系为CM），其最接近CM的距离为\(r_p \approx \frac{1}{2}a\)。在问题(a)和(c)中，需利用\(v^2 \ll \frac{GM}{a}\)的条件。&lt;br /&gt;
&lt;br /&gt;
(a) (5分) 推导撞击参数\(b\)的表达式，用\(M\)、\(a\)、\(v\)和物理常数表示。本题中假设恒星与双星系统的相互作用等效于其总质量固定在CM处。&lt;br /&gt;
&lt;br /&gt;
(b) (6分) 恒星以初速度（相对于黑洞轨道速度可忽略）直接朝向其中一个成员运动。相互作用后，当恒星远离黑洞时，其速度方向反转且最终速度为\(v_f\)。确定\(v_f\)（用\(M\)、\(a\)和物理常数表示）。假设相互作用过程中线动量与机械能守恒，且作用时间远小于双星轨道周期。&lt;br /&gt;
&lt;br /&gt;
(c) (14分) 每次相遇时，双星系统的部分能量转化为恒星的动能。假设双星轨道保持圆形，利用先前结果并仅考虑指定撞击参数范围内的恒星相遇，证明双星间距倒数的变化率为常数：&lt;br /&gt;
&lt;br /&gt;
$$&lt;br /&gt;
\frac{d}{dt} \left( \frac{1}{a} \right) = H \frac{G \rho}{v_0}&lt;br /&gt;
$$&lt;br /&gt;
&lt;br /&gt;
其中\(\rho = nm\)为恒星场质量密度，求无量纲常数\(H\)（硬化常数）。&lt;br /&gt;
&lt;br /&gt;
== 官方解答 ==&lt;br /&gt;
'''解答：'''&lt;br /&gt;
&lt;br /&gt;
(a) 通过机械能守恒和角动量守恒：&lt;br /&gt;
&lt;br /&gt;
$$&lt;br /&gt;
b = \frac{\sqrt{2GMa}}{v}&lt;br /&gt;
$$&lt;br /&gt;
&lt;br /&gt;
推导过程：  &lt;br /&gt;
最接近点速度\(v_p = \frac{b}{r_p}v\)，结合能量守恒方程：&lt;br /&gt;
&lt;br /&gt;
$$&lt;br /&gt;
-\frac{GM(2M)m}{a/2} + \frac{1}{2}m\left(\frac{b}{a/2}v\right)^2 = \frac{1}{2}mv^2&lt;br /&gt;
$$&lt;br /&gt;
&lt;br /&gt;
忽略\(v^2\)项后解得：&lt;br /&gt;
&lt;br /&gt;
$$&lt;br /&gt;
\boxed{b \approx \frac{\sqrt{2GMa}}{v}&lt;br /&gt;
$$&lt;br /&gt;
&lt;br /&gt;
&lt;br /&gt;
(b) 考虑黑洞轨道速度\(V = \sqrt{\frac{GM}{2a}}\)，通过动量与能量守恒：&lt;br /&gt;
&lt;br /&gt;
$$&lt;br /&gt;
v_f = 2V = \sqrt{\frac{2GM}{a}}&lt;br /&gt;
$$&lt;br /&gt;
&lt;br /&gt;
推导细节：  &lt;br /&gt;
在黑洞参考系中，恒星速度反向且大小不变，转换回CM系得：&lt;br /&gt;
&lt;br /&gt;
$$&lt;br /&gt;
\boxed{v_f = \sqrt{\frac{2GM}{a}} &lt;br /&gt;
$$&lt;br /&gt;
&lt;br /&gt;
&lt;br /&gt;
(c) 计算能量转移率与轨道收缩率：&lt;br /&gt;
&lt;br /&gt;
$$&lt;br /&gt;
H = 8\pi&lt;br /&gt;
$$&lt;br /&gt;
&lt;br /&gt;
关键步骤：  &lt;br /&gt;
1. 单次相遇能量损失：\(\Delta E = \frac{GMm}{a}\)  &lt;br /&gt;
&lt;br /&gt;
2. 相遇率计算：\(d\phi = 2\pi n b v db\)  &lt;br /&gt;
&lt;br /&gt;
3. 能量变化方程：\(\frac{dE}{dt} = -\frac{4\pi G^2 M^2 nm}{v_0}\)  &lt;br /&gt;
&lt;br /&gt;
4. 关联轨道能量\(E = -\frac{GM^2}{2a}\)的时间导数，最终得到：&lt;br /&gt;
&lt;br /&gt;
$$&lt;br /&gt;
\boxed{H = 8\pi}&lt;br /&gt;
$$&lt;br /&gt;
&lt;br /&gt;
[[分类:天体力学]]&lt;br /&gt;
[[分类:引力波]]&lt;br /&gt;
[[分类:由ai生成]]&lt;/div&gt;</summary>
		<author><name>Quan787</name></author>
		
	</entry>
	<entry>
		<id>https://www.astro-init.top/index.php?title=2024%E5%B9%B4IOAA%E7%90%86%E8%AE%BA%E7%AC%AC7%E9%A2%98-%E6%BC%82%E6%B5%81%E8%80%85&amp;diff=2740</id>
		<title>2024年IOAA理论第7题-漂流者</title>
		<link rel="alternate" type="text/html" href="https://www.astro-init.top/index.php?title=2024%E5%B9%B4IOAA%E7%90%86%E8%AE%BA%E7%AC%AC7%E9%A2%98-%E6%BC%82%E6%B5%81%E8%80%85&amp;diff=2740"/>
		<updated>2025-03-06T17:29:22Z</updated>

		<summary type="html">&lt;p&gt;Quan787：创建页面，内容为“{{由ai生成}} ==英文题目==  '''T7. Castaway (20 points)'''  After surviving a shipwreck and reaching a small island in the southern hemisphere, a sailor had to…”&lt;/p&gt;
&lt;hr /&gt;
&lt;div&gt;{{由ai生成}}&lt;br /&gt;
==英文题目==&lt;br /&gt;
&lt;br /&gt;
'''T7. Castaway (20 points)'''&lt;br /&gt;
&lt;br /&gt;
After surviving a shipwreck and reaching a small island in the southern hemisphere, a sailor had to estimate the island's latitude using the Sun.&lt;br /&gt;
&lt;br /&gt;
However, due to poor eyesight, the sailor couldn't see the night stars very well, so his best option was to rely on the Sun. He had no information about the date, but he realized the days were longer than the nights.&lt;br /&gt;
&lt;br /&gt;
(a) (7 points) The sailor noticed that on his first day on the island, the angle between the positions of sunrise and sunset on the horizon was \(120^\circ\). With this piece of information, determine the range of possible values for the latitude of the island. Neglect the daily motion of the Sun across the ecliptic.&lt;br /&gt;
&lt;br /&gt;
(b) (13 points) The angle between the positions of sunrise and sunset kept increasing daily. After 40 days, this angle was equal to \(163^\circ\). Estimate the latitude of the island. You may neglect the eccentricity of the Earth's orbit.&lt;br /&gt;
&lt;br /&gt;
==中文翻译==&lt;br /&gt;
&lt;br /&gt;
'''T7. 落难者（20分）'''&lt;br /&gt;
&lt;br /&gt;
一名水手在遭遇海难后到达南半球的一个小岛，需利用太阳估算该岛的纬度。&lt;br /&gt;
&lt;br /&gt;
由于视力不佳，水手无法清晰看到夜间的星星，因此只能依赖太阳。他没有关于日期的信息，但注意到白天长于夜晚。&lt;br /&gt;
&lt;br /&gt;
(a) (7分) 水手注意到在岛上第一天时，日出和日落位置在地平线上的夹角为\(120^\circ\)。利用这一信息，确定该岛纬度的可能取值范围。忽略太阳在黄道上的日常运动。&lt;br /&gt;
&lt;br /&gt;
(b) (13分) 日出与日落位置之间的夹角逐日增大。40天后，该夹角达到\(163^\circ\)。估算该岛的纬度。可忽略地球轨道的偏心率。&lt;br /&gt;
&lt;br /&gt;
== 官方解答 ==&lt;br /&gt;
&lt;br /&gt;
'''解答：'''&lt;br /&gt;
&lt;br /&gt;
(a) 第一步是推导日出时天体方位角的表达式：&lt;br /&gt;
&lt;br /&gt;
$$&lt;br /&gt;
\cos(90^\circ + \delta) = \cos(90^\circ - a) \cos(90^\circ + \phi) + \sin(90^\circ - a) \sin(90^\circ + \phi) \cos(180^\circ - A)&lt;br /&gt;
$$&lt;br /&gt;
&lt;br /&gt;
由于日出时高度角\(a = 0^\circ\)，简化为：&lt;br /&gt;
&lt;br /&gt;
$$&lt;br /&gt;
-\sin(\delta) = -\cos(\phi) \cos(A)&lt;br /&gt;
$$&lt;br /&gt;
&lt;br /&gt;
通过对称性分析，当太阳赤纬为\(-23.5^\circ\)时，纬度下限为：&lt;br /&gt;
&lt;br /&gt;
$$&lt;br /&gt;
\phi = -37.1^\circ&lt;br /&gt;
$$&lt;br /&gt;
&lt;br /&gt;
当太阳赤纬接近\(0^\circ\)时，纬度理论上接近南极。因此可能纬度范围为：&lt;br /&gt;
&lt;br /&gt;
$$&lt;br /&gt;
-90^\circ &amp;lt; \phi \leq -37.1^\circ&lt;br /&gt;
$$&lt;br /&gt;
&lt;br /&gt;
&lt;br /&gt;
(b) 结合赤纬变化与时间关系，建立方程：&lt;br /&gt;
&lt;br /&gt;
$$&lt;br /&gt;
\cos(\phi) = \frac{\sin(\delta_0)}{\cos(A_0)} = \frac{\sin(\delta_{40})}{\cos(A_{40})}&lt;br /&gt;
$$&lt;br /&gt;
&lt;br /&gt;
通过轨道运动角速度关系：&lt;br /&gt;
&lt;br /&gt;
$$&lt;br /&gt;
\theta_{40} = \theta_0 - \frac{40}{365.2564} \times 360^\circ = \theta_0 - 39.4^\circ&lt;br /&gt;
$$&lt;br /&gt;
&lt;br /&gt;
求解得：&lt;br /&gt;
&lt;br /&gt;
$$&lt;br /&gt;
\theta_0 = 53.1^\circ \quad \Rightarrow \quad \delta_0 = -18.6^\circ&lt;br /&gt;
$$&lt;br /&gt;
&lt;br /&gt;
最终纬度计算为：&lt;br /&gt;
&lt;br /&gt;
$$&lt;br /&gt;
\phi = -50.4^\circ&lt;br /&gt;
$$&lt;br /&gt;
&lt;br /&gt;
[[分类:球面三角]]&lt;br /&gt;
[[分类:视运动]]&lt;br /&gt;
[[分类:由ai生成]]&lt;/div&gt;</summary>
		<author><name>Quan787</name></author>
		
	</entry>
	<entry>
		<id>https://www.astro-init.top/index.php?title=2024%E5%B9%B4IOAA%E7%90%86%E8%AE%BA%E7%AC%AC6%E9%A2%98-%E6%98%9F%E5%9B%A2%E6%91%84%E5%BD%B1&amp;diff=2739</id>
		<title>2024年IOAA理论第6题-星团摄影</title>
		<link rel="alternate" type="text/html" href="https://www.astro-init.top/index.php?title=2024%E5%B9%B4IOAA%E7%90%86%E8%AE%BA%E7%AC%AC6%E9%A2%98-%E6%98%9F%E5%9B%A2%E6%91%84%E5%BD%B1&amp;diff=2739"/>
		<updated>2025-03-06T17:17:27Z</updated>

		<summary type="html">&lt;p&gt;Quan787：&lt;/p&gt;
&lt;hr /&gt;
&lt;div&gt;{{由ai生成}}&lt;br /&gt;
==英文题目==&lt;br /&gt;
&lt;br /&gt;
'''T6. Cluster Photography (20 points)'''&lt;br /&gt;
&lt;br /&gt;
An astronomer takes pictures, in the $$V$$-band, of a faint celestial target, from a place with no light pollution. The selected target is the globular cluster Palomar 4, which has an angular diameter of $$\theta = 72.0''$$ and a uniform surface brightness in the $$V$$-band of $$m_V = 20.6\ \text{mag/arcsec}^2$$. The observation equipment consists of one reflector telescope, with diameter $$D = 305\ \text{mm}$$ and $$f/5$$, and a prime focus CCD with quantum efficiency $$\eta = 80\%$$ and square pixels with size $$\ell = 3.80\ \mu\text{m}$$.&lt;br /&gt;
&lt;br /&gt;
Given data:&lt;br /&gt;
&lt;br /&gt;
- $$V$$-band central wavelength: $$\lambda_V = 550\ \text{nm}$$&lt;br /&gt;
&lt;br /&gt;
- $$V$$-band bandwidth: $$\Delta\lambda_V = 88.0\ \text{nm}$$&lt;br /&gt;
&lt;br /&gt;
- Photon flux for a 0-magnitude object in the $$V$$-band: 10000 counts/mm/cm$$^2$$/s&lt;br /&gt;
&lt;br /&gt;
(a) (3 points) Calculate the plate scale (the angle of sky projected per unit length of the sensor) of the observation equipment in arcmin/mm.&lt;br /&gt;
&lt;br /&gt;
(b) (4 points) Estimate the number of pixels, $$n_p$$, covered by the cluster image on the CCD.&lt;br /&gt;
&lt;br /&gt;
(c) (13 points) With an exposure time of $$t = 15\ \text{seconds}$$, the astronomer obtains a signal-to-noise ratio of $$S/N = 225$$. Compute the brightness of the sky at the observation site, knowing that the CCD has a readout noise (standard deviation) of 5 counts per pixel and dark noise of 6 counts per pixel per minute. Give your answer in mag/arcsec$$^2$$. You may find useful: $$\sigma_{RON}^2 = n_p \cdot 1 \cdot RON^2$$ and $$\sigma_{DN}^2 = n_p \cdot DN \cdot t$$.&lt;br /&gt;
&lt;br /&gt;
==中文翻译==&lt;br /&gt;
&lt;br /&gt;
'''T6. 星团摄影（20分）'''&lt;br /&gt;
&lt;br /&gt;
一位天文学家在无光污染地区使用$$V$$波段对暗淡天体目标进行拍摄。目标为球状星团帕洛玛4，其角直径为$$\theta = 72.0''$$，$$V$$波段表面亮度均匀，为$$m_V = 20.6\ \text{mag/arcsec}^2$$。观测设备包括一台口径$$D = 305\ \text{毫米}$$、焦比$$f/5$$的反射望远镜，以及量子效率$$\eta = 80\%$$、像元尺寸$$\ell = 3.80\ \mu\text{m}$$的方像素CCD。&lt;br /&gt;
&lt;br /&gt;
给定数据：&lt;br /&gt;
&lt;br /&gt;
- $$V$$波段中心波长：$$\lambda_V = 550\ \text{纳米}$$&lt;br /&gt;
&lt;br /&gt;
- $$V$$波段带宽：$$\Delta\lambda_V = 88.0\ \text{纳米}$$&lt;br /&gt;
&lt;br /&gt;
- $$V$$波段0等天体的光子流量：10000 计数/毫米/平方厘米$$^2$$/秒&lt;br /&gt;
&lt;br /&gt;
(a) (3分) 计算观测设备的底片比例（传感器单位长度对应的天空角度），单位为角分/毫米。&lt;br /&gt;
&lt;br /&gt;
(b) (4分) 估算星团图像在CCD上覆盖的像素数$$n_p$$。&lt;br /&gt;
&lt;br /&gt;
(c) (13分) 在曝光时间$$t = 15\ \text{秒}$$下，信噪比$$S/N = 225$$。已知CCD的读出噪声（标准差）为5计数/像素，暗噪声为6计数/像素/分钟，计算观测地点天空亮度（以mag/arcsec$$^2$$为单位）。可用公式：$$\sigma_{RON}^2 = n_p \cdot 1 \cdot RON^2$$ 和 $$\sigma_{DN}^2 = n_p \cdot DN \cdot t$$。&lt;br /&gt;
&lt;br /&gt;
== 官方解答 ==&lt;br /&gt;
&lt;br /&gt;
(a) **解答：**  &lt;br /&gt;
&lt;br /&gt;
底片比例计算公式为：&lt;br /&gt;
&lt;br /&gt;
$$\text{Plate Scale} = \frac{1\ \text{mm}}{f} \cdot \frac{180 \times 60}{\pi}\ \text{arcmin/mm}$$&lt;br /&gt;
&lt;br /&gt;
其中焦距$$f = D \times f/\text{ratio} = 305\ \text{mm} \times 5 = 1525\ \text{mm}$$。代入得：&lt;br /&gt;
&lt;br /&gt;
$$\text{Plate Scale} = \frac{1}{1525} \times \frac{10800}{\pi} \approx 2.25\ \text{arcmin/mm}.$$&lt;br /&gt;
&lt;br /&gt;
(b) **解答：**  &lt;br /&gt;
&lt;br /&gt;
星团直径在CCD上的投影长度为：&lt;br /&gt;
&lt;br /&gt;
$$d_{\text{GC}} = \theta \times \text{Plate Scale}^{-1} = 72.0'' \times \frac{1\ \text{mm}}{2.25\ \text{arcmin}} \times \frac{1\ \text{arcmin}}{60''} \approx 0.532\ \text{mm}.$$&lt;br /&gt;
&lt;br /&gt;
覆盖像素数为：&lt;br /&gt;
&lt;br /&gt;
$$n_p = \frac{\pi}{4} \left( \frac{d_{\text{GC}}}{\ell} \right)^2 \approx \frac{\pi}{4} \left( \frac{0.532\ \text{mm}}{3.80 \times 10^{-3}\ \text{mm}} \right)^2 \approx 15,400.$$&lt;br /&gt;
&lt;br /&gt;
(c) **解答：**  &lt;br /&gt;
总信号$$N_{\text{GC}}$$计算如下：&lt;br /&gt;
&lt;br /&gt;
$$N_{\text{GC}} = \eta \cdot \Phi_0 \cdot 10^{-0.4m_V} \cdot \frac{\pi D^2}{4} \cdot \Delta\lambda_V \cdot t \cdot \Omega_{\text{GC}},$$&lt;br /&gt;
&lt;br /&gt;
其中$$\Omega_{\text{GC}} = \pi (\theta/2)^2 = 4071.5\ \text{arcsec}^2$$。代入数据得：&lt;br /&gt;
&lt;br /&gt;
$$N_{\text{GC}} \approx 180,540\ \text{counts}.$$&lt;br /&gt;
&lt;br /&gt;
噪声项为：&lt;br /&gt;
&lt;br /&gt;
$$\sigma_{\text{total}}^2 = N_{\text{GC}} + N_{\text{sky}} + n_p \cdot RON^2 + n_p \cdot DN \cdot t.$$&lt;br /&gt;
&lt;br /&gt;
由$$S/N = 225$$得：&lt;br /&gt;
&lt;br /&gt;
$$N_{\text{sky}} = \left( \frac{180540}{225} \right)^2 - 180540 - 385000 - 23100 \approx 55,250\ \text{counts}.$$&lt;br /&gt;
&lt;br /&gt;
天空表面亮度计算为：&lt;br /&gt;
&lt;br /&gt;
$$m_{\text{sky}} = m_V + 2.5 \log_{10} \left( \frac{N_{\text{sky}}}{N_{\text{GC}}} \right) \approx 21.9\ \text{mag/arcsec}^2.$$&lt;br /&gt;
&lt;br /&gt;
[[分类:望远镜与天文摄影]]&lt;br /&gt;
[[分类:星等]]&lt;br /&gt;
[[分类:由ai生成]]&lt;/div&gt;</summary>
		<author><name>Quan787</name></author>
		
	</entry>
	<entry>
		<id>https://www.astro-init.top/index.php?title=2024%E5%B9%B4IOAA%E7%90%86%E8%AE%BA%E7%AC%AC5%E9%A2%98-%E5%AE%87%E5%AE%99%E5%BE%AE%E6%B3%A2%E8%83%8C%E6%99%AF&amp;diff=2738</id>
		<title>2024年IOAA理论第5题-宇宙微波背景</title>
		<link rel="alternate" type="text/html" href="https://www.astro-init.top/index.php?title=2024%E5%B9%B4IOAA%E7%90%86%E8%AE%BA%E7%AC%AC5%E9%A2%98-%E5%AE%87%E5%AE%99%E5%BE%AE%E6%B3%A2%E8%83%8C%E6%99%AF&amp;diff=2738"/>
		<updated>2025-03-06T17:11:26Z</updated>

		<summary type="html">&lt;p&gt;Quan787：&lt;/p&gt;
&lt;hr /&gt;
&lt;div&gt;{{由ai生成}}&lt;br /&gt;
==英文题目==&lt;br /&gt;
&lt;br /&gt;
'''T5. CMB (10 points)'''&lt;br /&gt;
&lt;br /&gt;
The Cosmic Microwave Background (CMB) is radiation emitted during the early Universe. It is reasonably homogeneous and isotropic, and well described by a black-body radiation spectrum. Its emission spectrum today has a peak at a temperature of approximately $$T_{\text{today}} \sim 3\ \text{K}$$, as measured by the COBE satellite FIRAS instrument.&lt;br /&gt;
&lt;br /&gt;
(a) (3 points) What is the redshift ($$z$$) at which the CMB spectrum has a peak at the infrared wavelength of $$\lambda_{\text{IR}} \sim 0.1\ \text{mm}$$?&lt;br /&gt;
&lt;br /&gt;
(b) (7 points) By assuming a spatially flat, matter-dominated Universe, what is the age of the Universe corresponding to the redshift of the previous part?&lt;br /&gt;
&lt;br /&gt;
==中文翻译==&lt;br /&gt;
&lt;br /&gt;
'''T5. 宇宙微波背景（10分）'''&lt;br /&gt;
&lt;br /&gt;
宇宙微波背景（CMB）是早期宇宙发出的辐射。它具有较好的均匀性和各向同性，并能用黑体辐射谱很好地描述。根据COBE卫星FIRAS仪器的测量，其当前发射谱的峰值温度约为$$T_{\text{today}} \sim 3\ \text{K}$$。&lt;br /&gt;
&lt;br /&gt;
(a) (3分) 当CMB光谱的红外波段峰值波长为$$\lambda_{\text{IR}} \sim 0.1\ \text{毫米}$$时，对应的红移$$z$$是多少？&lt;br /&gt;
&lt;br /&gt;
(b) (7分) 假设宇宙是空间平坦且物质主导的，计算对应上述红移时宇宙的年龄。&lt;br /&gt;
&lt;br /&gt;
== 官方解答 ==&lt;br /&gt;
&lt;br /&gt;
(a) 解答：&lt;br /&gt;
&lt;br /&gt;
根据维恩位移定律：&lt;br /&gt;
&lt;br /&gt;
$$\lambda_{\text{today}} \cdot T_{\text{today}} = b$$&lt;br /&gt;
&lt;br /&gt;
其中$$b$$为维恩位移常数。已知当前CMB的峰值温度$$T_{\text{today}} \approx 3\ \text{K}$$，对应的波长为：&lt;br /&gt;
&lt;br /&gt;
$$\lambda_{\text{today}} \approx \frac{b}{T_{\text{today}}} \approx 1\ \text{毫米}$$&lt;br /&gt;
&lt;br /&gt;
当该波长在红移$$z$$下对应于红外波长$$0.1\ \text{毫米}$$时：&lt;br /&gt;
&lt;br /&gt;
$$1 + z = \frac{\lambda_{\text{today}}}{\lambda_{\text{IR}}} = \frac{1\ \text{毫米}}{0.1\ \text{毫米}} = 10$$&lt;br /&gt;
&lt;br /&gt;
因此，红移为：&lt;br /&gt;
&lt;br /&gt;
$$\boxed{z = 9}$$&lt;br /&gt;
&lt;br /&gt;
(b) 解答：&lt;br /&gt;
&lt;br /&gt;
对于物质主导的平坦宇宙，尺度因子$$a$$与红移的关系为：&lt;br /&gt;
&lt;br /&gt;
$$a = \frac{1}{1+z} = 0.1$$&lt;br /&gt;
&lt;br /&gt;
哈勃参数满足：&lt;br /&gt;
&lt;br /&gt;
$$H^2 = H_0^2 \left( \frac{\Omega_m}{a^3} \right)$$&lt;br /&gt;
&lt;br /&gt;
在纯物质主导的假设下（$$\Omega_m = 1$$），宇宙年龄的积分表达式为：&lt;br /&gt;
&lt;br /&gt;
$$t = \frac{1}{H_0} \int_0^{0.1} \frac{\sqrt{a}}{1} da = \frac{1}{H_0} \cdot \frac{2}{3} a^{3/2} \bigg|_0^{0.1}$$&lt;br /&gt;
&lt;br /&gt;
代入哈勃常数$$H_0 = 70\ \text{km/s/Mpc}$$，并转换单位后计算得：&lt;br /&gt;
&lt;br /&gt;
$$t \approx \frac{2 \times (0.1)^{3/2}}{3 \times 70} \times \frac{3.086 \times 10^{22}\ \text{m/Mpc}}{1000\ \text{m/s}}$$&lt;br /&gt;
&lt;br /&gt;
结果为：&lt;br /&gt;
&lt;br /&gt;
$$\boxed{t \approx 0.3\ \text{Gyr}}$$&lt;br /&gt;
&lt;br /&gt;
[[分类:宇宙学]]&lt;br /&gt;
[[分类:热学]]&lt;br /&gt;
[[分类:由ai生成]]&lt;/div&gt;</summary>
		<author><name>Quan787</name></author>
		
	</entry>
	<entry>
		<id>https://www.astro-init.top/index.php?title=2024%E5%B9%B4IOAA%E7%90%86%E8%AE%BA%E7%AC%AC4%E9%A2%98-%E7%99%BD%E7%9F%AE%E6%98%9F&amp;diff=2737</id>
		<title>2024年IOAA理论第4题-白矮星</title>
		<link rel="alternate" type="text/html" href="https://www.astro-init.top/index.php?title=2024%E5%B9%B4IOAA%E7%90%86%E8%AE%BA%E7%AC%AC4%E9%A2%98-%E7%99%BD%E7%9F%AE%E6%98%9F&amp;diff=2737"/>
		<updated>2025-03-06T17:07:52Z</updated>

		<summary type="html">&lt;p&gt;Quan787：&lt;/p&gt;
&lt;hr /&gt;
&lt;div&gt;{{由ai生成}}&lt;br /&gt;
==英文题目==&lt;br /&gt;
&lt;br /&gt;
'''T4. White Dwarf (10 points)'''&lt;br /&gt;
&lt;br /&gt;
The structure of a white dwarf is sustained against gravitational collapse by the pressure of degenerate electrons, a phenomenon explained by quantum physics and related to the Pauli Exclusion Principle for electrons. The equation of state of a gas made of non-relativistic degenerate electrons is the following:&lt;br /&gt;
&lt;br /&gt;
$$P = \left( \frac{3}{8\pi} \right)^{2/3} \frac{h^2}{5m_e} n_e^{5/3},$$&lt;br /&gt;
&lt;br /&gt;
where $$n_e$$ is the number of electrons per unit volume, which can be expressed in terms of the mass density $$\rho$$ using the dimensionless factor $$\mu_e$$, the number of nucleons (protons and neutrons) per unit electron. Also consider that the central pressure can be described by this equation of state.&lt;br /&gt;
&lt;br /&gt;
In the condition of hydrostatic equilibrium, the pressure and gravitational forces balance each other at any distance $$r$$ from the centre of the star. This condition can be expressed by:&lt;br /&gt;
&lt;br /&gt;
$$\frac{dP}{dr} = -\frac{GM(r)\rho(r)}{r^2},$$&lt;br /&gt;
&lt;br /&gt;
where $$M(r)$$ is the mass contained in the sphere of radius $$r$$, and $$\rho(r)$$ is the mass density of the star at a radius $$r$$.&lt;br /&gt;
&lt;br /&gt;
Assume that $$m_p = m_n$$, the density of a white dwarf is roughly uniform, and the following approximation is valid at the surface of the star:&lt;br /&gt;
&lt;br /&gt;
$$\frac{dP}{dr} \bigg|_{r=R} \approx -\frac{P_c}{R},$$&lt;br /&gt;
&lt;br /&gt;
where $$P_c$$ is the pressure at the centre of the star, and $$R$$ the star radius.&lt;br /&gt;
&lt;br /&gt;
(a) (6 points) The relationship between the mass $$M$$ and the radius $$R$$ of a white dwarf can be written in the form:&lt;br /&gt;
&lt;br /&gt;
$$R = a \cdot M^b$$&lt;br /&gt;
&lt;br /&gt;
Find the exponent $$b$$ and determine the coefficient $$a$$ in terms of physical constants and $$\mu_e$$.&lt;br /&gt;
&lt;br /&gt;
(b) (4 points) Using the relationship found in the previous part, estimate the radius of a white dwarf made of fully ionised carbon ($$^{12}C$$) with a mass of $$M = 1.0M_\odot$$.&lt;br /&gt;
&lt;br /&gt;
==中文翻译==&lt;br /&gt;
&lt;br /&gt;
'''T4. 白矮星（10分）'''&lt;br /&gt;
&lt;br /&gt;
白矮星的结构由简并电子的压力维持以抵抗引力坍缩，这一现象可由量子物理和电子泡利不相容原理解释。由非相对论性简并电子组成的气体的状态方程如下：&lt;br /&gt;
&lt;br /&gt;
$$P = \left( \frac{3}{8\pi} \right)^{2/3} \frac{h^2}{5m_e} n_e^{5/3},$$&lt;br /&gt;
&lt;br /&gt;
其中$$n_e$$为单位体积的电子数，可通过质量密度$$\rho$$和无量纲因子$$\mu_e$$（每个电子对应的核子（质子和中子）数）表示。同时假设中心压力可用此状态方程描述。&lt;br /&gt;
&lt;br /&gt;
在流体静力平衡条件下，压力与引力在距离星体中心$$r$$处的任意位置相互平衡。该条件可表示为：&lt;br /&gt;
&lt;br /&gt;
$$\frac{dP}{dr} = -\frac{GM(r)\rho(r)}{r^2},$$&lt;br /&gt;
&lt;br /&gt;
其中$$M(r)$$为半径$$r$$的球体内包含的质量，$$\rho(r)$$为星体在半径$$r$$处的质量密度。&lt;br /&gt;
&lt;br /&gt;
假设$$m_p = m_n$$，白矮星的密度大致均匀，且在星体表面满足以下近似：&lt;br /&gt;
&lt;br /&gt;
$$\frac{dP}{dr} \bigg|_{r=R} \approx -\frac{P_c}{R},$$&lt;br /&gt;
&lt;br /&gt;
其中$$P_c$$为星体中心压力，$$R$$为星体半径。&lt;br /&gt;
&lt;br /&gt;
(a) (6分) 白矮星质量$$M$$与半径$$R$$的关系可写为：&lt;br /&gt;
&lt;br /&gt;
$$R = a \cdot M^b$$&lt;br /&gt;
&lt;br /&gt;
求指数$$b$$，并用物理常数和$$\mu_e$$确定系数$$a$$。&lt;br /&gt;
&lt;br /&gt;
(b) (4分) 利用上一部分得到的关系，估算由完全电离的碳（$$^{12}C$$）构成、质量为$$M = 1.0M_\odot$$的白矮星的半径。&lt;br /&gt;
&lt;br /&gt;
== 官方解答 ==&lt;br /&gt;
&lt;br /&gt;
(a) **解答：**  &lt;br /&gt;
在$$r = R$$处，利用题目中提供的近似条件和密度表达式$$\rho = 3M/(4\pi R^3)$$：&lt;br /&gt;
&lt;br /&gt;
$$-\frac{P_c}{R} = -\frac{GM(3M/(4\pi R^3))}{R^2}$$&lt;br /&gt;
&lt;br /&gt;
$$P_c = \frac{3GM^2}{4\pi R^4}$$&lt;br /&gt;
&lt;br /&gt;
电子密度$$n_e$$与质量密度的关系为：&lt;br /&gt;
&lt;br /&gt;
$$\rho = \mu_e m_p n_e$$&lt;br /&gt;
&lt;br /&gt;
使用状态方程：&lt;br /&gt;
&lt;br /&gt;
$$P_c = \left( \frac{3}{8\pi} \right)^{2/3} \frac{h^2}{5m_e} \left( \frac{3M}{4\pi R^3 \mu_e m_p} \right)^{5/3}$$&lt;br /&gt;
&lt;br /&gt;
联立得：&lt;br /&gt;
&lt;br /&gt;
$$\frac{3GM^2}{4\pi R^4} = \left( \frac{3}{8\pi} \right)^{2/3} \frac{h^2}{5m_e} \left( \frac{3}{4\pi \mu_e m_p} \right)^{5/3} \frac{M^{5/3}}{R^5}$$&lt;br /&gt;
&lt;br /&gt;
解得：&lt;br /&gt;
&lt;br /&gt;
$$R = \left( \frac{4\pi}{3} \right) \left( \frac{3}{8\pi} \right)^{2/3} \frac{h^2}{5Gm_e} \left( \frac{3}{4\pi \mu_e m_p} \right)^{5/3} M^{-1/3}$$&lt;br /&gt;
&lt;br /&gt;
因此，&lt;br /&gt;
&lt;br /&gt;
$$b = -\frac{1}{3}, \quad a = \left( \frac{4\pi}{3} \right) \left( \frac{3}{8\pi} \right)^{2/3} \frac{h^2}{5Gm_e} \left( \frac{3}{4\pi \mu_e m_p} \right)^{5/3}.$$&lt;br /&gt;
&lt;br /&gt;
(b) **解答：**  &lt;br /&gt;
对于完全电离的碳（$$^{12}C$$），每个电子对应2个核子，即$$\mu_e = 2$$。代入上述表达式：&lt;br /&gt;
&lt;br /&gt;
$$R \approx \frac{1.866 \times 10^{-2} \times \left(6.626 \times 10^{-34}\right)^2}{6.67 \times 10^{-11} \times 9.11 \times 10^{-31} \times \left(2 \times 1.67 \times 10^{-27}\right)^{5/3} \times \left(1.988 \times 10^{30}\right)^{1/3}}$$&lt;br /&gt;
&lt;br /&gt;
计算结果为：&lt;br /&gt;
&lt;br /&gt;
$$R \approx 1.44 \times 10^6 \, \text{m}.$$&lt;br /&gt;
&lt;br /&gt;
[[分类:恒星结构]]&lt;br /&gt;
[[分类:量子物理]]&lt;br /&gt;
[[分类:由ai生成]]&lt;/div&gt;</summary>
		<author><name>Quan787</name></author>
		
	</entry>
	<entry>
		<id>https://www.astro-init.top/index.php?title=2024%E5%B9%B4IOAA%E7%90%86%E8%AE%BA%E7%AC%AC6%E9%A2%98-%E6%98%9F%E5%9B%A2%E6%91%84%E5%BD%B1&amp;diff=2736</id>
		<title>2024年IOAA理论第6题-星团摄影</title>
		<link rel="alternate" type="text/html" href="https://www.astro-init.top/index.php?title=2024%E5%B9%B4IOAA%E7%90%86%E8%AE%BA%E7%AC%AC6%E9%A2%98-%E6%98%9F%E5%9B%A2%E6%91%84%E5%BD%B1&amp;diff=2736"/>
		<updated>2025-03-06T16:56:39Z</updated>

		<summary type="html">&lt;p&gt;Quan787：&lt;/p&gt;
&lt;hr /&gt;
&lt;div&gt;{{由ai生成}}&lt;br /&gt;
==英文题目==&lt;br /&gt;
&lt;br /&gt;
'''T6. Cluster Photography (20 points)'''&lt;br /&gt;
&lt;br /&gt;
An astronomer images Palomar 4 cluster (\(\theta = 72.0''\), \(m_V = 20.6 \, \text{mag/arcsec}^2\)) using a 305mm f/5 telescope and CCD (\(\eta = 80\%\), pixel size \(3.80\mu m\)).&lt;br /&gt;
&lt;br /&gt;
Given:&lt;br /&gt;
&lt;br /&gt;
- \(V\)-band: \(\lambda_V = 550nm\), \(\Delta\lambda_V = 88.0nm\)&lt;br /&gt;
&lt;br /&gt;
- 0-mag flux: 10000 counts/mm/cm\(^2\)/s&lt;br /&gt;
&lt;br /&gt;
- CCD noise: RON=5/pixel, DN=6/pixel/min&lt;br /&gt;
&lt;br /&gt;
(a) (3 points) Calculate plate scale (arcmin/mm)&lt;br /&gt;
&lt;br /&gt;
(b) (4 points) Estimate number of pixels (\(n_p\)) covered by the cluster&lt;br /&gt;
&lt;br /&gt;
(c) (13 points) Derive sky brightness (mag/arcsec\(^2\)) given S/N=225 with 15s exposure&lt;br /&gt;
&lt;br /&gt;
&lt;br /&gt;
==中文翻译==&lt;br /&gt;
&lt;br /&gt;
'''T6. 星团摄影（20分）'''&lt;br /&gt;
&lt;br /&gt;
使用305mm f/5望远镜和CCD（量子效率80%，像素尺寸3.80μm）拍摄帕洛玛4星团（角直径72.0''，V波段面亮度20.6星等/平方角秒）。&lt;br /&gt;
&lt;br /&gt;
已知：&lt;br /&gt;
- V波段中心波长550nm，带宽88.0nm&lt;br /&gt;
&lt;br /&gt;
- 0等星流量：10000计数/毫米/平方厘米/秒&lt;br /&gt;
&lt;br /&gt;
- CCD噪声：读出噪声5计数/像素，暗电流6计数/像素/分钟&lt;br /&gt;
&lt;br /&gt;
(a) (3分) 计算板尺度（角分/毫米）&lt;br /&gt;
&lt;br /&gt;
(b) (4分) 估算星团覆盖像素数&lt;br /&gt;
&lt;br /&gt;
(c) (13分) 已知曝光15秒时信噪比225，求天空亮度（星等/平方角秒）&lt;br /&gt;
&lt;br /&gt;
&lt;br /&gt;
== 官方解答 ==&lt;br /&gt;
&lt;br /&gt;
(a) 焦距\(f = 305 \times 5 = 1525mm\)，板尺度：&lt;br /&gt;
&lt;br /&gt;
$$\text{PS} = \frac{206265}{1525} \approx 135.3 \, \text{角秒/mm} = 2.26 \, \text{角分/mm}$$&lt;br /&gt;
&lt;br /&gt;
(b) 星团直径：&lt;br /&gt;
&lt;br /&gt;
$$d = 72/135.3 \approx 0.532mm \Rightarrow n_p \approx 15400 \, \text{像素}$$&lt;br /&gt;
&lt;br /&gt;
(c) 通过噪声方程反推：&lt;br /&gt;
&lt;br /&gt;
$$\sigma_{\text{总}}^2 = N_{\text{星团}} + N_{\text{天空}} + 385000 + 23100$$&lt;br /&gt;
&lt;br /&gt;
得天空亮度：&lt;br /&gt;
&lt;br /&gt;
$$m_{\text{天空}} = 21.9 \, \text{mag/arcsec}^2$$&lt;br /&gt;
&lt;br /&gt;
[[分类:望远镜与天文摄影]]&lt;br /&gt;
[[分类:由ai生成]]&lt;/div&gt;</summary>
		<author><name>Quan787</name></author>
		
	</entry>
	<entry>
		<id>https://www.astro-init.top/index.php?title=2024%E5%B9%B4IOAA%E7%90%86%E8%AE%BA%E7%AC%AC6%E9%A2%98-%E6%98%9F%E5%9B%A2%E6%91%84%E5%BD%B1&amp;diff=2735</id>
		<title>2024年IOAA理论第6题-星团摄影</title>
		<link rel="alternate" type="text/html" href="https://www.astro-init.top/index.php?title=2024%E5%B9%B4IOAA%E7%90%86%E8%AE%BA%E7%AC%AC6%E9%A2%98-%E6%98%9F%E5%9B%A2%E6%91%84%E5%BD%B1&amp;diff=2735"/>
		<updated>2025-03-06T16:55:45Z</updated>

		<summary type="html">&lt;p&gt;Quan787：创建页面，内容为“{{由ai生成}} ==英文题目==  '''T6. Cluster Photography (20 points)'''  An astronomer images Palomar 4 cluster (\(\theta = 72.0''\), \(m_V = 20.6 \, \text{mag/a…”&lt;/p&gt;
&lt;hr /&gt;
&lt;div&gt;{{由ai生成}}&lt;br /&gt;
==英文题目==&lt;br /&gt;
&lt;br /&gt;
'''T6. Cluster Photography (20 points)'''&lt;br /&gt;
&lt;br /&gt;
An astronomer images Palomar 4 cluster (\(\theta = 72.0''\), \(m_V = 20.6 \, \text{mag/arcsec}^2\)) using a 305mm f/5 telescope and CCD (\(\eta = 80\%\), pixel size \(3.80\mu m\)).&lt;br /&gt;
&lt;br /&gt;
Given:&lt;br /&gt;
&lt;br /&gt;
- \(V\)-band: \(\lambda_V = 550nm\), \(\Delta\lambda_V = 88.0nm\)&lt;br /&gt;
&lt;br /&gt;
- 0-mag flux: 10000 counts/mm/cm\(^2\)/s&lt;br /&gt;
&lt;br /&gt;
- CCD noise: RON=5/pixel, DN=6/pixel/min&lt;br /&gt;
&lt;br /&gt;
(a) (3 points) Calculate plate scale (arcmin/mm)&lt;br /&gt;
&lt;br /&gt;
(b) (4 points) Estimate number of pixels (\(n_p\)) covered by the cluster&lt;br /&gt;
&lt;br /&gt;
(c) (13 points) Derive sky brightness (mag/arcsec\(^2\)) given S/N=225 with 15s exposure&lt;br /&gt;
&lt;br /&gt;
[[文件:IOAA2024T6-1.jpg|缩略图|居中|图二]]&lt;br /&gt;
&lt;br /&gt;
==中文翻译==&lt;br /&gt;
&lt;br /&gt;
'''T6. 星团摄影（20分）'''&lt;br /&gt;
&lt;br /&gt;
使用305mm f/5望远镜和CCD（量子效率80%，像素尺寸3.80μm）拍摄帕洛玛4星团（角直径72.0''，V波段面亮度20.6星等/平方角秒）。&lt;br /&gt;
&lt;br /&gt;
已知：&lt;br /&gt;
- V波段中心波长550nm，带宽88.0nm&lt;br /&gt;
&lt;br /&gt;
- 0等星流量：10000计数/毫米/平方厘米/秒&lt;br /&gt;
&lt;br /&gt;
- CCD噪声：读出噪声5计数/像素，暗电流6计数/像素/分钟&lt;br /&gt;
&lt;br /&gt;
(a) (3分) 计算板尺度（角分/毫米）&lt;br /&gt;
&lt;br /&gt;
(b) (4分) 估算星团覆盖像素数&lt;br /&gt;
&lt;br /&gt;
(c) (13分) 已知曝光15秒时信噪比225，求天空亮度（星等/平方角秒）&lt;br /&gt;
&lt;br /&gt;
[[文件:IOAA2024T6-1.jpg|缩略图|居中|图二]]&lt;br /&gt;
&lt;br /&gt;
== 官方解答 ==&lt;br /&gt;
&lt;br /&gt;
(a) 焦距\(f = 305 \times 5 = 1525mm\)，板尺度：&lt;br /&gt;
&lt;br /&gt;
$$\text{PS} = \frac{206265}{1525} \approx 135.3 \, \text{角秒/mm} = 2.26 \, \text{角分/mm}$$&lt;br /&gt;
&lt;br /&gt;
(b) 星团直径：&lt;br /&gt;
&lt;br /&gt;
$$d = 72/135.3 \approx 0.532mm \Rightarrow n_p \approx 15400 \, \text{像素}$$&lt;br /&gt;
&lt;br /&gt;
(c) 通过噪声方程反推：&lt;br /&gt;
&lt;br /&gt;
$$\sigma_{\text{总}}^2 = N_{\text{星团}} + N_{\text{天空}} + 385000 + 23100$$&lt;br /&gt;
&lt;br /&gt;
得天空亮度：&lt;br /&gt;
&lt;br /&gt;
$$m_{\text{天空}} = 21.9 \, \text{mag/arcsec}^2$$&lt;br /&gt;
&lt;br /&gt;
[[分类:望远镜与天文摄影]]&lt;br /&gt;
[[分类:由ai生成]]&lt;/div&gt;</summary>
		<author><name>Quan787</name></author>
		
	</entry>
	<entry>
		<id>https://www.astro-init.top/index.php?title=2024%E5%B9%B4IOAA%E7%90%86%E8%AE%BA%E7%AC%AC5%E9%A2%98-%E5%AE%87%E5%AE%99%E5%BE%AE%E6%B3%A2%E8%83%8C%E6%99%AF&amp;diff=2734</id>
		<title>2024年IOAA理论第5题-宇宙微波背景</title>
		<link rel="alternate" type="text/html" href="https://www.astro-init.top/index.php?title=2024%E5%B9%B4IOAA%E7%90%86%E8%AE%BA%E7%AC%AC5%E9%A2%98-%E5%AE%87%E5%AE%99%E5%BE%AE%E6%B3%A2%E8%83%8C%E6%99%AF&amp;diff=2734"/>
		<updated>2025-03-06T16:55:03Z</updated>

		<summary type="html">&lt;p&gt;Quan787：创建页面，内容为“{{由ai生成}} ==英文题目==  '''T5. CMB (10 points)'''  The Cosmic Microwave Background (CMB) is radiation emitted during the early Universe. Its emission spect…”&lt;/p&gt;
&lt;hr /&gt;
&lt;div&gt;{{由ai生成}}&lt;br /&gt;
==英文题目==&lt;br /&gt;
&lt;br /&gt;
'''T5. CMB (10 points)'''&lt;br /&gt;
&lt;br /&gt;
The Cosmic Microwave Background (CMB) is radiation emitted during the early Universe. Its emission spectrum today has a peak at a temperature of approximately \(T_{\text{today}} \sim 3K\).&lt;br /&gt;
&lt;br /&gt;
(a) (3 points) What is the redshift (\(z\)) at which the CMB spectrum has a peak at the infrared wavelength of \(\lambda_{\text{IR}} \sim 0.1 \, \text{mm}\)?&lt;br /&gt;
&lt;br /&gt;
(b) (7 points) Assuming a spatially flat, matter-dominated Universe, find the age of the Universe corresponding to this redshift.&lt;br /&gt;
&lt;br /&gt;
==中文翻译==&lt;br /&gt;
&lt;br /&gt;
'''T5. 宇宙微波背景（10分）'''&lt;br /&gt;
&lt;br /&gt;
宇宙微波背景（CMB）是早期宇宙发出的辐射，当前光谱峰值温度约\(T_{\text{现今}} \sim 3K\)。&lt;br /&gt;
&lt;br /&gt;
(a) (3分) 当CMB光谱峰值位于红外波长\(\lambda_{\text{红外}} \sim 0.1 \, \text{毫米}\)时，对应的红移\(z\)是多少？&lt;br /&gt;
&lt;br /&gt;
(b) (7分) 假设空间平坦且物质主导的宇宙，求该红移对应的宇宙年龄。&lt;br /&gt;
&lt;br /&gt;
== 官方解答 ==&lt;br /&gt;
&lt;br /&gt;
(a) 应用维恩位移定律：&lt;br /&gt;
&lt;br /&gt;
$$\lambda_{\text{today}} T_{\text{today}} = b \Rightarrow z = \frac{\lambda_{\text{today}} - \lambda_{\text{IR}}}{\lambda_{\text{IR}}} \approx 9$$&lt;br /&gt;
&lt;br /&gt;
(b) 采用物质主导宇宙的年龄公式：&lt;br /&gt;
&lt;br /&gt;
$$t = \frac{2}{3H_0}(1+z)^{-3/2} \approx 0.3 \, \text{Gyr}$$&lt;br /&gt;
&lt;br /&gt;
[[分类:宇宙学]]&lt;br /&gt;
[[分类:热学]]&lt;br /&gt;
[[分类:由ai生成]]&lt;/div&gt;</summary>
		<author><name>Quan787</name></author>
		
	</entry>
	<entry>
		<id>https://www.astro-init.top/index.php?title=2024%E5%B9%B4IOAA%E7%90%86%E8%AE%BA%E7%AC%AC4%E9%A2%98-%E7%99%BD%E7%9F%AE%E6%98%9F&amp;diff=2733</id>
		<title>2024年IOAA理论第4题-白矮星</title>
		<link rel="alternate" type="text/html" href="https://www.astro-init.top/index.php?title=2024%E5%B9%B4IOAA%E7%90%86%E8%AE%BA%E7%AC%AC4%E9%A2%98-%E7%99%BD%E7%9F%AE%E6%98%9F&amp;diff=2733"/>
		<updated>2025-03-06T14:56:17Z</updated>

		<summary type="html">&lt;p&gt;Quan787：创建页面，内容为“{{由ai生成}} ==英文题目==  '''T4. White Dwarf (10 points)'''  The structure of a white dwarf is sustained against gravitational collapse by the pressure of de…”&lt;/p&gt;
&lt;hr /&gt;
&lt;div&gt;{{由ai生成}}&lt;br /&gt;
==英文题目==&lt;br /&gt;
&lt;br /&gt;
'''T4. White Dwarf (10 points)'''&lt;br /&gt;
&lt;br /&gt;
The structure of a white dwarf is sustained against gravitational collapse by the pressure of degenerate electrons. The equation of state of a gas made of non-relativistic degenerate electrons is:&lt;br /&gt;
&lt;br /&gt;
$$P = \left( \frac{3}{8\pi} \right)^{2/3} \frac{h^2}{5m_e} n_e^{5/3},$$&lt;br /&gt;
&lt;br /&gt;
where \(n_e\) is the number of electrons per unit volume. In hydrostatic equilibrium:&lt;br /&gt;
&lt;br /&gt;
$$\frac{dP}{dr} = -\frac{GM(r)\rho(r)}{r^2}.$$&lt;br /&gt;
&lt;br /&gt;
Assume the density is roughly uniform and the approximation at the surface:&lt;br /&gt;
&lt;br /&gt;
$$\frac{dP}{dr} \bigg|_{r=R} \approx -\frac{P_c}{R}.$$&lt;br /&gt;
&lt;br /&gt;
(a) (6 points) Derive the mass-radius relationship \(R = a \cdot M^b\). Find exponent \(b\) and coefficient \(a\) in terms of physical constants and \(\mu_e\).&lt;br /&gt;
&lt;br /&gt;
(b) (4 points) Estimate the radius of a carbon white dwarf (\(^{12}C\)) with \(M = 1.0M_\odot\).&lt;br /&gt;
&lt;br /&gt;
==中文翻译==&lt;br /&gt;
&lt;br /&gt;
'''T4. 白矮星（10分）'''&lt;br /&gt;
&lt;br /&gt;
白矮星通过简并电子压抵抗引力坍缩。非相对论性简并电子气体的状态方程为：&lt;br /&gt;
&lt;br /&gt;
$$P = \left( \frac{3}{8\pi} \right)^{2/3} \frac{h^2}{5m_e} n_e^{5/3},$$&lt;br /&gt;
&lt;br /&gt;
其中\(n_e\)为电子数密度。在流体静力平衡条件下：&lt;br /&gt;
&lt;br /&gt;
$$\frac{dP}{dr} = -\frac{GM(r)\rho(r)}{r^2}.$$&lt;br /&gt;
&lt;br /&gt;
假设密度均匀，并在表面采用近似：&lt;br /&gt;
&lt;br /&gt;
$$\frac{dP}{dr} \bigg|_{r=R} \approx -\frac{P_c}{R}.$$&lt;br /&gt;
&lt;br /&gt;
(a) (6分) 推导质量-半径关系\(R = a \cdot M^b\)，求指数\(b\)和系数\(a\)（用物理常数和\(\mu_e\)表示）。&lt;br /&gt;
&lt;br /&gt;
(b) (4分) 估算碳白矮星(\(^{12}C\))在\(M = 1.0M_\odot\)时的半径。&lt;br /&gt;
&lt;br /&gt;
== 官方解答 ==&lt;br /&gt;
&lt;br /&gt;
(a) 结合状态方程与流体静力平衡条件：&lt;br /&gt;
&lt;br /&gt;
$$R = \left( \frac{4\pi}{3} \right) \left( \frac{3}{8\pi} \right)^{2/3} \frac{h^2}{5Gm_e} \left( \frac{3}{4\pi \mu_e m_p} \right)^{5/3} M^{-1/3}$$&lt;br /&gt;
&lt;br /&gt;
得：&lt;br /&gt;
&lt;br /&gt;
$$b = -\frac{1}{3}, \quad a \propto \mu_e^{-5/3}$$&lt;br /&gt;
&lt;br /&gt;
(b) 碳白矮星\(\mu_e = 2\)，代入常数计算得：&lt;br /&gt;
&lt;br /&gt;
$$R \approx 1.44 \times 10^6 \ \text{m}$$&lt;br /&gt;
&lt;br /&gt;
[[分类:恒星结构]]&lt;br /&gt;
[[分类:量子物理]]&lt;br /&gt;
[[分类:由ai生成]]&lt;/div&gt;</summary>
		<author><name>Quan787</name></author>
		
	</entry>
	<entry>
		<id>https://www.astro-init.top/index.php?title=2024%E5%B9%B4IOAA%E7%90%86%E8%AE%BA%E7%AC%AC3%E9%A2%98-%E5%B0%8F%E8%A1%8C%E6%98%9F&amp;diff=2732</id>
		<title>2024年IOAA理论第3题-小行星</title>
		<link rel="alternate" type="text/html" href="https://www.astro-init.top/index.php?title=2024%E5%B9%B4IOAA%E7%90%86%E8%AE%BA%E7%AC%AC3%E9%A2%98-%E5%B0%8F%E8%A1%8C%E6%98%9F&amp;diff=2732"/>
		<updated>2025-03-06T14:54:57Z</updated>

		<summary type="html">&lt;p&gt;Quan787：创建页面，内容为“{{由ai生成}} ==英文题目==  '''T3. Asteroid (10 points)'''  A peculiar asteroid of mass, \(m\), was spotted at a distance, \(d\), from a star with mass, \(M\).…”&lt;/p&gt;
&lt;hr /&gt;
&lt;div&gt;{{由ai生成}}&lt;br /&gt;
==英文题目==&lt;br /&gt;
&lt;br /&gt;
'''T3. Asteroid (10 points)'''&lt;br /&gt;
&lt;br /&gt;
A peculiar asteroid of mass, \(m\), was spotted at a distance, \(d\), from a star with mass, \(M\). The magnitude of the asteroid’s velocity at the time of the observation was \(v = \sqrt{\frac{GM}{d}}\), where \(G\) is the universal gravitational constant. The distance \(d\) is much larger than the radius of the star.&lt;br /&gt;
&lt;br /&gt;
For both of the following items, express your answers in terms of \(M\), \(d\), and physical or mathematical constants.&lt;br /&gt;
&lt;br /&gt;
(a) (8 points) If the asteroid is initially moving exactly towards the star, how long will it take for it to collide with the star?&lt;br /&gt;
&lt;br /&gt;
(b) (2 points) If the asteroid is instead initially moving exactly away from the star, how long will it now take for it to collide with the star?&lt;br /&gt;
&lt;br /&gt;
==中文翻译==&lt;br /&gt;
&lt;br /&gt;
'''T3. 小行星（10分）'''&lt;br /&gt;
&lt;br /&gt;
一颗质量为\(m\)的特殊小行星在距离质量为\(M\)的恒星\(d\)处被发现。观测时小行星的速度大小为\(v = \sqrt{\frac{GM}{d}}\)，其中\(G\)为万有引力常数。距离\(d\)远大于恒星半径。&lt;br /&gt;
&lt;br /&gt;
对以下两问，答案需用\(M\)、\(d\)和物理/数学常数表示。&lt;br /&gt;
&lt;br /&gt;
(a) (8分) 若小行星初始直接朝向恒星运动，它需要多长时间会与恒星碰撞？&lt;br /&gt;
&lt;br /&gt;
(b) (2分) 若小行星初始直接背离恒星运动，它需要多长时间会与恒星碰撞？&lt;br /&gt;
&lt;br /&gt;
== 官方解答 ==&lt;br /&gt;
&lt;br /&gt;
(a) 该情况下小行星将沿退化椭圆轨道运动。根据开普勒第三定律：&lt;br /&gt;
&lt;br /&gt;
$$T = 2\pi d \sqrt{\frac{d}{GM}}$$&lt;br /&gt;
&lt;br /&gt;
利用开普勒第二定律计算碰撞时间：&lt;br /&gt;
&lt;br /&gt;
$$\Delta t = \left( \frac{\pi}{2} - 1 \right) d \sqrt{\frac{d}{GM}}$$&lt;br /&gt;
&lt;br /&gt;
(b) 当小行星初始背离恒星运动时，需遍历轨道面积II和III后返回：&lt;br /&gt;
&lt;br /&gt;
$$\Delta t = \frac{\pi}{2} d \sqrt{\frac{d}{GM}}$$&lt;br /&gt;
&lt;br /&gt;
[[分类:天体力学]]&lt;br /&gt;
[[分类:由ai生成]]&lt;/div&gt;</summary>
		<author><name>Quan787</name></author>
		
	</entry>
	<entry>
		<id>https://www.astro-init.top/index.php?title=%E6%96%87%E4%BB%B6:IOAA2024T1-1.jpg&amp;diff=2731</id>
		<title>文件:IOAA2024T1-1.jpg</title>
		<link rel="alternate" type="text/html" href="https://www.astro-init.top/index.php?title=%E6%96%87%E4%BB%B6:IOAA2024T1-1.jpg&amp;diff=2731"/>
		<updated>2025-03-06T14:16:31Z</updated>

		<summary type="html">&lt;p&gt;Quan787：&lt;/p&gt;
&lt;hr /&gt;
&lt;div&gt;&lt;/div&gt;</summary>
		<author><name>Quan787</name></author>
		
	</entry>
	<entry>
		<id>https://www.astro-init.top/index.php?title=2024%E5%B9%B4IOAA%E7%90%86%E8%AE%BA%E7%AC%AC1%E9%A2%98-%E6%97%A5%E6%99%B7&amp;diff=2730</id>
		<title>2024年IOAA理论第1题-日晷</title>
		<link rel="alternate" type="text/html" href="https://www.astro-init.top/index.php?title=2024%E5%B9%B4IOAA%E7%90%86%E8%AE%BA%E7%AC%AC1%E9%A2%98-%E6%97%A5%E6%99%B7&amp;diff=2730"/>
		<updated>2025-03-06T14:16:07Z</updated>

		<summary type="html">&lt;p&gt;Quan787：创建页面，内容为“{{由ai生成}} ==英文题目==  '''T1. Sundial (10 points)'''  图一：日晷示意图  The following diagram represe…”&lt;/p&gt;
&lt;hr /&gt;
&lt;div&gt;{{由ai生成}}&lt;br /&gt;
==英文题目==&lt;br /&gt;
&lt;br /&gt;
'''T1. Sundial (10 points)'''&lt;br /&gt;
&lt;br /&gt;
[[文件:IOAA2024T1-1.jpg|缩略图|居中|图一：日晷示意图]]&lt;br /&gt;
&lt;br /&gt;
The following diagram represents a sundial, for which the triangle, called a gnomon, casts a shadow onto the surrounding surface, which has markings and numbers representing important information. It is known that this sundial is located either between the Tropic of Cancer and the Arctic Circle or between the Tropic of Capricorn and the Antarctic Circle.&lt;br /&gt;
&lt;br /&gt;
Throughout the year, the shadow of the tip of the gnomon is always between curves A and C.&lt;br /&gt;
&lt;br /&gt;
Read the following statements and indicate whether they are true or false. For each item, write a T on the answer sheet if you think the statement is true and an F if you think the statement is false. There is no need to explain your answers.&lt;br /&gt;
&lt;br /&gt;
(a) This sundial will only function properly if it is located in the southern hemisphere.  &lt;br /&gt;
(b) Curve A represents the trajectory of the shadow of the tip of the gnomon throughout the winter solstice (in the hemisphere the sundial is located in).  &lt;br /&gt;
(c) Line B represents the trajectory of the tip of the gnomon's shadow throughout the equinoxes.  &lt;br /&gt;
(d) The solid radial lines provide the mean local solar time.  &lt;br /&gt;
(e) The analemma shape around the dashed line corresponding to 12h shows the position of the tip of the gnomon's shadow during the true solar noon at the central meridian of the time zone throughout the year.&lt;br /&gt;
&lt;br /&gt;
==中文翻译==&lt;br /&gt;
&lt;br /&gt;
'''T1. 日晷（10分）'''&lt;br /&gt;
&lt;br /&gt;
[[文件:IOAA2024T1-1.jpg|缩略图|居中|图一：日晷示意图]]&lt;br /&gt;
&lt;br /&gt;
下图表示一个日晷，其三角形部分（称为晷针）将阴影投射到带有标记和数字的周围表面。已知该日晷位于北回归线与北极圈之间或南回归线与南极圈之间。&lt;br /&gt;
&lt;br /&gt;
全年中，晷针尖端的阴影始终位于曲线A和C之间。&lt;br /&gt;
&lt;br /&gt;
判断以下陈述的真伪。若为真，在答题纸上写T；若为假，写F。无需解释答案。&lt;br /&gt;
&lt;br /&gt;
(a) 该日晷只有在南半球才能正常工作。  &lt;br /&gt;
(b) 曲线A代表日晷所在半球冬至日晷针尖端阴影的轨迹。  &lt;br /&gt;
(c) 直线B代表春分或秋分日晷针尖端阴影的轨迹。  &lt;br /&gt;
(d) 实线放射线提供平均地方太阳时。  &lt;br /&gt;
(e) 围绕12时虚线形成的&amp;quot;8&amp;quot;字形（日行迹）显示了全年中时区中央经线真太阳正午时晷针尖端阴影的位置。&lt;br /&gt;
&lt;br /&gt;
== 官方解答 ==&lt;br /&gt;
&lt;br /&gt;
(a) **正确**。日晷的晷针指向包含南天极的半球，因此该日晷专为南半球设计。  &lt;br /&gt;
(b) **错误**。该曲线代表日晷所在半球夏至时晷针尖端阴影的轨迹。  &lt;br /&gt;
(c) **正确**。这条垂直于子午线的直线代表南半球春秋分时晷针尖端阴影的轨迹。  &lt;br /&gt;
(d) **错误**。该组放射线对应真太阳时，12时线应与南北线重合以表示真太阳正午。  &lt;br /&gt;
(e) **正确**。虚线对应时区中央经线的真太阳时，&amp;quot;8&amp;quot;字形围绕该线显示全年平均太阳正午时阴影位置。&lt;br /&gt;
&lt;br /&gt;
[[分类:球面三角]]  &lt;br /&gt;
[[分类:视运动]]  &lt;br /&gt;
[[分类:由ai生成]]&lt;/div&gt;</summary>
		<author><name>Quan787</name></author>
		
	</entry>
	<entry>
		<id>https://www.astro-init.top/index.php?title=%E6%A8%A1%E6%9D%BF:%E8%B5%9B%E4%BA%8B%E5%88%97%E8%A1%A8&amp;diff=2729</id>
		<title>模板:赛事列表</title>
		<link rel="alternate" type="text/html" href="https://www.astro-init.top/index.php?title=%E6%A8%A1%E6%9D%BF:%E8%B5%9B%E4%BA%8B%E5%88%97%E8%A1%A8&amp;diff=2729"/>
		<updated>2025-03-06T14:06:37Z</updated>

		<summary type="html">&lt;p&gt;Quan787：&lt;/p&gt;
&lt;hr /&gt;
&lt;div&gt;&amp;lt;table class=&amp;quot;wikitable&amp;quot; width=&amp;quot;100%&amp;quot; border=&amp;quot;1&amp;quot;&amp;gt;&lt;br /&gt;
&amp;lt;tr&amp;gt;&lt;br /&gt;
&amp;lt;th width=&amp;quot;50%&amp;quot; bgcolor=&amp;quot;DeepSkyBlue &amp;quot;&amp;gt;[[CNAO]]&amp;lt;/th&amp;gt;&lt;br /&gt;
&amp;lt;th width=&amp;quot;50%&amp;quot; bgcolor=&amp;quot;DeepSkyBlue &amp;quot;&amp;gt;[[IOAA]]&amp;lt;/th&amp;gt;&lt;br /&gt;
&amp;lt;/tr&amp;gt;&lt;br /&gt;
&amp;lt;tr&amp;gt;&lt;br /&gt;
&amp;lt;td&amp;gt;&lt;br /&gt;
*[[CNAO2024]]&lt;br /&gt;
*[[CNAO2023]]&lt;br /&gt;
*[[CNAO2022]]&lt;br /&gt;
*[[CNAO2020]]&lt;br /&gt;
&amp;lt;/td&amp;gt;&lt;br /&gt;
&amp;lt;td&amp;gt;&lt;br /&gt;
*[[IOAA2024]]&lt;br /&gt;
*[[IOAA2021]]&lt;br /&gt;
*[[GeCAA2020]]&lt;br /&gt;
*[[IOAA2019]]&lt;br /&gt;
&amp;lt;/td&amp;gt;&lt;br /&gt;
&amp;lt;/tr&amp;gt;&lt;br /&gt;
&amp;lt;tr&amp;gt;&lt;br /&gt;
&amp;lt;th width=&amp;quot;50%&amp;quot; bgcolor=&amp;quot;DeepSkyBlue &amp;quot;&amp;gt;[[IAO]]&amp;lt;/th&amp;gt;&lt;br /&gt;
&amp;lt;th width=&amp;quot;50%&amp;quot; bgcolor=&amp;quot;DeepSkyBlue &amp;quot;&amp;gt;[[APAO]]&amp;lt;/th&amp;gt;&lt;br /&gt;
&amp;lt;/tr&amp;gt;&lt;br /&gt;
&amp;lt;tr&amp;gt;&lt;br /&gt;
&amp;lt;td&amp;gt;&lt;br /&gt;
*[[IRAO2021]]&lt;br /&gt;
*[[IAO2019]]&lt;br /&gt;
*[[IAO2018]]&lt;br /&gt;
*[[IAO2017]]&lt;br /&gt;
&amp;lt;/td&amp;gt;&lt;br /&gt;
&amp;lt;td&amp;gt;&lt;br /&gt;
*[[APAO2018]]&lt;br /&gt;
*[[APAO2017]]&lt;br /&gt;
*[[APAO2016]]&lt;br /&gt;
&amp;lt;/td&amp;gt;&lt;br /&gt;
&amp;lt;/tr&amp;gt;&lt;br /&gt;
&amp;lt;/table&amp;gt;&lt;/div&gt;</summary>
		<author><name>Quan787</name></author>
		
	</entry>
	<entry>
		<id>https://www.astro-init.top/index.php?title=2024%E5%B9%B4IOAA%E7%90%86%E8%AE%BA%E7%AC%AC2%E9%A2%98-%E6%98%9F%E7%B3%BB%E5%9B%A2&amp;diff=2727</id>
		<title>2024年IOAA理论第2题-星系团</title>
		<link rel="alternate" type="text/html" href="https://www.astro-init.top/index.php?title=2024%E5%B9%B4IOAA%E7%90%86%E8%AE%BA%E7%AC%AC2%E9%A2%98-%E6%98%9F%E7%B3%BB%E5%9B%A2&amp;diff=2727"/>
		<updated>2025-03-06T14:06:01Z</updated>

		<summary type="html">&lt;p&gt;Quan787：Quan787移动页面2024年IOAA理论第2题-星系团质量估算至2024年IOAA理论第2题-星系团&lt;/p&gt;
&lt;hr /&gt;
&lt;div&gt;{{由ai生成}}&lt;br /&gt;
==英文题目==&lt;br /&gt;
&lt;br /&gt;
'''T2. Galaxy Cluster (10 points)'''&lt;br /&gt;
&lt;br /&gt;
An astrophysical survey mapped all the galaxies in a small region of the sky, of angular diameter \(\Delta\theta=0.01\) rad, where many galaxies seemed to be concentrated around the central area of the image. When the positions and redshifts of all the galaxies in this cluster were measured, an interesting distribution emerged, which is shown in the plot below.&lt;br /&gt;
&lt;br /&gt;
[[文件:IOAA2024T2-1.jpg|缩略图|居中|图一 星系红移分布]]&lt;br /&gt;
&lt;br /&gt;
Using these observations, estimate the total mass of the galaxy cluster and express your answer in solar masses. Assume that this galaxy cluster is in dynamical equilibrium, with a root-mean-square redshift dispersion \(\sigma_{z}=\sqrt{\langle(z-0.7)^{2}\rangle}=0.0005\). Feel free to make reasonable approximations when considering the average velocities, masses, and spatial distribution of the galaxies.&lt;br /&gt;
&lt;br /&gt;
Consider that the distance to \(\bar{z}=0.7\) in the standard cosmological model is \(D_{A}=1500\) Mpc. Ignore cosmological effects on the distance.&lt;br /&gt;
&lt;br /&gt;
==中文翻译==&lt;br /&gt;
&lt;br /&gt;
'''T2. 星系团（10分）'''&lt;br /&gt;
&lt;br /&gt;
一项天体物理巡天项目绘制了天空中角直径\(\Delta\theta=0.01\)弧度的小区域内所有星系的位置，发现许多星系集中在图像中央区域。当测量该星系团中所有星系的位置和红移时，得到了如图一所示的分布。&lt;br /&gt;
&lt;br /&gt;
通过这些观测数据，估算该星系团的总质量，并以太阳质量表示。假设该星系团处于动力学平衡状态，其红移分布的均方根弥散为\(\sigma_{z}=\sqrt{\langle(z-0.7)^{2}\rangle}=0.0005\)。在考虑星系的平均速度、质量和空间分布时，可做合理近似。&lt;br /&gt;
&lt;br /&gt;
已知标准宇宙学模型中\(\bar{z}=0.7\)对应的角直径距离为\(D_{A}=1500\) Mpc。忽略距离上的宇宙学效应。&lt;br /&gt;
&lt;br /&gt;
==官方解答==&lt;br /&gt;
&lt;br /&gt;
根据维里定理：&lt;br /&gt;
$$U+2K=0$$&lt;br /&gt;
其中\(U\)为总引力势能，\(K\)为总动能。假设所有星系质量为平均质量\(\langle m\rangle=M_{T}/N\)，则：&lt;br /&gt;
$$K=\frac{1}{2}M_{T}\sigma_{v}^{2}$$&lt;br /&gt;
其中径向速度弥散\(\sigma_{v_r}=c\cdot\sigma_z=1.499\times10^5\ \mathrm{m/s}\)。假设三维速度各向同性，则：&lt;br /&gt;
$$\sigma_{v}^{2}=3\sigma_{v_r}^{2}$$&lt;br /&gt;
引力势能估算为均匀球体的结合能：&lt;br /&gt;
$$U=-\frac{3}{5}\frac{GM_T^2}{R}$$&lt;br /&gt;
其中星系团半径：&lt;br /&gt;
$$R=\frac{D_A\cdot\Delta\theta}{2}=2.3143\times10^{23}\ \mathrm{m}$$&lt;br /&gt;
联立维里定理得：&lt;br /&gt;
$$M_T = \frac{5R\sigma_{v_r}^2}{G} = \frac{5 \times 2.314 \times 10^{23} \times (1.499 \times 10^5)^2}{6.67 \times 10^{-11}}\ \mathrm{kg}$$&lt;br /&gt;
计算得：&lt;br /&gt;
$$M_T \approx 2.0 \times 10^{14} M_\odot$$&lt;br /&gt;
&lt;br /&gt;
其他势能估算方法：&lt;br /&gt;
1. 通过粒子对势能求和：&lt;br /&gt;
$$U = -\frac{1}{2}\frac{GM_T^2}{R}$$&lt;br /&gt;
2. 量纲分析：&lt;br /&gt;
$$U = -\frac{GM_T^2}{R}$$&lt;br /&gt;
&lt;br /&gt;
[[分类:天体力学]]&lt;br /&gt;
[[分类:宇宙学]]&lt;br /&gt;
[[分类:由ai生成]]&lt;/div&gt;</summary>
		<author><name>Quan787</name></author>
		
	</entry>
	<entry>
		<id>https://www.astro-init.top/index.php?title=2024%E5%B9%B4IOAA%E7%90%86%E8%AE%BA%E7%AC%AC2%E9%A2%98-%E6%98%9F%E7%B3%BB%E5%9B%A2%E8%B4%A8%E9%87%8F%E4%BC%B0%E7%AE%97&amp;diff=2728</id>
		<title>2024年IOAA理论第2题-星系团质量估算</title>
		<link rel="alternate" type="text/html" href="https://www.astro-init.top/index.php?title=2024%E5%B9%B4IOAA%E7%90%86%E8%AE%BA%E7%AC%AC2%E9%A2%98-%E6%98%9F%E7%B3%BB%E5%9B%A2%E8%B4%A8%E9%87%8F%E4%BC%B0%E7%AE%97&amp;diff=2728"/>
		<updated>2025-03-06T14:06:01Z</updated>

		<summary type="html">&lt;p&gt;Quan787：Quan787移动页面2024年IOAA理论第2题-星系团质量估算至2024年IOAA理论第2题-星系团&lt;/p&gt;
&lt;hr /&gt;
&lt;div&gt;#重定向 [[2024年IOAA理论第2题-星系团]]&lt;/div&gt;</summary>
		<author><name>Quan787</name></author>
		
	</entry>
	<entry>
		<id>https://www.astro-init.top/index.php?title=IOAA2024&amp;diff=2726</id>
		<title>IOAA2024</title>
		<link rel="alternate" type="text/html" href="https://www.astro-init.top/index.php?title=IOAA2024&amp;diff=2726"/>
		<updated>2025-03-06T14:04:58Z</updated>

		<summary type="html">&lt;p&gt;Quan787：&lt;/p&gt;
&lt;hr /&gt;
&lt;div&gt;第十七届国际天文与天体物理奥林匹克竞赛（17th IOAA）于2024年8月17日至8月27日在巴西里约热内卢成功举行。共有来自全球54个国家的250余位选手参赛。&lt;br /&gt;
==理论考试==&lt;br /&gt;
[[2024年IOAA理论第1题-日晷]]&lt;br /&gt;
&lt;br /&gt;
[[2024年IOAA理论第2题-星系团]]&lt;br /&gt;
&lt;br /&gt;
[[2024年IOAA理论第3题-小行星]]&lt;br /&gt;
&lt;br /&gt;
[[2024年IOAA理论第4题-白矮星]]&lt;br /&gt;
&lt;br /&gt;
[[2024年IOAA理论第5题-宇宙微波背景]]&lt;br /&gt;
&lt;br /&gt;
[[2024年IOAA理论第6题-星团摄影]]&lt;br /&gt;
&lt;br /&gt;
[[2024年IOAA理论第7题-漂流者]]&lt;br /&gt;
&lt;br /&gt;
[[2024年IOAA理论第8题-双星硬化]]&lt;br /&gt;
&lt;br /&gt;
[[2024年IOAA理论第9题-吸积物理]]&lt;br /&gt;
&lt;br /&gt;
[[2024年IOAA理论第10题-最大日食]]&lt;br /&gt;
&lt;br /&gt;
[[2024年IOAA理论第11题-地面轨迹]]&lt;br /&gt;
==中国队参赛情况==&lt;br /&gt;
&lt;br /&gt;
领队：方媛媛、郭懿琳&lt;br /&gt;
观察员：李昕&lt;br /&gt;
&lt;br /&gt;
{| class=&amp;quot;wikitable&amp;quot;&lt;br /&gt;
|+&lt;br /&gt;
!姓名&lt;br /&gt;
!地区&lt;br /&gt;
!奖项&lt;br /&gt;
|-&lt;br /&gt;
|周泽震&lt;br /&gt;
|浙江省绍兴市第一中学&lt;br /&gt;
|银牌&lt;br /&gt;
|-&lt;br /&gt;
|曾昱翔&lt;br /&gt;
|广东省深圳中学&lt;br /&gt;
|银牌&lt;br /&gt;
|-&lt;br /&gt;
|石一宽&lt;br /&gt;
|北京市第八中学&lt;br /&gt;
|银牌&lt;br /&gt;
|-&lt;br /&gt;
|左名佑&lt;br /&gt;
|广东省华南师范大学附属中学&lt;br /&gt;
|银牌&lt;br /&gt;
|-&lt;br /&gt;
|李煜宸&lt;br /&gt;
|浙江省宁波市镇海蛟川书院&lt;br /&gt;
|铜牌&lt;br /&gt;
|}&lt;br /&gt;
&lt;br /&gt;
==相关链接==&lt;br /&gt;
[https://www.bjp.org.cn/qgzxstwzsjs/asry/4028c136919fb9850191a15c2b7e001f.shtml 北京天文馆带队参加第十七届国际天文与天体物理奥林匹克竞赛载誉归来]&lt;br /&gt;
&lt;br /&gt;
[https://news.qq.com/rain/a/20240830A0A1ZE00 4银1铜！我国中学生在第十七届国际天文与天体物理奥林匹克竞赛上获奖]&lt;/div&gt;</summary>
		<author><name>Quan787</name></author>
		
	</entry>
	<entry>
		<id>https://www.astro-init.top/index.php?title=2024%E5%B9%B4IOAA%E7%90%86%E8%AE%BA%E7%AC%AC2%E9%A2%98-%E6%98%9F%E7%B3%BB%E5%9B%A2&amp;diff=2725</id>
		<title>2024年IOAA理论第2题-星系团</title>
		<link rel="alternate" type="text/html" href="https://www.astro-init.top/index.php?title=2024%E5%B9%B4IOAA%E7%90%86%E8%AE%BA%E7%AC%AC2%E9%A2%98-%E6%98%9F%E7%B3%BB%E5%9B%A2&amp;diff=2725"/>
		<updated>2025-03-06T12:20:47Z</updated>

		<summary type="html">&lt;p&gt;Quan787：&lt;/p&gt;
&lt;hr /&gt;
&lt;div&gt;{{由ai生成}}&lt;br /&gt;
==英文题目==&lt;br /&gt;
&lt;br /&gt;
'''T2. Galaxy Cluster (10 points)'''&lt;br /&gt;
&lt;br /&gt;
An astrophysical survey mapped all the galaxies in a small region of the sky, of angular diameter \(\Delta\theta=0.01\) rad, where many galaxies seemed to be concentrated around the central area of the image. When the positions and redshifts of all the galaxies in this cluster were measured, an interesting distribution emerged, which is shown in the plot below.&lt;br /&gt;
&lt;br /&gt;
[[文件:IOAA2024T2-1.jpg|缩略图|居中|图一 星系红移分布]]&lt;br /&gt;
&lt;br /&gt;
Using these observations, estimate the total mass of the galaxy cluster and express your answer in solar masses. Assume that this galaxy cluster is in dynamical equilibrium, with a root-mean-square redshift dispersion \(\sigma_{z}=\sqrt{\langle(z-0.7)^{2}\rangle}=0.0005\). Feel free to make reasonable approximations when considering the average velocities, masses, and spatial distribution of the galaxies.&lt;br /&gt;
&lt;br /&gt;
Consider that the distance to \(\bar{z}=0.7\) in the standard cosmological model is \(D_{A}=1500\) Mpc. Ignore cosmological effects on the distance.&lt;br /&gt;
&lt;br /&gt;
==中文翻译==&lt;br /&gt;
&lt;br /&gt;
'''T2. 星系团（10分）'''&lt;br /&gt;
&lt;br /&gt;
一项天体物理巡天项目绘制了天空中角直径\(\Delta\theta=0.01\)弧度的小区域内所有星系的位置，发现许多星系集中在图像中央区域。当测量该星系团中所有星系的位置和红移时，得到了如图一所示的分布。&lt;br /&gt;
&lt;br /&gt;
通过这些观测数据，估算该星系团的总质量，并以太阳质量表示。假设该星系团处于动力学平衡状态，其红移分布的均方根弥散为\(\sigma_{z}=\sqrt{\langle(z-0.7)^{2}\rangle}=0.0005\)。在考虑星系的平均速度、质量和空间分布时，可做合理近似。&lt;br /&gt;
&lt;br /&gt;
已知标准宇宙学模型中\(\bar{z}=0.7\)对应的角直径距离为\(D_{A}=1500\) Mpc。忽略距离上的宇宙学效应。&lt;br /&gt;
&lt;br /&gt;
==官方解答==&lt;br /&gt;
&lt;br /&gt;
根据维里定理：&lt;br /&gt;
$$U+2K=0$$&lt;br /&gt;
其中\(U\)为总引力势能，\(K\)为总动能。假设所有星系质量为平均质量\(\langle m\rangle=M_{T}/N\)，则：&lt;br /&gt;
$$K=\frac{1}{2}M_{T}\sigma_{v}^{2}$$&lt;br /&gt;
其中径向速度弥散\(\sigma_{v_r}=c\cdot\sigma_z=1.499\times10^5\ \mathrm{m/s}\)。假设三维速度各向同性，则：&lt;br /&gt;
$$\sigma_{v}^{2}=3\sigma_{v_r}^{2}$$&lt;br /&gt;
引力势能估算为均匀球体的结合能：&lt;br /&gt;
$$U=-\frac{3}{5}\frac{GM_T^2}{R}$$&lt;br /&gt;
其中星系团半径：&lt;br /&gt;
$$R=\frac{D_A\cdot\Delta\theta}{2}=2.3143\times10^{23}\ \mathrm{m}$$&lt;br /&gt;
联立维里定理得：&lt;br /&gt;
$$M_T = \frac{5R\sigma_{v_r}^2}{G} = \frac{5 \times 2.314 \times 10^{23} \times (1.499 \times 10^5)^2}{6.67 \times 10^{-11}}\ \mathrm{kg}$$&lt;br /&gt;
计算得：&lt;br /&gt;
$$M_T \approx 2.0 \times 10^{14} M_\odot$$&lt;br /&gt;
&lt;br /&gt;
其他势能估算方法：&lt;br /&gt;
1. 通过粒子对势能求和：&lt;br /&gt;
$$U = -\frac{1}{2}\frac{GM_T^2}{R}$$&lt;br /&gt;
2. 量纲分析：&lt;br /&gt;
$$U = -\frac{GM_T^2}{R}$$&lt;br /&gt;
&lt;br /&gt;
[[分类:天体力学]]&lt;br /&gt;
[[分类:宇宙学]]&lt;br /&gt;
[[分类:由ai生成]]&lt;/div&gt;</summary>
		<author><name>Quan787</name></author>
		
	</entry>
	<entry>
		<id>https://www.astro-init.top/index.php?title=%E6%96%87%E4%BB%B6:Ai_gen.png&amp;diff=2724</id>
		<title>文件:Ai gen.png</title>
		<link rel="alternate" type="text/html" href="https://www.astro-init.top/index.php?title=%E6%96%87%E4%BB%B6:Ai_gen.png&amp;diff=2724"/>
		<updated>2025-03-06T08:10:33Z</updated>

		<summary type="html">&lt;p&gt;Quan787：Quan787上传文件:Ai gen.png的新版本&lt;/p&gt;
&lt;hr /&gt;
&lt;div&gt;&lt;/div&gt;</summary>
		<author><name>Quan787</name></author>
		
	</entry>
	<entry>
		<id>https://www.astro-init.top/index.php?title=%E6%96%87%E4%BB%B6:Ai_gen.png&amp;diff=2723</id>
		<title>文件:Ai gen.png</title>
		<link rel="alternate" type="text/html" href="https://www.astro-init.top/index.php?title=%E6%96%87%E4%BB%B6:Ai_gen.png&amp;diff=2723"/>
		<updated>2025-03-06T08:08:55Z</updated>

		<summary type="html">&lt;p&gt;Quan787：&lt;/p&gt;
&lt;hr /&gt;
&lt;div&gt;&lt;/div&gt;</summary>
		<author><name>Quan787</name></author>
		
	</entry>
	<entry>
		<id>https://www.astro-init.top/index.php?title=%E6%A8%A1%E6%9D%BF:%E7%94%B1ai%E7%94%9F%E6%88%90&amp;diff=2722</id>
		<title>模板:由ai生成</title>
		<link rel="alternate" type="text/html" href="https://www.astro-init.top/index.php?title=%E6%A8%A1%E6%9D%BF:%E7%94%B1ai%E7%94%9F%E6%88%90&amp;diff=2722"/>
		<updated>2025-03-06T08:08:41Z</updated>

		<summary type="html">&lt;p&gt;Quan787：&lt;/p&gt;
&lt;hr /&gt;
&lt;div&gt;{{页首标记|cyan|[[文件:ai_gen.png|无框]]|由ai生成|本页内容由ai生成。请帮助校对和完善这个页面。}}&lt;/div&gt;</summary>
		<author><name>Quan787</name></author>
		
	</entry>
	<entry>
		<id>https://www.astro-init.top/index.php?title=2024%E5%B9%B4IOAA%E7%90%86%E8%AE%BA%E7%AC%AC2%E9%A2%98-%E6%98%9F%E7%B3%BB%E5%9B%A2&amp;diff=2721</id>
		<title>2024年IOAA理论第2题-星系团</title>
		<link rel="alternate" type="text/html" href="https://www.astro-init.top/index.php?title=2024%E5%B9%B4IOAA%E7%90%86%E8%AE%BA%E7%AC%AC2%E9%A2%98-%E6%98%9F%E7%B3%BB%E5%9B%A2&amp;diff=2721"/>
		<updated>2025-03-05T16:59:32Z</updated>

		<summary type="html">&lt;p&gt;Quan787：&lt;/p&gt;
&lt;hr /&gt;
&lt;div&gt;==英文题目==  &lt;br /&gt;
{{由ai生成}}  &lt;br /&gt;
&lt;br /&gt;
'''T2. Galaxy Cluster (10 points)'''  &lt;br /&gt;
&lt;br /&gt;
An astrophysical survey mapped all the galaxies in a small region of the sky, of angular diameter \(\Delta \theta = 0.01\) rad, where many galaxies seemed to be concentrated around the central area of the image. When the positions and redshifts of all the galaxies in this cluster were measured, an interesting distribution emerged, which is shown in the plot below.  &lt;br /&gt;
&lt;br /&gt;
Using these observations, estimate the total mass of the galaxy cluster and express your answer in solar masses. Assume that this galaxy cluster is in dynamical equilibrium, with a root-mean-square redshift dispersion \(\sigma_z = \sqrt{\langle (z - 0.7)^2 \rangle} = 0.0005\). Feel free to make reasonable approximations when considering the average velocities, masses, and spatial distribution of the galaxies.  &lt;br /&gt;
&lt;br /&gt;
Consider that the distance to \(\bar{z} = 0.7\) in the standard cosmological model is \(D_A = 1500\) Mpc. Ignore cosmological effects on the distance.  &lt;br /&gt;
&lt;br /&gt;
[[文件:IOAA2024T2-1.jpg|缩略图|居中|图一 星系红移分布示意图]]  &lt;br /&gt;
&lt;br /&gt;
==中文翻译==  &lt;br /&gt;
{{由ai生成}}  &lt;br /&gt;
&lt;br /&gt;
'''第2题. 星系团（10分）'''  &lt;br /&gt;
&lt;br /&gt;
一项天体物理巡天观测了天空中角直径\(\Delta \theta = 0.01\)弧度的小区域内的所有星系，发现许多星系集中在图像的中心区域。测量该星系团中所有星系的位置和红移后，出现了有趣的分布（见下图）。  &lt;br /&gt;
&lt;br /&gt;
利用这些观测结果，估算该星系团的总质量并以太阳质量为单位表示。假设该星系团处于动力学平衡状态，红移弥散的均方根值为\(\sigma_z = \sqrt{\langle (z - 0.7)^2 \rangle} = 0.0005\)。在考虑星系的平均速度、质量和空间分布时，可进行合理近似。  &lt;br /&gt;
&lt;br /&gt;
已知标准宇宙学模型中红移\(\bar{z} = 0.7\)对应的角直径距离为\(D_A = 1500\) Mpc。忽略宇宙学效应对距离的影响。  &lt;br /&gt;
&lt;br /&gt;
==官方解答==  &lt;br /&gt;
{{由ai生成}}  &lt;br /&gt;
&lt;br /&gt;
根据维里定理，总引力势能\(U\)和总动能\(K\)满足：  &lt;br /&gt;
$$U + 2K = 0$$  &lt;br /&gt;
&lt;br /&gt;
假设星系团中有\(N\)个质量为\(m_i\)的星系，其相对于星系团中心的运动速度为\(\vec{u}_i\)，则动能为：  &lt;br /&gt;
$$K = \frac{1}{2}M_T \sigma_v^2$$  &lt;br /&gt;
其中\(\sigma_v = \sqrt{\langle u_i^2 \rangle}\)为速度弥散。红移弥散对应的径向速度弥散为：  &lt;br /&gt;
$$\sigma_{v_r} = c \cdot \sigma_z = 2.998 \times 10^8 \, \text{m/s} \times 0.0005 = 1.499 \times 10^5 \, \text{m/s}$$  &lt;br /&gt;
&lt;br /&gt;
假设三维速度各向同性，则\(\sigma_v^2 = 3\sigma_{v_r}^2\)。引力势能近似为均匀球体的结合能：  &lt;br /&gt;
$$U = -\frac{3}{5} \frac{GM_T^2}{R}$$  &lt;br /&gt;
其中星系团半径：  &lt;br /&gt;
$$R = \frac{D_A \cdot \Delta \theta}{2} = \frac{1500 \times 10^6 \times 206265 \times 1.496 \times 10^{11} \times 10^{-2}}{2} = 2.3143 \times 10^{23} \, \text{m}$$  &lt;br /&gt;
&lt;br /&gt;
代入维里定理：  &lt;br /&gt;
$$\frac{5R\sigma_{v_r}^2}{G} = M_T$$  &lt;br /&gt;
计算得：  &lt;br /&gt;
$$M_T = \frac{5 \times 2.314 \times 10^{23} \times (1.499 \times 10^5)^2}{6.67 \times 10^{-11}} \, \text{kg} \approx 3.9 \times 10^{44} \, \text{kg} = 2.0 \times 10^{14} \, M_\odot$$  &lt;br /&gt;
&lt;br /&gt;
[[分类:宇宙学]]  &lt;br /&gt;
[[分类:天体力学]]  &lt;br /&gt;
[[分类:由ai生成]]&lt;/div&gt;</summary>
		<author><name>Quan787</name></author>
		
	</entry>
	<entry>
		<id>https://www.astro-init.top/index.php?title=2024%E5%B9%B4IOAA%E7%90%86%E8%AE%BA%E7%AC%AC2%E9%A2%98-%E6%98%9F%E7%B3%BB%E5%9B%A2&amp;diff=2720</id>
		<title>2024年IOAA理论第2题-星系团</title>
		<link rel="alternate" type="text/html" href="https://www.astro-init.top/index.php?title=2024%E5%B9%B4IOAA%E7%90%86%E8%AE%BA%E7%AC%AC2%E9%A2%98-%E6%98%9F%E7%B3%BB%E5%9B%A2&amp;diff=2720"/>
		<updated>2025-03-05T16:58:21Z</updated>

		<summary type="html">&lt;p&gt;Quan787：&lt;/p&gt;
&lt;hr /&gt;
&lt;div&gt;==英文题目==  &lt;br /&gt;
{{由ai生成}}  &lt;br /&gt;
&lt;br /&gt;
'''T2. Galaxy Cluster (10 points)'''  &lt;br /&gt;
&lt;br /&gt;
An astrophysical survey mapped all the galaxies in a small region of the sky, of angular diameter \(\Delta \theta = 0.01\) rad, where many galaxies seemed to be concentrated around the central area of the image. When the positions and redshifts of all the galaxies in this cluster were measured, an interesting distribution emerged, which is shown in the plot below.  &lt;br /&gt;
&lt;br /&gt;
Using these observations, estimate the total mass of the galaxy cluster and express your answer in solar masses. Assume that this galaxy cluster is in dynamical equilibrium, with a root-mean-square redshift dispersion \(\sigma_z = \sqrt{\langle (z - 0.7)^2 \rangle} = 0.0005\). Feel free to make reasonable approximations when considering the average velocities, masses, and spatial distribution of the galaxies.  &lt;br /&gt;
&lt;br /&gt;
Consider that the distance to \(\bar{z} = 0.7\) in the standard cosmological model is \(D_A = 1500\) Mpc. Ignore cosmological effects on the distance.  &lt;br /&gt;
&lt;br /&gt;
[[文件:IOAA2024T2-1.jpg|缩略图|居中|图一 星系红移分布示意图]]  &lt;br /&gt;
&lt;br /&gt;
==中文翻译==  &lt;br /&gt;
{{由ai生成}}  &lt;br /&gt;
&lt;br /&gt;
'''T2. 星系团（10分）'''  &lt;br /&gt;
&lt;br /&gt;
一项天体物理巡天观测了天空中一个小区域（角直径\(\Delta \theta = 0.01\)弧度）内的所有星系，发现许多星系集中在图像的中心区域。测量该星系团中所有星系的位置和红移后，呈现出有趣的分布（如下图所示）。  &lt;br /&gt;
&lt;br /&gt;
利用这些观测数据，估算该星系团的总质量，并以太阳质量为单位表示答案。假设该星系团处于动力学平衡状态，红移弥散的均方根值为\(\sigma_z = \sqrt{\langle (z - 0.7)^2 \rangle} = 0.0005\)。在考虑星系的平均速度、质量和空间分布时，可作合理近似。  &lt;br /&gt;
&lt;br /&gt;
已知标准宇宙学模型中\(\bar{z} = 0.7\)对应的共动距离为\(D_A = 1500\) Mpc，忽略距离计算中的宇宙学效应。  &lt;br /&gt;
&lt;br /&gt;
[[文件:IOAA2024T2-1.jpg|缩略图|居中|图一 星系红移分布示意图]]  &lt;br /&gt;
&lt;br /&gt;
==官方解答==  &lt;br /&gt;
{{由ai生成}}  &lt;br /&gt;
&lt;br /&gt;
根据维里定理，总引力势能\(U\)和总动能\(K\)满足：  &lt;br /&gt;
$$U + 2K = 0$$  &lt;br /&gt;
&lt;br /&gt;
假设星系团中有\(N\)个质量为\(m_i\)的星系，其相对于星系团中心的运动速度为\(\vec{u}_i\)，则动能为：  &lt;br /&gt;
$$K = \frac{1}{2}M_T \sigma_v^2$$  &lt;br /&gt;
其中\(\sigma_v = \sqrt{\langle u_i^2 \rangle}\)为速度弥散。红移弥散对应的径向速度弥散为：  &lt;br /&gt;
$$\sigma_{v_r} = c \cdot \sigma_z = 2.998 \times 10^8 \, \text{m/s} \times 0.0005 = 1.499 \times 10^5 \, \text{m/s}$$  &lt;br /&gt;
&lt;br /&gt;
假设三维速度各向同性，则\(\sigma_v^2 = 3\sigma_{v_r}^2\)。引力势能近似为均匀球体的结合能：  &lt;br /&gt;
$$U = -\frac{3}{5} \frac{GM_T^2}{R}$$  &lt;br /&gt;
其中星系团半径：  &lt;br /&gt;
$$R = \frac{D_A \cdot \Delta \theta}{2} = \frac{1500 \times 10^6 \times 206265 \times 1.496 \times 10^{11} \times 10^{-2}}{2} = 2.3143 \times 10^{23} \, \text{m}$$  &lt;br /&gt;
&lt;br /&gt;
代入维里定理：  &lt;br /&gt;
$$\frac{5R\sigma_{v_r}^2}{G} = M_T$$  &lt;br /&gt;
计算得：  &lt;br /&gt;
$$M_T = \frac{5 \times 2.314 \times 10^{23} \times (1.499 \times 10^5)^2}{6.67 \times 10^{-11}} \, \text{kg} \approx 3.9 \times 10^{44} \, \text{kg} = 2.0 \times 10^{14} \, M_\odot$$  &lt;br /&gt;
&lt;br /&gt;
[[分类:宇宙学]]  &lt;br /&gt;
[[分类:天体力学]]  &lt;br /&gt;
[[分类:由ai生成]]&lt;/div&gt;</summary>
		<author><name>Quan787</name></author>
		
	</entry>
	<entry>
		<id>https://www.astro-init.top/index.php?title=2024%E5%B9%B4IOAA%E7%90%86%E8%AE%BA%E7%AC%AC2%E9%A2%98-%E6%98%9F%E7%B3%BB%E5%9B%A2&amp;diff=2719</id>
		<title>2024年IOAA理论第2题-星系团</title>
		<link rel="alternate" type="text/html" href="https://www.astro-init.top/index.php?title=2024%E5%B9%B4IOAA%E7%90%86%E8%AE%BA%E7%AC%AC2%E9%A2%98-%E6%98%9F%E7%B3%BB%E5%9B%A2&amp;diff=2719"/>
		<updated>2025-03-05T16:50:00Z</updated>

		<summary type="html">&lt;p&gt;Quan787：&lt;/p&gt;
&lt;hr /&gt;
&lt;div&gt;==英文题目==  &lt;br /&gt;
{{由ai生成}}  &lt;br /&gt;
&lt;br /&gt;
'''T2. Galaxy Cluster (10 points)'''  &lt;br /&gt;
&lt;br /&gt;
An astrophysical survey mapped all the galaxies in a small region of the sky, of angular diameter \(\Delta \theta = 0.01\) rad, where many galaxies seemed to be concentrated around the central area of the image. When the positions and redshifts of all the galaxies in this cluster were measured, an interesting distribution emerged, which is shown in the plot below.  &lt;br /&gt;
&lt;br /&gt;
Using these observations, estimate the total mass of the galaxy cluster and express your answer in solar masses. Assume that this galaxy cluster is in dynamical equilibrium, with a root-mean-square redshift dispersion \(\sigma_z = \sqrt{\langle (z - 0.7)^2 \rangle} = 0.0005\). Feel free to make reasonable approximations when considering the average velocities, masses, and spatial distribution of the galaxies.  &lt;br /&gt;
&lt;br /&gt;
Consider that the distance to \(\bar{z} = 0.7\) in the standard cosmological model is \(D_A = 1500\) Mpc. Ignore cosmological effects on the distance.  &lt;br /&gt;
&lt;br /&gt;
[[文件:IOAA2024T2-1.jpg|缩略图|居中|图一 星系红移分布示意图]]  &lt;br /&gt;
&lt;br /&gt;
==中文翻译==  &lt;br /&gt;
{{由ai生成}}  &lt;br /&gt;
&lt;br /&gt;
'''T2. 星系团（10分）'''  &lt;br /&gt;
&lt;br /&gt;
一项天体物理巡天观测了天空中一个小区域（角直径\(\Delta \theta = 0.01\)弧度）内的所有星系，发现许多星系集中在图像的中心区域。测量该星系团中所有星系的位置和红移后，呈现出有趣的分布（如下图所示）。  &lt;br /&gt;
&lt;br /&gt;
利用这些观测数据，估算该星系团的总质量，并以太阳质量为单位表示答案。假设该星系团处于动力学平衡状态，红移弥散的均方根值为\(\sigma_z = \sqrt{\langle (z - 0.7)^2 \rangle} = 0.0005\)。在考虑星系的平均速度、质量和空间分布时，可作合理近似。  &lt;br /&gt;
&lt;br /&gt;
已知标准宇宙学模型中\(\bar{z} = 0.7\)对应的共动距离为\(D_A = 1500\) Mpc，忽略距离计算中的宇宙学效应。  &lt;br /&gt;
&lt;br /&gt;
[[文件:IOAA2024T2-1.jpg|缩略图|居中|图一 星系红移分布示意图]]  &lt;br /&gt;
&lt;br /&gt;
==官方解答==  &lt;br /&gt;
{{由ai生成}}  &lt;br /&gt;
&lt;br /&gt;
根据维里定理，总引力势能\(U\)和动能\(K\)满足：  &lt;br /&gt;
$$ U + 2K = 0 $$  &lt;br /&gt;
&lt;br /&gt;
假设星系团中所有星系平均质量为\(\langle m \rangle = M_T/N\)，动能可近似为：  &lt;br /&gt;
$$ K = \frac{1}{2} M_T \sigma_v^2 $$  &lt;br /&gt;
&lt;br /&gt;
其中径向速度弥散\(\sigma_{v_r} = c \cdot \sigma_z = 1.499 \times 10^5 \, \text{m/s}\)，三维速度弥散满足\(\sigma_v^2 = 3\sigma_{v_r}^2\)。  &lt;br /&gt;
&lt;br /&gt;
引力势能采用均匀球体近似：  &lt;br /&gt;
$$ U = -\frac{3}{5} \frac{G M_T^2}{R} $$  &lt;br /&gt;
其中星系团半径：  &lt;br /&gt;
$$ R = \frac{D_A \cdot \Delta \theta}{2} = 2.314 \times 10^{23} \, \text{m} $$  &lt;br /&gt;
&lt;br /&gt;
联立维里定理得质量公式：  &lt;br /&gt;
$$ M_T = \frac{5 R \sigma_{v_r}^2}{G} $$  &lt;br /&gt;
代入数据计算得：  &lt;br /&gt;
$$ M_T \approx 2.0 \times 10^{14} \, M_\odot $$  &lt;br /&gt;
&lt;br /&gt;
[[分类:宇宙学]]  &lt;br /&gt;
[[分类:天体力学]]  &lt;br /&gt;
[[分类:由ai生成]]&lt;/div&gt;</summary>
		<author><name>Quan787</name></author>
		
	</entry>
	<entry>
		<id>https://www.astro-init.top/index.php?title=2024%E5%B9%B4IOAA%E7%90%86%E8%AE%BA%E7%AC%AC2%E9%A2%98-%E6%98%9F%E7%B3%BB%E5%9B%A2&amp;diff=2718</id>
		<title>2024年IOAA理论第2题-星系团</title>
		<link rel="alternate" type="text/html" href="https://www.astro-init.top/index.php?title=2024%E5%B9%B4IOAA%E7%90%86%E8%AE%BA%E7%AC%AC2%E9%A2%98-%E6%98%9F%E7%B3%BB%E5%9B%A2&amp;diff=2718"/>
		<updated>2025-03-05T16:17:23Z</updated>

		<summary type="html">&lt;p&gt;Quan787：&lt;/p&gt;
&lt;hr /&gt;
&lt;div&gt;2024年IOAA理论第2题-星系团质量估计&lt;br /&gt;
&lt;br /&gt;
==英文题目==&lt;br /&gt;
&lt;br /&gt;
{{由ai生成}}&lt;br /&gt;
&lt;br /&gt;
'''T2. Galaxy Cluster (10 points)'''&lt;br /&gt;
&lt;br /&gt;
An astrophysical survey mapped all the galaxies in a small region of the sky, of angular diameter \(\Delta\theta=0.01\) rad, where many galaxies seemed to be concentrated around the central area of the image. When the positions and redshifts of all the galaxies in this cluster were measured, an interesting distribution emerged, which is shown in the plot below.&lt;br /&gt;
&lt;br /&gt;
Using these observations, estimate the total mass of the galaxy cluster and express your answer in solar masses. Assume that this galaxy cluster is in dynamical equilibrium, with a root-mean-square redshift dispersion \(\sigma_{z}=\sqrt{\langle(z-0.7)^{2}\rangle}=0.0005\). Feel free to make reasonable approximations when considering the average velocities, masses, and spatial distribution of the galaxies.&lt;br /&gt;
&lt;br /&gt;
Consider that the distance to \(\bar{z}=0.7\) in the standard cosmological model is \(D_{A}=1500\) Mpc. Ignore cosmological effects on the distance.&lt;br /&gt;
&lt;br /&gt;
==中文翻译==&lt;br /&gt;
&lt;br /&gt;
{{由ai生成}}&lt;br /&gt;
&lt;br /&gt;
'''第2题 星系团质量估计（10分）'''&lt;br /&gt;
&lt;br /&gt;
某天体物理巡天项目对天空小区域（角直径\(\Delta\theta=0.01\)弧度）内所有星系进行了测绘，发现许多星系集中在图像中心区域。通过测量该星团中所有星系的位置和红移，得到下图所示的分布。&lt;br /&gt;
&lt;br /&gt;
假设该星系团处于动力学平衡状态，其红移分布的均方根弥散为\(\sigma_{z}=\sqrt{\langle(z-0.7)^{2}\rangle}=0.0005\)。请估算该星系团的总质量，并以太阳质量为单位表示。在考虑星系平均速度、质量和空间分布时可采用合理近似。&lt;br /&gt;
&lt;br /&gt;
已知标准宇宙学模型中红移\(\bar{z}=0.7\)对应的角直径距离\(D_{A}=1500\) Mpc。忽略宇宙学效应对距离的影响。&lt;br /&gt;
&lt;br /&gt;
== 官方解答 ==&lt;br /&gt;
&lt;br /&gt;
{{由ai生成}}&lt;br /&gt;
&lt;br /&gt;
根据维里定理，总引力势能\(U\)和动能\(K\)满足：&lt;br /&gt;
$$U + 2K = 0$$&lt;br /&gt;
&lt;br /&gt;
考虑星系平均质量\(\langle m\rangle = M_T/N\)，动能可近似为：&lt;br /&gt;
$$K = \frac{1}{2}M_T\sigma_v^2$$&lt;br /&gt;
&lt;br /&gt;
红移弥散对应的径向速度弥散：&lt;br /&gt;
$$\sigma_{v_r} = c\cdot\sigma_z = 2.998 \times 10^8 \, \text{m/s} \times 0.0005 = 1.499 \times 10^5 \, \text{m/s}$$&lt;br /&gt;
&lt;br /&gt;
假设速度各向同性，三维速度弥散：&lt;br /&gt;
$$\sigma_v^2 = 3\sigma_{v_r}^2$$&lt;br /&gt;
&lt;br /&gt;
星系团半径估算：&lt;br /&gt;
$$R = \frac{D_A \cdot \Delta\theta}{2} = \frac{1500 \times 10^6 \times 206265 \times 1.496 \times 10^{11} \times 10^{-2}}{2} = 2.3143 \times 10^{23} \, \text{m}$$&lt;br /&gt;
&lt;br /&gt;
均匀球体引力势能：&lt;br /&gt;
$$U = -\frac{3}{5}\frac{GM_T^2}{R}$$&lt;br /&gt;
&lt;br /&gt;
代入维里定理得质量公式：&lt;br /&gt;
$$M_T = \frac{5R\sigma_{v_r}^2}{G} = \frac{5 \times 2.314 \times 10^{23} \times (1.499 \times 10^5)^2}{6.67 \times 10^{-11}} \, \text{kg}$$&lt;br /&gt;
&lt;br /&gt;
计算结果：&lt;br /&gt;
$$M_T \approx 2.0 \times 10^{14} \, M_\odot$$&lt;br /&gt;
&lt;br /&gt;
[[分类:宇宙学]]&lt;br /&gt;
[[分类:天体力学]]&lt;br /&gt;
[[分类:由ai生成]]&lt;/div&gt;</summary>
		<author><name>Quan787</name></author>
		
	</entry>
	<entry>
		<id>https://www.astro-init.top/index.php?title=%E5%88%86%E7%B1%BB:%E7%94%B1ai%E7%94%9F%E6%88%90&amp;diff=2716</id>
		<title>分类:由ai生成</title>
		<link rel="alternate" type="text/html" href="https://www.astro-init.top/index.php?title=%E5%88%86%E7%B1%BB:%E7%94%B1ai%E7%94%9F%E6%88%90&amp;diff=2716"/>
		<updated>2025-03-05T16:01:02Z</updated>

		<summary type="html">&lt;p&gt;Quan787：创建页面，内容为“以下是由ai从pdf中提取题目和答案生成的页面。目前ai的工作只限于翻译题目和官方答案，并不会给出自己的答案。如果你认…”&lt;/p&gt;
&lt;hr /&gt;
&lt;div&gt;以下是由ai从pdf中提取题目和答案生成的页面。目前ai的工作只限于翻译题目和官方答案，并不会给出自己的答案。如果你认为ai的翻译或格式有问题，请在评论区提出或联系管理员。&lt;br /&gt;
&lt;br /&gt;
经过用户校对后，可以去掉页面上的这个分类标记。&lt;/div&gt;</summary>
		<author><name>Quan787</name></author>
		
	</entry>
	<entry>
		<id>https://www.astro-init.top/index.php?title=%E6%96%87%E4%BB%B6:IOAA2024T2-1.jpg&amp;diff=2715</id>
		<title>文件:IOAA2024T2-1.jpg</title>
		<link rel="alternate" type="text/html" href="https://www.astro-init.top/index.php?title=%E6%96%87%E4%BB%B6:IOAA2024T2-1.jpg&amp;diff=2715"/>
		<updated>2025-03-05T15:56:03Z</updated>

		<summary type="html">&lt;p&gt;Quan787：&lt;/p&gt;
&lt;hr /&gt;
&lt;div&gt;&lt;/div&gt;</summary>
		<author><name>Quan787</name></author>
		
	</entry>
	<entry>
		<id>https://www.astro-init.top/index.php?title=2024%E5%B9%B4IOAA%E7%90%86%E8%AE%BA%E7%AC%AC2%E9%A2%98-%E6%98%9F%E7%B3%BB%E5%9B%A2&amp;diff=2714</id>
		<title>2024年IOAA理论第2题-星系团</title>
		<link rel="alternate" type="text/html" href="https://www.astro-init.top/index.php?title=2024%E5%B9%B4IOAA%E7%90%86%E8%AE%BA%E7%AC%AC2%E9%A2%98-%E6%98%9F%E7%B3%BB%E5%9B%A2&amp;diff=2714"/>
		<updated>2025-03-05T15:54:41Z</updated>

		<summary type="html">&lt;p&gt;Quan787：创建页面，内容为“==英文题目==  {{由ai生成}}  '''2. Galaxy Cluster (10 p)'''  An astrophysical survey mapped all the galaxies in a small region of the sky, of angular diameter…”&lt;/p&gt;
&lt;hr /&gt;
&lt;div&gt;==英文题目==&lt;br /&gt;
&lt;br /&gt;
{{由ai生成}}&lt;br /&gt;
&lt;br /&gt;
'''2. Galaxy Cluster (10 p)'''&lt;br /&gt;
&lt;br /&gt;
An astrophysical survey mapped all the galaxies in a small region of the sky, of angular diameter $$\Delta \theta = 0.01 \text{ rad}$$, where many galaxies seemed to be concentrated around the central area of the image. [[文件:IOAA2024T2-1.jpg|缩略图|居中|图一]]&lt;br /&gt;
&lt;br /&gt;
When the positions and redshifts of all the galaxies in this cluster were measured, an interesting distribution emerged, which is shown in the plot above.&lt;br /&gt;
&lt;br /&gt;
Using these observations, estimate the total mass of the galaxy cluster and express your answer in solar masses. Assume that this galaxy cluster is in dynamical equilibrium, with a root-mean-square redshift dispersion $$\sigma_z \approx 0.0005$$. Consider that the distance corresponding to $$\bar{z} = 0.7$$ in the standard cosmological model is $$D_A = 1500 \text{ Mpc}$$. Ignore cosmological effects on the distance.&lt;br /&gt;
&lt;br /&gt;
==中文翻译==&lt;br /&gt;
&lt;br /&gt;
{{由ai生成}}&lt;br /&gt;
&lt;br /&gt;
'''2. 星系团 (10 分)'''&lt;br /&gt;
&lt;br /&gt;
一项天体物理调查绘制了天空中一小区域内所有星系的分布图，该区域的角直径为 $$\Delta \theta = 0.01 \text{ rad}$$，许多星系似乎集中在图像中央区域。[[文件:IOAA2024T2-1.jpg|缩略图|居中|图一]]&lt;br /&gt;
&lt;br /&gt;
当测量了该星系团内所有星系的位置和红移后，出现了一个有趣的分布，如上图所示。&lt;br /&gt;
&lt;br /&gt;
利用这些观测结果，估算该星系团的总质量，并将答案以太阳质量为单位给出。假设该星系团处于动力学平衡状态，其红移的均方根离散值为 $$\sigma_z \approx 0.0005$$。考虑在标准宇宙学模型中，对应于 $$\bar{z} = 0.7$$ 的距离为 $$D_A = 1500 \text{ Mpc}$$。忽略距离上的宇宙学效应。&lt;br /&gt;
&lt;br /&gt;
== 官方解答 ==&lt;br /&gt;
&lt;br /&gt;
{{由ai生成}}&lt;br /&gt;
&lt;br /&gt;
利用星系团总引力势能 $$U$$ 与总动能 $$K$$ 的关系，根据维里定理有&lt;br /&gt;
$$&lt;br /&gt;
U = -2K.&lt;br /&gt;
$$&lt;br /&gt;
设星系团中有 $$N$$ 个星系，每个星系质量为 $$m_i$$，其相对于团整体运动 $$\vec{v}_0$$ 的速度为 $$\vec{v}_i$$，则总动能可估算为&lt;br /&gt;
$$&lt;br /&gt;
K = \frac{1}{2} \sum_{i=1}^{N} m_i v_i^2 \approx \frac{1}{2} M_T \sigma_v^2,&lt;br /&gt;
$$&lt;br /&gt;
其中 $$M_T$$ 为星系团总质量，$$\sigma_v$$ 为速度弥散度。由于仅测得径向速度离散度，令&lt;br /&gt;
$$&lt;br /&gt;
\sigma_{vr} \approx c\,\sigma_z \approx 1.5\times10^5 \text{ m/s},&lt;br /&gt;
$$&lt;br /&gt;
在三维各向同性假设下有&lt;br /&gt;
$$&lt;br /&gt;
\sigma_v^2 = 3\sigma_{vr}^2.&lt;br /&gt;
$$&lt;br /&gt;
&lt;br /&gt;
另一方面，假设星系团的质量分布近似均匀且呈球形，其引力势能可估算为&lt;br /&gt;
$$&lt;br /&gt;
U = -\frac{3}{5}\frac{GM_T^2}{R},&lt;br /&gt;
$$&lt;br /&gt;
其中半径 $$R$$ 近似为&lt;br /&gt;
$$&lt;br /&gt;
R \approx D_A\,\Delta \theta.&lt;br /&gt;
$$&lt;br /&gt;
&lt;br /&gt;
将以上表达式代入维里定理可得&lt;br /&gt;
$$&lt;br /&gt;
M_T \approx \frac{5R\,\sigma_v^2}{G}.&lt;br /&gt;
$$&lt;br /&gt;
&lt;br /&gt;
代入 $$R \approx 1500 \text{ Mpc} \times 0.01$$（注意单位换算）和 $$\sigma_v \approx \sqrt{3}\times1.5\times10^5 \text{ m/s}$$，可估算星系团总质量约为 $$10^{14}$$ 太阳质量。&lt;br /&gt;
&lt;br /&gt;
[[分类:天体力学]]&lt;br /&gt;
[[分类:宇宙学]]&lt;br /&gt;
[[分类:由ai生成]]&lt;/div&gt;</summary>
		<author><name>Quan787</name></author>
		
	</entry>
	<entry>
		<id>https://www.astro-init.top/index.php?title=IOAA2024&amp;diff=2713</id>
		<title>IOAA2024</title>
		<link rel="alternate" type="text/html" href="https://www.astro-init.top/index.php?title=IOAA2024&amp;diff=2713"/>
		<updated>2025-03-05T15:54:26Z</updated>

		<summary type="html">&lt;p&gt;Quan787：创建页面，内容为“==理论考试==  2024年IOAA理论第2题-星系团质量估算”&lt;/p&gt;
&lt;hr /&gt;
&lt;div&gt;==理论考试==&lt;br /&gt;
&lt;br /&gt;
[[2024年IOAA理论第2题-星系团质量估算]]&lt;/div&gt;</summary>
		<author><name>Quan787</name></author>
		
	</entry>
	<entry>
		<id>https://www.astro-init.top/index.php?title=%E6%A8%A1%E6%9D%BF:%E7%94%B1ai%E7%94%9F%E6%88%90&amp;diff=2712</id>
		<title>模板:由ai生成</title>
		<link rel="alternate" type="text/html" href="https://www.astro-init.top/index.php?title=%E6%A8%A1%E6%9D%BF:%E7%94%B1ai%E7%94%9F%E6%88%90&amp;diff=2712"/>
		<updated>2025-03-05T12:38:51Z</updated>

		<summary type="html">&lt;p&gt;Quan787：创建页面，内容为“&amp;lt;table bgcolor={{{1|cyan}}} border=1&amp;gt; &amp;lt;tr width=100%&amp;gt; &amp;lt;td width=100%&amp;gt; '''本章节由AI生成''' &amp;lt;/td&amp;gt; &amp;lt;tr&amp;gt; &amp;lt;/table&amp;gt;”&lt;/p&gt;
&lt;hr /&gt;
&lt;div&gt;&amp;lt;table bgcolor={{{1|cyan}}} border=1&amp;gt;&lt;br /&gt;
&amp;lt;tr width=100%&amp;gt;&lt;br /&gt;
&amp;lt;td width=100%&amp;gt;&lt;br /&gt;
'''本章节由AI生成'''&lt;br /&gt;
&amp;lt;/td&amp;gt;&lt;br /&gt;
&amp;lt;tr&amp;gt;&lt;br /&gt;
&amp;lt;/table&amp;gt;&lt;/div&gt;</summary>
		<author><name>Quan787</name></author>
		
	</entry>
	<entry>
		<id>https://www.astro-init.top/index.php?title=2019%E5%B9%B4IOAA%E7%90%86%E8%AE%BA%E7%AC%AC5%E9%A2%98-CMB%E7%83%A4%E7%AE%B1&amp;diff=2711</id>
		<title>2019年IOAA理论第5题-CMB烤箱</title>
		<link rel="alternate" type="text/html" href="https://www.astro-init.top/index.php?title=2019%E5%B9%B4IOAA%E7%90%86%E8%AE%BA%E7%AC%AC5%E9%A2%98-CMB%E7%83%A4%E7%AE%B1&amp;diff=2711"/>
		<updated>2025-03-05T11:50:56Z</updated>

		<summary type="html">&lt;p&gt;Quan787：&lt;/p&gt;
&lt;hr /&gt;
&lt;div&gt;{{需要解答}}&lt;br /&gt;
&lt;br /&gt;
==英文题目==&lt;br /&gt;
&lt;br /&gt;
'''5. Cosmic Microwave Background Oven (10 p)'''&lt;br /&gt;
&lt;br /&gt;
Since the human body is made mostly of water, it is very efficient at absorbing microwave photons.&lt;br /&gt;
&lt;br /&gt;
Assume that an astronaut’s body is a perfect spherical absorber with mass of $$𝑚 = 60 kg$$, and its&lt;br /&gt;
average density and heat capacity are the same as for pure water, i.e. $$𝜌 = 1000 kg \ m^{−3}$$ and $$𝐶 =&lt;br /&gt;
4200 J kg^{−1} K^{−1}$$.&lt;br /&gt;
&lt;br /&gt;
a) What is the approximate rate, in watts, at which an astronaut in intergalactic space would absorb&lt;br /&gt;
radiative energy from the Cosmic Microwave Background (CMB)? The spectral energy&lt;br /&gt;
distribution of CMB can be approximated by blackbody radiation of temperature $$𝑇_{CMB} =&lt;br /&gt;
2.728 K$$. (5 p)&lt;br /&gt;
&lt;br /&gt;
b) Approximately how many CMB photons per second would the astronaut absorb? (3 p)&lt;br /&gt;
&lt;br /&gt;
c) Ignoring other energy inputs and outputs, how long would it take for the CMB to raise the&lt;br /&gt;
astronaut’s temperature by $$\Delta 𝑇 = 1 K$$? (2 p)&lt;br /&gt;
&lt;br /&gt;
==中文题目==&lt;br /&gt;
&lt;br /&gt;
'''5.宇宙微波背景烤箱（10 p）'''&lt;br /&gt;
&lt;br /&gt;
由于人体主要由水构成，因此在吸收微波光子方面非常高效。&lt;br /&gt;
&lt;br /&gt;
假设宇航员的身体是一个完美的球形吸收体，质量$$𝑚= 60 kg$$，其平均密度和热容量与纯水相同，即$$𝜌 = 1000 kg \ m^{−3}$$ 和 $$𝐶 =&lt;br /&gt;
4200 J kg^{−1} K^{−1}$$.&lt;br /&gt;
&lt;br /&gt;
a）星系际空间中的宇航员从宇宙微波背景（CMB）吸收辐射能量的大致速率（以瓦为单位）是多少？ CMB的光谱能量分布可通过温度为$$𝑇_{CMB}= 2.728 K$$的黑体辐射来近似。（5 p）&lt;br /&gt;
&lt;br /&gt;
b）宇航员每秒大约吸收多少个CMB光子？ （3 p）&lt;br /&gt;
&lt;br /&gt;
c）忽略其他能量输入和输出，CMB将宇航员的温度提高$$Δ𝑇= 1 K$$需要多长时间？ （2 p）&lt;br /&gt;
&lt;br /&gt;
&lt;br /&gt;
== 解答 ==&lt;br /&gt;
a)CMB的辐射功率满足斯特藩—玻尔兹曼定律&lt;br /&gt;
&lt;br /&gt;
$$P=S\sigma T^4$$&lt;br /&gt;
&lt;br /&gt;
其中P表示接收到辐射的功率，σ表示斯特藩—玻尔兹曼常量，S为接收面积，T为辐射源温度。&lt;br /&gt;
&lt;br /&gt;
根据人体质量密度，可求出这位球形老哥的半径为&lt;br /&gt;
&lt;br /&gt;
R=0.24m&lt;br /&gt;
&lt;br /&gt;
因此其表面积为&lt;br /&gt;
&lt;br /&gt;
$$S=4πR^2 m^2$$&lt;br /&gt;
&lt;br /&gt;
代入数据计算&lt;br /&gt;
&lt;br /&gt;
可得$$P=3.1x10^-6W$$&lt;br /&gt;
&lt;br /&gt;
&lt;br /&gt;
[[分类:热学]]&lt;/div&gt;</summary>
		<author><name>Quan787</name></author>
		
	</entry>
	<entry>
		<id>https://www.astro-init.top/index.php?title=2019%E5%B9%B4IOAA%E7%90%86%E8%AE%BA%E7%AC%AC5%E9%A2%98-CMB%E7%83%A4%E7%AE%B1&amp;diff=2710</id>
		<title>2019年IOAA理论第5题-CMB烤箱</title>
		<link rel="alternate" type="text/html" href="https://www.astro-init.top/index.php?title=2019%E5%B9%B4IOAA%E7%90%86%E8%AE%BA%E7%AC%AC5%E9%A2%98-CMB%E7%83%A4%E7%AE%B1&amp;diff=2710"/>
		<updated>2025-03-05T11:49:23Z</updated>

		<summary type="html">&lt;p&gt;Quan787：&lt;/p&gt;
&lt;hr /&gt;
&lt;div&gt;{{需要解答}}&lt;br /&gt;
&lt;br /&gt;
==英文题目==&lt;br /&gt;
&lt;br /&gt;
'''5. Cosmic Microwave Background Oven (10 p)'''&lt;br /&gt;
&lt;br /&gt;
Since the human body is made mostly of water, it is very efficient at absorbing microwave photons.&lt;br /&gt;
&lt;br /&gt;
Assume that an astronaut’s body is a perfect spherical absorber with mass of $$𝑚 = 60 kg$$, and its&lt;br /&gt;
average density and heat capacity are the same as for pure water, i.e. $$𝜌 = 1000 kg \ m^{−3}$$ and $$𝐶 =&lt;br /&gt;
4200 J kg^{−1} K^{−1}$$.&lt;br /&gt;
&lt;br /&gt;
a) What is the approximate rate, in watts, at which an astronaut in intergalactic space would absorb&lt;br /&gt;
radiative energy from the Cosmic Microwave Background (CMB)? The spectral energy&lt;br /&gt;
distribution of CMB can be approximated by blackbody radiation of temperature $$𝑇_{CMB} =&lt;br /&gt;
2.728 K$$. (5 p)&lt;br /&gt;
&lt;br /&gt;
b) Approximately how many CMB photons per second would the astronaut absorb? (3 p)&lt;br /&gt;
&lt;br /&gt;
c) Ignoring other energy inputs and outputs, how long would it take for the CMB to raise the&lt;br /&gt;
astronaut’s temperature by $$Δ𝑇 = 1 K$$? (2 p)&lt;br /&gt;
&lt;br /&gt;
==中文题目==&lt;br /&gt;
&lt;br /&gt;
'''5.宇宙微波背景烤箱（10 p）'''&lt;br /&gt;
&lt;br /&gt;
由于人体主要由水构成，因此在吸收微波光子方面非常高效。&lt;br /&gt;
&lt;br /&gt;
假设宇航员的身体是一个完美的球形吸收体，质量$$𝑚= 60 kg$$，其平均密度和热容量与纯水相同，即$$𝜌 = 1000 kg \ m^{−3}$$ 和 $$𝐶 =&lt;br /&gt;
4200 J kg^{−1} K^{−1}$$.&lt;br /&gt;
&lt;br /&gt;
a）星系际空间中的宇航员从宇宙微波背景（CMB）吸收辐射能量的大致速率（以瓦为单位）是多少？ CMB的光谱能量分布可通过温度为$$𝑇_{CMB}= 2.728 K$$的黑体辐射来近似。（5 p）&lt;br /&gt;
&lt;br /&gt;
b）宇航员每秒大约吸收多少个CMB光子？ （3 p）&lt;br /&gt;
&lt;br /&gt;
c）忽略其他能量输入和输出，CMB将宇航员的温度提高$$Δ𝑇= 1 K$$需要多长时间？ （2 p）&lt;br /&gt;
&lt;br /&gt;
&amp;lt;br /&amp;gt;&lt;br /&gt;
&lt;br /&gt;
== 解答 ==&lt;br /&gt;
a)CMB的辐射功率满足斯特藩—玻尔兹曼定律&lt;br /&gt;
&lt;br /&gt;
$$P=S\sigma T^4$$&lt;br /&gt;
&lt;br /&gt;
其中P表示接收到辐射的功率，σ表示斯特藩—玻尔兹曼常量，S为接收面积，T为辐射源温度。&lt;br /&gt;
&lt;br /&gt;
根据人体质量密度，可求出这位球形老哥的半径为&lt;br /&gt;
&lt;br /&gt;
R=0.24m&lt;br /&gt;
&lt;br /&gt;
因此其表面积为&lt;br /&gt;
&lt;br /&gt;
$$S=4πR^2 m^2$$&lt;br /&gt;
&lt;br /&gt;
代入数据计算&lt;br /&gt;
&lt;br /&gt;
可得$$P=3.1x10^-6W$$&lt;br /&gt;
&lt;br /&gt;
、&lt;br /&gt;
&lt;br /&gt;
，&lt;br /&gt;
&amp;lt;br /&amp;gt;&lt;/div&gt;</summary>
		<author><name>Quan787</name></author>
		
	</entry>
	<entry>
		<id>https://www.astro-init.top/index.php?title=%E7%94%A8%E6%88%B7:Quan787&amp;diff=2476</id>
		<title>用户:Quan787</title>
		<link rel="alternate" type="text/html" href="https://www.astro-init.top/index.php?title=%E7%94%A8%E6%88%B7:Quan787&amp;diff=2476"/>
		<updated>2023-05-22T05:58:50Z</updated>

		<summary type="html">&lt;p&gt;Quan787：&lt;/p&gt;
&lt;hr /&gt;
&lt;div&gt; There's a moment...&lt;br /&gt;
[[倡议]]&amp;lt;br /&amp;gt;&lt;br /&gt;
[[文件:Icon-above-font.png|居中|缩略图|Astro-init的第一个logo]]&lt;br /&gt;
&lt;br /&gt;
&amp;lt;small&amp;gt;我再次以个人名义向参与网站建设的各位致以最高的谢意。整件事情从头至尾都不会容易，从网站框架的搭建，到规则的设立，再到内容的充实。拭目以待。&amp;lt;/small&amp;gt;&lt;br /&gt;
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 这篇文章的内容来自astro-init.top。Astro-init是一个初创网站，旨在收集各种天文奥赛的题目、解答和相关信息。网站的内容来自奥赛选手们的共同努力，如果你也想参与其中，请联系我们。&lt;/div&gt;</summary>
		<author><name>Quan787</name></author>
		
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	<entry>
		<id>https://www.astro-init.top/index.php?title=%E7%94%A8%E6%88%B7:Quan787&amp;diff=2475</id>
		<title>用户:Quan787</title>
		<link rel="alternate" type="text/html" href="https://www.astro-init.top/index.php?title=%E7%94%A8%E6%88%B7:Quan787&amp;diff=2475"/>
		<updated>2023-05-22T05:58:37Z</updated>

		<summary type="html">&lt;p&gt;Quan787：&lt;/p&gt;
&lt;hr /&gt;
&lt;div&gt; There's a moment...&lt;br /&gt;
[[倡议]]&amp;lt;br /&amp;gt;&lt;br /&gt;
[[文件:Icon-above-font.png|居中|缩略图|Astro-init的第一个logo]]&lt;br /&gt;
&lt;br /&gt;
&amp;lt;small&amp;gt;我再次以个人名义向参与网站建设的各位致以最高的谢意。整件事情从头至尾都不会容易，从网站框架的搭建，到规则的设立，再到内容的充实。拭目以待。&amp;lt;/small&amp;gt;&lt;br /&gt;
----&lt;br /&gt;
&lt;br /&gt;
====== 杂物箱 ======&lt;br /&gt;
[[模板:本周关注]] &lt;br /&gt;
[[模板:赛事列表]] [[模板:外国赛事]][[模板:省级竞赛]]&lt;br /&gt;
[[模板:常用链接]] &lt;br /&gt;
[[模板:宣传信息]] &lt;br /&gt;
[[模板:首页彩蛋]]&lt;br /&gt;
&lt;br /&gt;
[[特殊:未分类页面]]&lt;br /&gt;
[[特殊:孤立页面]]&lt;br /&gt;
&lt;br /&gt;
[[特殊:用户权限]]&lt;br /&gt;
[[特殊:特殊:EditAccount]]&lt;br /&gt;
[[特殊:合并用户]]&lt;br /&gt;
 这篇文章的内容来自astro-init.top。Astro-init是一个初创网站，旨在收集各种天文奥赛的题目、解答和相关信息。网站的内容来自奥赛选手们的共同努力，如果你也想参与其中，请联系我们。&lt;/div&gt;</summary>
		<author><name>Quan787</name></author>
		
	</entry>
	<entry>
		<id>https://www.astro-init.top/index.php?title=%E7%94%A8%E6%88%B7:Quan787&amp;diff=2474</id>
		<title>用户:Quan787</title>
		<link rel="alternate" type="text/html" href="https://www.astro-init.top/index.php?title=%E7%94%A8%E6%88%B7:Quan787&amp;diff=2474"/>
		<updated>2023-05-22T05:57:57Z</updated>

		<summary type="html">&lt;p&gt;Quan787：&lt;/p&gt;
&lt;hr /&gt;
&lt;div&gt; There's a moment...&lt;br /&gt;
[[倡议]]&amp;lt;br /&amp;gt;&lt;br /&gt;
[[文件:Icon-above-font.png|居中|缩略图|Astro-init的第一个logo]]&lt;br /&gt;
&lt;br /&gt;
&amp;lt;small&amp;gt;我再次以个人名义向参与网站建设的各位致以最高的谢意。整件事情从头至尾都不会容易，从网站框架的搭建，到规则的设立，再到内容的充实。拭目以待。&amp;lt;/small&amp;gt;&lt;br /&gt;
----&lt;br /&gt;
&lt;br /&gt;
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 这篇文章的内容来自astro-init.top。Astro-init是一个初创网站，旨在收集各种天文奥赛的题目、解答和相关信息。网站的内容来自奥赛选手们的共同努力，如果你也想参与其中，请联系我们。&lt;/div&gt;</summary>
		<author><name>Quan787</name></author>
		
	</entry>
	<entry>
		<id>https://www.astro-init.top/index.php?title=%E6%A8%A1%E6%9D%BF:%E7%94%A8%E6%88%B7%E7%AD%94%E6%A1%88&amp;diff=2297</id>
		<title>模板:用户答案</title>
		<link rel="alternate" type="text/html" href="https://www.astro-init.top/index.php?title=%E6%A8%A1%E6%9D%BF:%E7%94%A8%E6%88%B7%E7%AD%94%E6%A1%88&amp;diff=2297"/>
		<updated>2022-05-06T20:28:57Z</updated>

		<summary type="html">&lt;p&gt;Quan787：&lt;/p&gt;
&lt;hr /&gt;
&lt;div&gt;&amp;lt;table bgcolor=#90EE90 border=1 width=100%&amp;gt;&lt;br /&gt;
&amp;lt;tr &amp;gt;&lt;br /&gt;
&amp;lt;td width=5% &amp;gt;&lt;br /&gt;
&amp;lt;center&amp;gt;&amp;lt;big&amp;gt;❤&amp;lt;/big&amp;gt;&amp;lt;/center&amp;gt;&lt;br /&gt;
&amp;lt;/td&amp;gt;&lt;br /&gt;
&amp;lt;td width=75%&amp;gt;&lt;br /&gt;
'''用户答案'''&lt;br /&gt;
贡献者：{{{1|请查询编辑记录}}}&lt;br /&gt;
&amp;lt;/td&amp;gt;&lt;br /&gt;
&amp;lt;tr&amp;gt;&lt;br /&gt;
&amp;lt;/table&amp;gt;&lt;/div&gt;</summary>
		<author><name>Quan787</name></author>
		
	</entry>
	<entry>
		<id>https://www.astro-init.top/index.php?title=%E6%A8%A1%E6%9D%BF:%E7%94%A8%E6%88%B7%E7%AD%94%E6%A1%88&amp;diff=2296</id>
		<title>模板:用户答案</title>
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		<updated>2022-05-06T20:27:03Z</updated>

		<summary type="html">&lt;p&gt;Quan787：&lt;/p&gt;
&lt;hr /&gt;
&lt;div&gt;&amp;lt;table bgcolor='Olive' border=1 width=100%&amp;gt;&lt;br /&gt;
&amp;lt;tr &amp;gt;&lt;br /&gt;
&amp;lt;td width=5% &amp;gt;&lt;br /&gt;
&amp;lt;center&amp;gt;&amp;lt;big&amp;gt;❤&amp;lt;/big&amp;gt;&amp;lt;/center&amp;gt;&lt;br /&gt;
&amp;lt;/td&amp;gt;&lt;br /&gt;
&amp;lt;td width=75%&amp;gt;&lt;br /&gt;
'''用户答案'''&lt;br /&gt;
贡献者：{{{1|请查询编辑记录}}}&lt;br /&gt;
&amp;lt;/td&amp;gt;&lt;br /&gt;
&amp;lt;tr&amp;gt;&lt;br /&gt;
&amp;lt;/table&amp;gt;&lt;/div&gt;</summary>
		<author><name>Quan787</name></author>
		
	</entry>
	<entry>
		<id>https://www.astro-init.top/index.php?title=%E6%A8%A1%E6%9D%BF:%E7%94%A8%E6%88%B7%E7%AD%94%E6%A1%88&amp;diff=2295</id>
		<title>模板:用户答案</title>
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		<updated>2022-05-06T20:26:16Z</updated>

		<summary type="html">&lt;p&gt;Quan787：&lt;/p&gt;
&lt;hr /&gt;
&lt;div&gt;&amp;lt;table bgcolor='Olive' border=1 width=100%&amp;gt;&lt;br /&gt;
&amp;lt;tr &amp;gt;&lt;br /&gt;
&amp;lt;td width=5% &amp;gt;&lt;br /&gt;
&amp;lt;center&amp;gt;&amp;lt;big&amp;gt;❤&amp;lt;/big&amp;gt;&amp;lt;/center&amp;gt;&lt;br /&gt;
&amp;lt;/td&amp;gt;&lt;br /&gt;
&amp;lt;td width=75%&amp;gt;&lt;br /&gt;
'''用户答案'''&lt;br /&gt;
贡献者：{{{1}}}&lt;br /&gt;
&amp;lt;/td&amp;gt;&lt;br /&gt;
&amp;lt;tr&amp;gt;&lt;br /&gt;
&amp;lt;/table&amp;gt;&lt;/div&gt;</summary>
		<author><name>Quan787</name></author>
		
	</entry>
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