| 引用本文: | 贺波勇,李海阳,沈红新,等.载人登月着陆窗口与定点返回轨道耦合设计.[J].国防科技大学学报,2017,39(1):11-16.[点击复制] |
| HE Boyong,LI Haiyang,SHEN Hongxin,et al.Coupled design of landing window and point return orbit for manned lunar landing mission[J].Journal of National University of Defense Technology,2017,39(1):11-16[点击复制] |
|
| |
|
|
| 本文已被：浏览 9605次 下载 6438次 |
| 载人登月着陆窗口与定点返回轨道耦合设计 |
| 贺波勇1, 李海阳1, 沈红新2, 彭祺擘3 |
|
(1.国防科技大学 航天科学与工程学院， 湖南 长沙 410073;2.西安卫星测控中心， 陕西 西安 710043;3.载人航天总体研究论证中心， 北京 100094)
|
| 摘要: |
| 对于月面中高纬度着陆且定点返回地球中高纬度着陆场的载人登月任务而言，月面着陆窗口与定点返回轨道设计存在耦合关系，这是工程任务面对的关键技术之一。针对任务背景及约束条件，建立月面着陆窗口与定点返回轨道求解数学模型；通过数值求解着陆窗口与返回轨道参数规律，并从空间几何关系分析耦合机理；以2025年载人月面虹湾探测为例，给出了着陆窗口与定点返回轨道求解流程及验证算例。计算结果经商业软件STK校验正确，表明该方法是一种简捷精确的载人登月任务规划方法，可在未来载人登月工程任务规划时直接使用。 |
| 关键词: 载人登月 着陆窗口 定点返回 轨道设计 |
| DOI：10.11887/j.cn.201701003 |
| 投稿日期：2015-09-11 |
| 基金项目:国家自然科学基金资助项目(11372345,11402295);国家重点基础研究发展计划资助项目(2013CB733100) |
|
| Coupled design of landing window and point return orbit for manned lunar landing mission |
| HE Boyong1, LI Haiyang1, SHEN Hongxin2, PENG Qibo3 |
|
(1. College of Aerospace Science and Engineering, National University of Defense Technology, Changsha 410073, China;2. Xi′an Satellite Control Center, Xi′an 710043, China;3. Manned Space System Research Center, Beijing 100094, China)
|
| Abstract: |
| For the manned lunar landing mission that lands on the moon high latitude destination and returns to earth high latitude recovery field, a design of moon landing window and point return orbit is coupled in complexity, so it is one of the key technologies in the engineering task. In view to task demands and engineering constraints, the mathematical models for finding lands window and designing point return orbit were established in the first place; Secondly, by solving the rules of landing window and point return orbit parameters, the coupled geometrical principle was analyzed; Taking a mission that lands on Sinus Iridium in 2025 for example, the strategy of coupled design landing window and the point return orbit were given, which was provided by validation example. The verification by commercial Software STK(system tool kits, by AGI company) of simulation results is correct, the proposed strategy is a simple and precise method for planning manned lunar landing mission, which can be used in the future manned lunar landing mission directly. |
| Keywords: manned lunar landing landing window point return orbit design |
|
|
|
|
|
