| 引用本文: | 肖齐英,黄教民,王正志,等.登月探测器轨道计算的自动寻优设计.[J].国防科技大学学报,1996,18(4):36-39.[点击复制] |
| Xiao Qiying,Huang Jiaomin,Wang Zhengzhi,et al.Calculation of the Automatical Optimizing Trajectory of Lunar Prober[J].Journal of National University of Defense Technology,1996,18(4):36-39[点击复制] |
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| 登月探测器轨道计算的自动寻优设计 |
| 肖齐英1, 黄教民1, 王正志1, 李明强2 |
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(1.国防科技大学 自动控制系 湖南 长沙 410073;2.北京仿真中心)
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| 摘要: |
| 研究探测器从停泊轨道出发飞向月球并击中月球的轨道自动寻优设计问题。着重讨论登月轨道计算的自动寻优设计。最后给出实验结果。 |
| 关键词: 登月探测器，标准轨道，自动寻优，瞄准角 |
| DOI： |
| 投稿日期：1996-04-25 |
| 基金项目: |
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| Calculation of the Automatical Optimizing Trajectory of Lunar Prober |
| Xiao Qiying1, Huang Jiaomin1, Wang Zhengzhi1, Li Mingqiang2 |
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(1.Department of Automatic Control，NUDT，Changsha，410073;2.Beijing Simulation Center)
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| Abstract: |
| The purpose of this paper is to solve the problem of designing optimized trajectory, based on the task that the prober is launched from the anchorage orbit and lands on the moon. This paper emphasizingly discusses the design of automatical optimizing trajectory calculation of lunar prober. Finallly, simulation results show good standard trajectory. |
| Keywords: lunar prober, standard trajectory, automatical optimizing, aiming angle |
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