CN116880528A - 一种登月航天器着陆控制方法、装置及设备 - Google Patents
一种登月航天器着陆控制方法、装置及设备 Download PDFInfo
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Citations (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPH04108099A (ja) * | 1990-08-29 | 1992-04-09 | Mitsubishi Electric Corp | 宇宙機の着陸誘導制御装置 |
CN107885082A (zh) * | 2017-11-13 | 2018-04-06 | 浙江大学 | 一种基于正交配置优化的月球着陆器轨迹控制器 |
CN109211246A (zh) * | 2018-11-07 | 2019-01-15 | 北京理工大学 | 不确定环境下行星着陆轨迹规划方法 |
CN109506662A (zh) * | 2018-10-30 | 2019-03-22 | 北京控制工程研究所 | 一种小天体着陆初始对准方法、其相对导航基准确定方法及装置 |
CN111537000A (zh) * | 2020-06-08 | 2020-08-14 | 中国科学院微小卫星创新研究院 | 深空小天体着陆段光学导航算法的地面验证系统及方法 |
CN114132530A (zh) * | 2021-09-17 | 2022-03-04 | 北京空间飞行器总体设计部 | 一种基于触地关机的地外天体安全软着陆方法 |
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- 2023-07-24 CN CN202310907657.5A patent/CN116880528B/zh active Active
Patent Citations (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPH04108099A (ja) * | 1990-08-29 | 1992-04-09 | Mitsubishi Electric Corp | 宇宙機の着陸誘導制御装置 |
CN107885082A (zh) * | 2017-11-13 | 2018-04-06 | 浙江大学 | 一种基于正交配置优化的月球着陆器轨迹控制器 |
CN109506662A (zh) * | 2018-10-30 | 2019-03-22 | 北京控制工程研究所 | 一种小天体着陆初始对准方法、其相对导航基准确定方法及装置 |
CN109211246A (zh) * | 2018-11-07 | 2019-01-15 | 北京理工大学 | 不确定环境下行星着陆轨迹规划方法 |
CN111537000A (zh) * | 2020-06-08 | 2020-08-14 | 中国科学院微小卫星创新研究院 | 深空小天体着陆段光学导航算法的地面验证系统及方法 |
CN114132530A (zh) * | 2021-09-17 | 2022-03-04 | 北京空间飞行器总体设计部 | 一种基于触地关机的地外天体安全软着陆方法 |
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