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旋转非合作目标终端逼近的姿轨控制研究

刘海龙 韩旭 史小平

刘海龙, 韩旭, 史小平. 旋转非合作目标终端逼近的姿轨控制研究[J]. 空间科学学报, 2015, 35(5): 603-610. doi: 10.11728/cjss2015.05.603
引用本文: 刘海龙, 韩旭, 史小平. 旋转非合作目标终端逼近的姿轨控制研究[J]. 空间科学学报, 2015, 35(5): 603-610. doi: 10.11728/cjss2015.05.603
LIU Hailong, HAN Xu, SHI Xiaoping. Attitude And Translation Control For Spacecraft To Approach To A Tumbling Non-Cooperative Object During The Final Phase[J]. Journal of Space Science, 2015, 35(5): 603-610. doi: 10.11728/cjss2015.05.603
Citation: LIU Hailong, HAN Xu, SHI Xiaoping. Attitude And Translation Control For Spacecraft To Approach To A Tumbling Non-Cooperative Object During The Final Phase[J]. Journal of Space Science, 2015, 35(5): 603-610. doi: 10.11728/cjss2015.05.603

旋转非合作目标终端逼近的姿轨控制研究

doi: 10.11728/cjss2015.05.603
详细信息
    通讯作者:

    刘海龙,E-mail:11b904016@hit.edu.cn

  • 中图分类号: V448.2

Attitude And Translation Control For Spacecraft To Approach To A Tumbling Non-Cooperative Object During The Final Phase

  • 摘要: 针对旋转非合作目标的终端逼近过程进行研究, 建立了适用于任意偏心率的精 确航天器相对运动和姿态动力学模型, 并对传统的直线型同步自旋逼近策略进行 改进, 设计了用于保障终端逼近安全性的指数衰减型参考轨迹; 推导了基于比例 微分加解耦控制方法的相对轨道和姿态控制律, 通过数值仿真验证了控制器的有效性.

     

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  • 被引次数: 0
出版历程
  • 收稿日期:  2014-07-26
  • 修回日期:  2015-03-02
  • 刊出日期:  2015-09-15

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