可实现定点停泊与轨迹逼近的航天器交会控制

侯云忆; 景前峰; 马广富

可实现定点停泊与轨迹逼近的航天器交会控制

1.
哈尔滨工业大学航天学院, 哈尔滨 150001
2. 上海宇航系统工程研究所, 上海 201108

详细信息

中图分类号: V 448.234
计量
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- 被引次数: 0
出版历程
- 收稿日期: 2011-01-06
- 网络出版日期: 2012-08-30

Orbital rendezvous control method for berthing and tracking approach

1.
School of Astronautics, Harbin Institute of Technology, Harbin 150001, China
2. Shanghai Aerospace System Engineering Institute, Shanghai 201108, China

摘要

摘要: 许多空间任务均需进行轨道交会,据任务的不同,对轨道交会的要求也不同,某些情况下需要跟踪星在交会的过程中暂时停泊于某一点,某些情况下对交会过程的视线角与轨迹提出一定的要求.针对这种需求,设计了一种闭环反馈控制方法,可以使跟踪星在设定的某点进行停泊及停泊保持,也可以沿设定的某条轨迹逼近目标,以满足不同任务对交会过程的不同要求.经仿真表明,此方法能够很好的满足任务要求,并具有精度高、能耗低、跟踪速度快的特点.
- 航天器轨道交会 /
- 闭环反馈控制 /
- 逼近控制 /
- 停泊保持 /
- 轨迹逼近
Abstract: The spacecraft orbital rendezvous technology is required for many missions, and the requirements of orbital control vary with the different tasks. In some cases, the tracker will be asked to stop in specified position temporarily; in other cases, the line-of-sight angle and trajectory are limited in the process of orbital rendezvous. To meet the different needs of various tasks, a closed-loop feedback control law was designed. By using this method of orbital control, the tracker can stop and keep in fixed point and approach target along the predetermined trajectory. The simulation shows that the control method has the advantages of fast tracking speed, high-accuracy, and low power consumption.
- spacecraft orbital rendezvous /
- closed-loop feedback control /
- approach control /
- fixed point berthing /
- tracking approach

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参考文献(6)

[1]	林来兴.空间交会对接技术[M].北京:国防工业出版社,1995 Lin Laixing.Space rendezvous and docking technology[M].Beijing: National Defence Industry Press,1995(in Chinese)
[2]	王颖,吴宏鑫,解永春.基于视线制导的交会停靠控制方法[J].航天控制,2004,22(6):21-24 Wang Ying, Wu Hongxin,Xie Yongchun.Line of sight guidance based rendezvous and berthing control method [J].Areospace Control, 2004,22(6):21-24(in Chinese)
[3]	朱仁璋,尹艳.论空间交会最终平移段制导设计[J].中国空间科学技术,2004,5:1-8 Zhu Renzhang, Yin Yan.Guidance strategy design for the final translation of space rendezvous [J].Chinese Space Science and Technology,2004,5:1-8(in Chinese)
[4]	Hablani H B.Guidance and relative navigation for autonomous rendezvous in a circular orbit[J].Journal of Guidance, Control and Dynamics, 2002,25(3):553-562
[5]	陈统.空间自主交会的轨道动力学与控制方法研究 .北京:北京航空航天大学,宇航学院,2008 Chen Tong, A study on orbital dynamics and control of space autonomous rendezvous .Beijing:School of Austronautics,Beijing University of Aeronautics and Astronautics,2008(in Chinese)
[6]	Singla P,Subbarao K,Junkins J L.Adaptive output feedback control for spacecraft rendezvous and docking under measurement uncertainty[J].Journal of Guidance, Control, and Dynamic, 2006, 29(4):892-902