宇航学报 ›› 2011, Vol. 32 ›› Issue (4): 815-822.doi: 10.3873/j.issn.1000-1328.2011.04.017

• 制导、导航与控制 • 上一篇    下一篇

对无控旋转目标逼近的自适应滑模控制

李九人, 李海阳, 唐国金   

  1. 国防科技大学航天与材料工程学院,长沙  410073
  • 收稿日期:2010-03-15 修回日期:2010-07-18 出版日期:2011-04-15 发布日期:2011-04-26
  • 基金资助:
    国家自然科学基金(10902121)

Adaptive Sliding Mode Control for Approach to Uncontrolled Rotating Satellite

LI Jiu   

  1. College of Aerospace and Material Engineering, National University of Defense Technology, Changsha  410073, China
  • Received:2010-03-15 Revised:2010-07-18 Online:2011-04-15 Published:2011-04-26

摘要: 对追踪器逼近无控旋转目标器的轨迹和姿态六自由度控制问题进行了研究。基于适用于任意偏心率的航天器相对运动轨道和姿态动力学模型,对追踪器逼近无控旋转目标的参考轨迹和参考姿态进行了分析与设计,推导了一种用于六自由度逼近控制的自适应滑模控制器。通过仿真分析,证明了所设计的逼近参考轨迹和参考姿态的合理性,同时验证了自适应滑模控制器的有效性。

关键词: 航天器, 空间交会, 相对运动, 轨迹, 姿态, 自适应滑模控制

Abstract: The problem of trajectory and attitude control for a chaser to approach to an uncontrolled rotating target satellite is researched in this paper. Based on the orbit and attitude dynamics equations of two relative motion spacecrafts with arbitrary eccentrics, the reference trajectory and the attitude for a chaser to approach to an uncontrolled rotating target are analyzed and designed, and a kind of adaptive sliding mode controller is proposed for the six degree of freedom position and attitude control. The simulation results shown that the reference trajectory and attitude designed are reasonable, and the adaptive sliding mode controller is effective.

Key words: Spacecraft, Space rendezvous, Relative motion, Trajectory, Attitude, Adaptive sliding mode control  

中图分类号: