Journal of Systems Engineering and Electronics ›› 2009, Vol. 31 ›› Issue (5): 1162-1166.

• 制导、导航与控制 • 上一篇    下一篇

空间站力矩平衡姿态稳定性研究

周黎妮, 唐国金, 罗亚中, 李海阳   

  1. 国防科技大学航天与材料工程学院, 湖南, 长沙, 410073
  • 收稿日期:2008-01-10 修回日期:2008-08-30 出版日期:2009-05-20 发布日期:2010-01-03
  • 作者简介:周黎妮(1980- ),女,博上研究生,主要研究方向为航天器姿态动力学与控制.E-mail;lindalnzhou@sohu.com

Stability analysis for space station torque equilibrium attitude

ZHOU Li-ni, TANG Guo-jin, LUO Ya-zhong, LI Hai-yang   

  1. Coll. of Aerospace and Material Engineering, National Univ. of Defense Technology, Changsha 410073, China
  • Received:2008-01-10 Revised:2008-08-30 Online:2009-05-20 Published:2010-01-03

摘要: 力矩平衡姿态的稳定性是空间站姿态TEA定向控制研究的重要问题.采用Lyapunov理论中求解导算子特征值的方法判断TEA的稳定性,基于线性化的姿态动力学方程采用基于稳定度设计的LQR方法设计空间站的姿态控制器,通过仿真验证了:(1)TEA作为平衡姿态的优点;(2)用导算子的特征值判断TEA姿态稳定性的方法的有效性.

Abstract: The stability of TEA is a very important problem in the space station TEA maintaining control study.The Lyapunov theory is used to judge the stability of TEA by calculating all the characteristic vectors and eigenvalues of the differential operator,and the stability-based LQR controller for space station attitude control is developed based on the linearized attitude dynamic equations.The simulation results prove:(1) the advantages of TEA as a balanced attitude;(2) the effectiveness of the stability judge method of calculating all the characteristic vectors and eigenvalues of the differential operator.

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