中国空间科学技术

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Research on Small Satellite Formation Reconfiguration Control

Wei Juan * Ning Fangli ** Huang Yongxuan * (*Institute of System Engineering, Xi'an JiaoTong University, Xi'an 710049) (**College of Mechanical Engineering, Northwestern Polytechnical University, Xi'an 710072)   

  • Published:2003-08-25
  • Supported by:
    863高技术航天领域课题 ( 863 2 2 4 8)

Abstract: In this paper, 6DOF control of formation flying for formation reconfiguration is studied Firstly, rotation and translational motion model is established Then translational motion rale is designed mainly using robust control theory, the controller for closed loop system is obtained Finally, the correctness of the method is exemplified, the simulating result shows that the method is effective and feasible