中国空间科学技术

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小卫星编队重构控制研究

韦娟,宁方立,黄永宣   

  1. 西安交通大学系统工程研究所,西北工业大学机电工程学院,西安交通大学系统工程研究所 西安710049 ,西安710072 ,西安710049
  • 发布日期:2003-08-25

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)

摘要： 主要研究对编队飞行卫星进行 6自由度控制以达到所要求的编队构型。首先 ,分别建立了平移运动模型和旋转运动模型 ;其次 ,重点利用鲁棒控制理论进行平移控制律设计 ,得到了使闭环系统稳定的控制器 ;最后进行了仿真计算 ,验证了控制律设计的有效性和可行性

关键词: 编队飞行, 鲁棒控制, 仿真模型, 小型卫星

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