The design of the high-precision attitude control system of the LEO

摘要：

This paper designs the H∞ state feedback controller of the low-orbit satellite to achieve the high precision attitude control. Based on the analysis of the system uncertainty and environment disturbance of the low-orbit satellite, H∞ method is adopted and the LMI arithmetic is used to make the computation easier. The results of the system simulation prove that the algorithm is useful and can make the attitude control system achieve the high precision requirements.

作者: Song Ting Hao Tianwei Xia Yongjiang Chen Xueqin

作者单位: Shanghai Aerospace Control Engineering Institute,Shanghai,200233,China. Research Center of Satellite Technology,Harbin Institute of Technology,Harbin,150001,China.

会议类型: 国际会议

会议名称: The 3rd International Symposium on Systems and Control in Aeronautics and Astronautics(第三届航空航天系统与控制国际会议 ISSCAA 2010)

会议地点: 哈尔滨

会议语种:英文

页码: 340-343

在线出版日期: 2010-01-08（万方平台首次上网日期，不代表论文的发表时间）