Attitude Adaptive Control Of Combined Spacecraft

被引：0
|
作者：
Wang, Qian [1 ]
Li, Xinhong [1 ]
He, Guanghong [1 ]
Zhang, Zhibin [1 ]
An, Jiping [1 ]
机构：
[1] Acad Equipment, 3380 Huairou 95, Beijing 101416, Peoples R China
来源：
PROCEEDINGS OF THE 2017 2ND JOINT INTERNATIONAL INFORMATION TECHNOLOGY, MECHANICAL AND ELECTRONIC ENGINEERING CONFERENCE (JIMEC 2017) | 2017年 / 62卷
关键词：
combination of spacecraft; attitude; adaptive control; RODRIGUES PARAMETERS;
D O I：
暂无
中图分类号：
TP39 [计算机的应用];
学科分类号：
081203 ; 0835 ;
摘要：
Aiming at the attitude adaptive control of spacecraft after docking, an adaptive attitude control method is proposed. Firstly, the dynamic modeling and spatial disturbance torque modeling of the combined spacecraft are carried out using the modified Rodriguez parameters to describe the attitude of the combined spacecraft. Secondly, according to the equation of attitude motion, the characteristic equation of closed-loop control system is deduced, and an adaptive attitude controller is designed. Finally, Matlab/Simulink simulation tool simulates the analysis. The simulation results show the effectiveness of the proposed controller for attitude control of the combined spacecraft.
引用
收藏
页码：85 / 89
页数：5
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