Robust Adaptive Nonlinear Attitude Tracking Control of Flexible Spacecraft

被引：0
|
作者：
Zhou, Chengbao [1 ,2 ]
Hou, Lei [1 ,2 ]
Li, Yanfei [1 ,2 ]
Yang, Wenguang [2 ]
机构：
[1] North Informat Control Res Acad Grp Co Ltd, Nanjing 211153, Jiangsu, Peoples R China
[2] North Automat Control Technol Inst, Taiyuan 030006, Shanxi, Peoples R China
来源：
2018 37TH CHINESE CONTROL CONFERENCE (CCC) | 2018年
关键词：
Dynamic surface control; Adaptive control; Sliding mode control; Attitude tracking; Flexible spacecraft; DYNAMIC SURFACE CONTROL; VARIABLE-STRUCTURE; STABILIZATION;
D O I：
暂无
中图分类号：
TP [自动化技术、计算机技术];
学科分类号：
0812 ;
摘要：
The nonlinear attitude Kinematics of flexible spacecraft are expressed by the Euler angles and described by the vector form. Based on the dynamic surface control (DSC) approach, a robust adaptive nonlinear sliding mode attitude tracking algorithm is designed for flexible spacecraft in the presence of the external disturbances and system parameter uncertainties. This attitude control algorithm can be used when the upper bound of the lumped disturbances is unknown. Meanwhile the active vibration suppression control is adopted for flexible spacecraft. By the Lyapunov stability analyses, the desigied algorithms can guarantee the stability of the spacecraft attitude tracking control system. With the modal velocity feedback (MVF) method, the undesirable vibration of the flexible appendages of spacecraft is in the active suppression. Finally, the control simulation analyses verified the effectiveness of the proposed control strategy.
引用
收藏
页码：10082 / 10087
页数：6
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