Adaptive attitude takeover control for space non-cooperative targets with stochastic actuator faults

被引:14
作者
Wang, Zheng [1 ,2 ]
Yuan, Jianping [1 ,2 ]
Che, Dejia [1 ,2 ]
机构
[1] Northwestern Polytech Univ, Natl Key Lab Aerosp Flight Dynam, Xian, Peoples R China
[2] Northwestern Polytech Univ, Sch Astronaut, Xian, Peoples R China
来源
OPTIK | 2017年 / 137卷
基金
中国国家自然科学基金;
关键词
Stochastic actuator faults; Non-cooperative targets; Attitude takeover control; Fault tolerant control; Dual-arm space robot; SLIDING-MODE CONTROL; TOLERANT CONTROL; TRACKING; SYSTEMS; DYNAMICS; CAPTURE;
D O I
10.1016/j.ijleo.2017.02.071
中图分类号
O43 [光学];
学科分类号
070207 ; 0803 ;
摘要
This paper focuses on the attitude takeover control for the space non-cooperative targets with stochastic actuator faults. In this paper, the stochastic deviation faults and gain faults of the actuators, as well as the inertia tensor calculated errors are all under consideration. By introducing an adaptive deviation fault compensation term and an input uncertainty compensation law in a nonlinear feedback controller, an adaptive fault tolerant attitude takeover control scheme is synthesized in this paper. The considered stochastic thruster faults, the calculated inertia tensor error and the external disturbance can be compensated, the stochastic attitude stabilization and tracking are maintained as a result. Based on a quadratic Lyapunov function, the proof of the stochastic convergence is completed. Simulation results demonstrate the effectiveness and advantages of the proposed method. (C) 2017 Elsevier GmbH. All rights reserved.
引用
收藏
页码:279 / 290
页数:12
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