Backstepping sliding mode control for combined spacecraft with nonlinear disturbance observer

被引：0
|
作者：
Gao, Han [1 ]
Lv, Yueyong [1 ]
Ma, Guangfu [1 ]
Li, Chuanjiang [1 ]
机构：
[1] Harbin Inst Technol, Dept Control Sci & Engn, Harbin, Peoples R China
来源：
2016 UKACC 11TH INTERNATIONAL CONFERENCE ON CONTROL (CONTROL) | 2016年
关键词：
combined spacecraft; nonlinear disturbance observer; backstepping; sliding mode; ATTITUDE TRACKING;
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：
To attenuate the effects of inertia uncertainty and external disturbance of combined spacecraft on attitude control accuracy and stability, a composite control law by combining nonlinear disturbance observer (NDO) and backstepping sliding mode control is proposed. In this paper, the nonlinear disturbance observer (NDO) is added to observe the unknown inertia and external disturbance, and asymptotic stability of the backstepping sliding mode control with NDO is demonstrated. The performance of the proposed attitude control for combined spacecraft is discussed, and the simulation results demonstrate the effectiveness and feasibility of the proposed controller.
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页数：6
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