Adaptive Sliding Mode Control for Spacecraft Formation Flying with Thruster Faults

被引：0
|
作者：
Cao, Xibin [1 ]
Liu, Ruixia [1 ]
Liu, Ming [1 ]
机构：
[1] Harbin Inst Technol, Res Ctr Satellite Technol, Harbin 150001, Heilongjiang, Peoples R China
来源：
IECON 2017 - 43RD ANNUAL CONFERENCE OF THE IEEE INDUSTRIAL ELECTRONICS SOCIETY | 2017年
基金：
中国国家自然科学基金;
关键词：
SWITCHED LINEAR-SYSTEMS; TIME; GUIDANCE;
D O I：
暂无
中图分类号：
T [工业技术];
学科分类号：
08 ;
摘要：
This paper studies the problem of spacecraft formation flying control with external disturbance and thruster faults. The Clohessy- Wiltshire equation without linearization is employed to describe the relative dynamic model. An adaptive sliding mode control scheme is designed to eliminate the effects of the thruster faults and external disturbances, such that the reachability of the proposed integral sliding surface is ensured. Finally, a numerical example is established to illustrate the effectiveness of the proposed control approach.
引用
收藏
页码：4015 / 4020
页数：6
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