Adaptive control for spacecraft relative translation with parametric uncertainty

被引：29

作者：

Wu, Shunan ^{[1
,2
]}

Wu, Zhigang ^{[2
]}

Radice, Gianmarco ^{[3
]}

Wang, Rui ^{[2
]}

机构：

[1] Dalian Univ Technol, State Key Lab Struct Anal Ind Equipment, Dalian 116024, Peoples R China

[2] Dalian Univ Technol, Sch Aeronaut & Astronaut, Dalian 116024, Peoples R China

[3] Univ Glasgow, Sch Engn, Space Adv Res Team, Glasgow G12 8QQ, Lanark, Scotland

来源：

AEROSPACE SCIENCE AND TECHNOLOGY | 2013年 / 31卷 / 01期

基金：

中国博士后科学基金; 中国国家自然科学基金;

关键词：

Adaptive control; Relative translation; Parametric uncertainty; Spacecraft; QUATERNION BASED CONTROL; OUTPUT-FEEDBACK CONTROL; LOW-THRUST; ORBIT; OPTIMIZATION; GUIDANCE;

D O I：

10.1016/j.ast.2013.09.006

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

This paper investigates the adaptive control problem for spacecraft relative translation. The critical issues surrounding relative translation are firstly discussed, and then the relative motion model implemented in this paper is introduced. An adaptive controller that allows performing relative translation in the presence of uncertain orbital parameters is developed. The escape acceleration of the target is further considered, and a modified adaptive controller is then proposed in the presence of uncertain orbital parameters and escape trajectory. By constructing a particular Lyapunov function, the stability of the proposed controllers for the closed-loop systems is proven theoretically. Numerical simulations are finally provided to illustrate the performance of the proposed controllers. (C) 2013 Elsevier Masson SAS. All rights reserved.

引用

页码：53 / 58

页数：6

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