Non-linear filter-based adaptive output feedback control for spacecraft formation flying

被引：6

作者：

Shan, J. ^{[1
]}

Lin, H. ^{[1
]}

机构：

[1] York Univ, Toronto, ON M3J 1P3, Canada

来源：

PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART I-JOURNAL OF SYSTEMS AND CONTROL ENGINEERING | 2009年 / 223卷 / I5期

关键词：

spacecraft formation flying; adaptive output control; non-linear filter;

D O I：

10.1243/09596518JSCE752

中图分类号：

TP [自动化技术、计算机技术];

学科分类号：

0812 ;

摘要：

This paper presents a non-linear filter-based adaptive output control for spacecraft formation flying missions. The study is motivated by the fact that only accurate position measurements are available for some systems, and velocities have to be estimated from those measurements. The proposed adaptive output controller guarantees asymptotic stability of the position and velocity tracking motion, even in the presence of uncertainties and external perturbations. The effectiveness of the proposed controller is verified by numerical simulations.

引用

页码：683 / 691

页数：9

共 48 条

[31] Distributed attitude consensus tracking control for spacecraft formation flying via adaptive nonsingular fast terminal sliding mode control
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