Robust H∞ control of spacecraft rendezvous on elliptical orbit

被引：43
|
作者：
Gao, Xiangyu [1 ,3 ]
Teo, Kok Lay [2 ,3 ]
Duan, Guang-Ren [3 ]
机构：
[1] Heilongjiang Univ, Sch Math Sci, Harbin 150080, Peoples R China
[2] Curtin Univ Technol, Dept Math & Stat, Perth, WA 6845, Australia
[3] Harbin Inst Technol, Ctr Control Theory & Guidance Technol, Harbin 150001, Peoples R China
来源：
JOURNAL OF THE FRANKLIN INSTITUTE-ENGINEERING AND APPLIED MATHEMATICS | 2012年 / 349卷 / 08期
基金：
中国国家自然科学基金;
关键词：
MATRIX; DESIGN; GUIDANCE; LYAPUNOV; SYSTEMS;
D O I：
10.1016/j.jfranklin.2012.08.005
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 investigates the robust H-infinity control problem of spacecraft rendezvous on elliptical orbit. Based on Lyapunov theory, a sufficient condition for the existence of the robust H-infinity controller is given in terms of the periodic Riccati differential equation (RDE). Then, a stabilizable controller design method based on a fast multi-shot algorithm is proposed. With the controller obtained, the spacecraft rendezvous mission can be accomplished. An illustrative example is provided to show the effectiveness of the proposed control design method. (C) 2012 The Franklin Institute. Published by Elsevier Ltd. All rights reserved.
引用
收藏
页码：2515 / 2529
页数：15
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