Research Repository

Multi-Objective Robust H-infinity Control of Spacecraft Rendezvous

Gao, Huijun and Yang, Xuebo and Shi, Peng (2009) Multi-Objective Robust H-infinity Control of Spacecraft Rendezvous. IEEE Transactions on Control Systems Technology, 17 (4). pp. 794-802. ISSN 1063-6536

[img] Text
(4297)Article_-_Multi-objective_Robust_H_-_2009-TCST-GYS.pdf

Download (345kB)

Abstract

Based on the relative motion dynamic model illustrated by C-W equations, the problem of robust Hinfin control for a class of spacecraft rendezvous systems is investigated, which contains parametric uncertainties, external disturbances and input constraints. An Hinfin state-feedback controller is designed via a Lyapunov approach, which guarantees the closed-loop system to meet the multi-objective design requirements. The existence conditions for admissible controllers are formulated in the form of linear matrix inequalities (LMIs), and the controller design is cast into a convex optimization problem subject to LMI constraints. An illustrative example is provided to show the effectiveness of the proposed control design method.

Item Type: Article
Uncontrolled Keywords: ResPubID17501, H-infinity control, Lyapunov methods, aircraft control, closed loop systems, control system synthesis, convex programming, linear matrix inequalities, robust control, state feedback, uncertain systems
Subjects: SEO Classification > 970109 Expanding Knowledge in Engineering
Faculty/School/Research Centre/Department > Institute for Logistics and Supply Chain Management (ILSCM)
FOR Classification > 0199 Other Mathematical Sciences Information Systems
Depositing User: VUIR
Date Deposited: 09 Jun 2011 01:48
Last Modified: 23 Dec 2014 04:51
URI: http://vuir.vu.edu.au/id/eprint/4297
DOI: 10.1109/TCST.2008.2012166
ePrint Statistics: View download statistics for this item
Citations in Scopus: 44 - View on Scopus

Repository staff only

View Item View Item

Search Google Scholar