DocumentCode :
3485047
Title :
LPV methods for spacecraft control: An overview and two case studies
Author :
Corti, Andrea ; Dardanelli, A. ; Lovera, Marco
Author_Institution :
Dipt. di Elettron. e Inf., Politec. di Milano, Milan, Italy
fYear :
2012
fDate :
27-29 June 2012
Firstpage :
1555
Lastpage :
1560
Abstract :
In recent years there has been an increasing interest in the field of spacecraft control for the application of LPV methods to various systems (e.g., launchers, re-entry vehicles, satellites). The paper will first provide an overview of the state-of-the-art of the application of LPV techniques in this field. Then, the application of LPV modelling and controller design methods to the spacecraft attitude control problem will be specifically considered and two case studies will be illustrated. More precisely, first the problem of satellite attitude control using magnetic actuation will be introduced and an LPV formulation will be given; subsequently, the problem of attitude control using control moment gyros (CMGs) as primary actuators will be discussed and the LPV approach to the problem of developing steering laws for the CMGs will be described.
Keywords :
aircraft control; attitude control; control system synthesis; gyroscopes; linear systems; magnetic actuators; space vehicles; time-varying systems; CMG; LPV methods; LPV modelling; control moment gyros; controller design methods; linear parameter varying analysis; magnetic actuation; primary actuators; spacecraft attitude control; Actuators; Attitude control; Orbits; Satellites; Space vehicles; Torque; Vectors;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
American Control Conference (ACC), 2012
Conference_Location :
Montreal, QC
ISSN :
0743-1619
Print_ISBN :
978-1-4577-1095-7
Electronic_ISBN :
0743-1619
Type :
conf
DOI :
10.1109/ACC.2012.6315534
Filename :
6315534
Link To Document :
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