DocumentCode :
3421919
Title :
Nonlinear tracking control of rigid spacecraft under disturbance using PD and PID type ℋ state feedback
Author :
Ikeda, Yuichi ; Kida, Takashi ; Nagashio, Tomoyuki
Author_Institution :
Dept. of Mech. Syst. Eng., Shinshu Univ., Nagano, Japan
fYear :
2011
fDate :
12-15 Dec. 2011
Firstpage :
6184
Lastpage :
6191
Abstract :
This study investigates six degrees-of-freedom nonlinear tracking control of rigid spacecraft under external disturbances. We propose two nonlinear tracking controllers having disturbance attenuation ability, namely, a proportional-derivative (PD)-type H state feedback controller and a proportional-integral-derivative (PID)-type H state feedback controller. Both these controllers have positive definite gain matrices whose conditions to be satisfied are given by linear matrix inequalities. The properties of these controller are compared and discussed through numerical studies.
Keywords :
H control; PD control; linear matrix inequalities; nonlinear control systems; position control; space vehicles; state feedback; three-term control; LMI; PD control; PID type H state feedback; disturbance attenuation ability; linear matrix inequalities; nonlinear tracking control; positive definite gain matrices; proportional-integral-derivative controller; rigid spacecraft; Attitude control; Closed loop systems; PD control; Quaternions; Space vehicles; State feedback; Target tracking;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Decision and Control and European Control Conference (CDC-ECC), 2011 50th IEEE Conference on
Conference_Location :
Orlando, FL
ISSN :
0743-1546
Print_ISBN :
978-1-61284-800-6
Electronic_ISBN :
0743-1546
Type :
conf
DOI :
10.1109/CDC.2011.6160253
Filename :
6160253
Link To Document :
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