DocumentCode
3075674
Title
Nonlinear adaptive attitude control of satellite using gyrotorquers
Author
Iyer, Ashok ; Singh, Sahjendra N.
Author_Institution
Dept. of Comput. Sci. & Electr. Eng., Nevada Univ., Las Vegas, NV, USA
fYear
1990
fDate
5-7 Dec 1990
Firstpage
3357
Abstract
A nonlinear adaptive control law for the attitude control of satellites using gyrotorquers is presented. The derivation of the control law does not require any information on the system dynamics and the environmental disturbance torques acting on the satellite. A simplified control law for spinning satellites is derived. The controller requires only attitude tracking error and its derivative for feedback. Simulation results are presented which show that, in the closed-loop system, precise attitude control can be accomplished in spite of the uncertainty in the system
Keywords
adaptive control; artificial satellites; attitude control; gyroscopes; nonlinear control systems; attitude control; attitude tracking error; closed-loop system; feedback; gyrotorquers; nonlinear adaptive control; spinning satellites; Adaptive control; Attitude control; Control systems; Error correction; Feedback; Nonlinear dynamical systems; Programmable control; Satellites; Spinning; Torque control;
fLanguage
English
Publisher
ieee
Conference_Titel
Decision and Control, 1990., Proceedings of the 29th IEEE Conference on
Conference_Location
Honolulu, HI
Type
conf
DOI
10.1109/CDC.1990.203418
Filename
203418
Link To Document