DocumentCode
289342
Title
Spacecraft attitude control using nonlinear servomechanism theory
Author
Huang, Jie ; Lin, Ching-Fang ; Hadaegh, Fred Y. ; Chiang, Richard Y.
Author_Institution
GNC Corp., Canoga Park, CA, USA
fYear
1994
fDate
24-26 Aug 1994
Firstpage
941
Abstract
The nonlinear servomechanism theory is applied to the attitude control of large maneuvering spacecraft subject to sinusoidal disturbances and parametric uncertainties. Simulation shows significant advantages of our attitude controller over the controller resulting from the feedback linearization approach
Keywords
attitude control; nonlinear control systems; servomechanisms; space vehicles; large maneuvering spacecraft; nonlinear servomechanism theory; parametric uncertainties; sinusoidal disturbances; spacecraft attitude control; Nonlinear systems; Position control; Servosystems; Space vehicles;
fLanguage
English
Publisher
ieee
Conference_Titel
Control Applications, 1994., Proceedings of the Third IEEE Conference on
Conference_Location
Glasgow
Print_ISBN
0-7803-1872-2
Type
conf
DOI
10.1109/CCA.1994.381183
Filename
381183
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