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
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;
Conference_Titel :
Control Applications, 1994., Proceedings of the Third IEEE Conference on
Conference_Location :
Glasgow
Print_ISBN :
0-7803-1872-2
DOI :
10.1109/CCA.1994.381183
