DocumentCode :
2413478
Title :
A family of optimal nonlinear feedback controllers that globally stabilize angular velocity
Author :
Wan, Chih-Jian ; Bernstein, Dennis S.
Author_Institution :
Dept. of Aerosp. Eng., Michigan Univ., Ann Arbor, MI, USA
fYear :
1992
fDate :
1992
Firstpage :
1143
Abstract :
Hamilton-Jacobi-Bellman theory is used to derive optimal nonlinear feedback control laws for a special class of nonlinear systems. The results are applied to a spacecraft angular velocity stabilization problem with two torque inputs. A family of optimal nonlinear feedback controllers that globally asymptotically stabilize angular velocity is established. Special cases of this family of controllers include generalizations of the locally stabilizing controllers of Brockett and Aeyels to global stabilization as well as the globally stabilizing controller of Byrnes and Isidori
Keywords :
aerospace control; angular velocity control; feedback; nonlinear control systems; optimal control; stability; Hamilton-Jacobi-Bellman theory; aerospace control; angular velocity stabilization; global stabilization; nonlinear systems; optimal nonlinear feedback controllers; spacecraft; Adaptive control; Angular velocity; Angular velocity control; Control systems; Equations; Feedback control; Force control; Nonlinear control systems; Nonlinear systems; Optimal control; Space vehicles; Torque;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Decision and Control, 1992., Proceedings of the 31st IEEE Conference on
Conference_Location :
Tucson, AZ
Print_ISBN :
0-7803-0872-7
Type :
conf
DOI :
10.1109/CDC.1992.371538
Filename :
371538
Link To Document :
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