DocumentCode :
3073434
Title :
Successive Galerkin approximation of nonlinear optimal attitude
Author :
Lawton, Jonathan ; Beard, Randal W. ; Mclain, Tim
Author_Institution :
Dept. of Electr. & Comput. Eng., Brigham Young Univ., Provo, UT, USA
Volume :
6
fYear :
1999
fDate :
1999
Firstpage :
4373
Abstract :
This paper presents the application of the successive Galerkin approximation (SGA) to the Hamilton-Jacobi-Bellman equation to obtain solutions of the optimal attitude control problem. Galerkin´s method approximates the value function by a truncated Galerkin series expansion. To do so, a truncated Galerkin basis set is formed. A sufficient number of functions must be included in this Galerkin basis set in order to guarantee that the solution will be a stabilizing control. By increasing the size of the Galerkin basis the quality of the approximation is improved at the cost of rapid growth in the computation load of the SGA. A major result of this paper is the development of the Galerkin basis set in the context of the optimal attitude control problem
Keywords :
Galerkin method; approximation theory; attitude control; dynamics; feedback; kinematics; nonlinear control systems; optimal control; robust control; Galerkin approximation; Hamilton-Jacobi-Bellman equation; aerospace control; attitude control; dynamics; feedback; kinematics; nonlinear control systems; optimal control; robust control; Angular velocity; Angular velocity control; Attitude control; Equations; Kinematics; Linear feedback control systems; Moment methods; Optimal control; Performance analysis; Space vehicles;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
American Control Conference, 1999. Proceedings of the 1999
Conference_Location :
San Diego, CA
ISSN :
0743-1619
Print_ISBN :
0-7803-4990-3
Type :
conf
DOI :
10.1109/ACC.1999.786394
Filename :
786394
Link To Document :
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