DocumentCode
1751709
Title
Globally convergent approximate dynamic programming applied to an autolander
Author
Murray, J. ; Cox, C. ; Saeks, R. ; Lendaris, G.
Author_Institution
Dept. of Electr. Eng., State Univ. of New York, Stony Brook, NY, USA
Volume
4
fYear
2001
fDate
2001
Firstpage
2901
Abstract
A globally convergent nonlinear approximate dynamic programming algorithm is described, and an implementation of the algorithm in the linear case is developed. The resultant linear approximate dynamic programming algorithm is illustrated via the design of an autolander for the NASA X-43 research aircraft, without a priori knowledge of the X-43´s flight dynamics
Keywords
aircraft control; convergence; dynamic programming; dynamics; linear programming; self-adjusting systems; stability; NASA; X-43 research aircraft; autolander; dynamic programming; flight dynamics; linear programming; stability; Convergence; Cost function; Dynamic programming; Equations; Heuristic algorithms; Jacobian matrices; NASA; Optimal control; Stability; State-space methods;
fLanguage
English
Publisher
ieee
Conference_Titel
American Control Conference, 2001. Proceedings of the 2001
Conference_Location
Arlington, VA
ISSN
0743-1619
Print_ISBN
0-7803-6495-3
Type
conf
DOI
10.1109/ACC.2001.946342
Filename
946342
Link To Document