DocumentCode
2256301
Title
A new neural architecture for homing missile guidance
Author
Balakrishnan, S.N. ; Biega, Victor
Author_Institution
Dept. of Mech. & Aerosp. Eng., Missouri Univ., Rolla, MO, USA
Volume
3
fYear
1995
fDate
21-23 Jun 1995
Firstpage
2148
Abstract
We present a new neural architecture which imbeds dynamic programming solutions to solve optimal target-intercept problems. They provide feedback guidance solutions, which are optimal with any initial conditions and time-to-go, for a 2D scenario. The method discussed in this study determines an optimal control law for a system by successively adapting two networks - an action and a critic network. This method determines the control law for an entire range of initial conditions; it simultaneously determines and adapts the neural networks to the optimal control policy for both linear and nonlinear systems. In addition, it is important to know that the form of control does not need to be known in order to use this method
Keywords
dynamic programming; feedback; missile guidance; neural net architecture; neurocontrollers; optimal control; feedback guidance; homing missile guidance; imbeds dynamic programming; neural architecture; neural networks; optimal control; target-interception; Adaptive control; Aerospace engineering; Design engineering; Dynamic programming; Missiles; Neurocontrollers; Nonlinear systems; Open loop systems; Optimal control; Power engineering and energy;
fLanguage
English
Publisher
ieee
Conference_Titel
American Control Conference, Proceedings of the 1995
Conference_Location
Seattle, WA
Print_ISBN
0-7803-2445-5
Type
conf
DOI
10.1109/ACC.1995.531278
Filename
531278
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