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Use of Hopfield neural networks in optimal guidance

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2 Author(s)
Steck, J.E. ; Dept. of Mech. Eng., Wichita State Univ., KS ; Balakrishnan, S.N.

A Hopfield neural network architecture is developed to solve the optimal control problem for homing missile guidance. A linear quadratic optimal control problem is formulated in the form of an efficient parallel computing device known as a Hopfield neural network. Convergence of the Hopfield network is analyzed from a theoretical perspective, showing that the network, as a dynamical system approaches a unique fixed point which is the solution to the optimal control problem at any instant during the missile pursuit. Several target-intercept scenarios are provided to demonstrate the use of the recurrent feedback neural net formulation

Published in:
Aerospace and Electronic Systems, IEEE Transactions on  (Volume:30 ,  Issue: 1 )

Date of Publication: Jan 1994

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