OPTIMAL MIDCOURSE GUIDANCE LAW WITH NEURAL NETWORKS
Dongchen Han*, S.N.Balakrishnan*, E.J Ohlmeyer**
* Department of Mechanical and Aerospace Engineering and Engineering Mechanics University of Missouri-Rolla, Rolla, MO 65409-0050
** Naval Surface Warfare Center, Dahlgren, Va
A neural-network-based synthesis of an optimal midcourse guidance law is presented in this study. We use a set of two neural networks; the first network called a critic outputs the Lagranges multipliers arising in an optimal control formulation and second network, called an action network, outputs the optimal guidance-control. The system equations, the optimality conditions, the costate equations are used in conjunction with the network outputs to provide the targets for the neural networks. When the critic and action network are mutually consistent, the output of the action network yields optimal guidance-control. Numerical results for a number of scenarios show that the network performance is excellent. Corroboration for optimality is provided by comparisons of the numerical solutions using a shooting method for a number of scenarios.
Keywords: Aerospace, Optimal Control, Neural Networks
Session slot T-Tu-E06: Advances in Missile Guidance and Control/Area code 8a : Aerospace

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