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1. State-Constrained Agile Missile Control With Adaptive-Critic-Based Neural Networks.

Author

Dongchen Han and Balakrishnan, S.N.

Subjects
ADAPTIVE control systems, GUIDED missiles, FLIGHT control systems
Abstract

Develops an adaptive-critic-based controller to steer an agile missile that has a constraint on the minimum flight Mach number from various initial Mach numbers to a given final Mach number in minimum time while completely reversing the flightpath angle. Use of a two-neural-network structure called 'adaptive critic'; Solution of optimal control-related equations resulting from a Hamiltonian formulation.

Published
2002
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