Derives optimal guidance laws incorporating hard time-varying acceleration bounds into LQ control for linear missile and target dynamics, with nonlinear simulations showing improved interception over unbounded and soft-constrained alternatives.
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Optimal Ground-to-Air Interception with Time-Varying Acceleration Bounds
Derives optimal guidance laws incorporating hard time-varying acceleration bounds into LQ control for linear missile and target dynamics, with nonlinear simulations showing improved interception over unbounded and soft-constrained alternatives.