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This work presents a computational way of calculating the bias to be appended to the classical missile-guidance law called proportional navigation, where the objective is to capture the target at a desired impact time.
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This page is a summary of: Computational Impact-Time Guidance with Biased Proportional Navigation, Journal of Guidance Control and Dynamics, June 2024, American Institute of Aeronautics and Astronautics (AIAA),
DOI: 10.2514/1.g007910.
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