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This Note introduces an analytical optimal counter guidance law for intercepting a PN-guided incoming missile, whose main advantage lies in its optimal nature and low maneuverability requirement.
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This page is a summary of: Analytical Optimal Counter Guidance Against Proportional Navigation, Journal of Guidance Control and Dynamics, September 2024, American Institute of Aeronautics and Astronautics (AIAA),
DOI: 10.2514/1.g008370.
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