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Radiative heat can be the major source of heat in aerocapture. We prove that this source of heat is minimized by the trajectory that minimizes propellant consumption. We also provide a novel optimal guidance that takes attitude kinematics into accounts
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This page is a summary of: Minimum Radiative Heat and Propellant Aerocapture Guidance with Attitude Kinematics Constraints, Journal of Guidance Control and Dynamics, September 2025, American Institute of Aeronautics and Astronautics (AIAA),
DOI: 10.2514/1.g008917.
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