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We analyze the heritage Desensitized Optimal Control technique to make it more computationally efficient. This approach leads to the idea of dominant sensitivity, which makes simpler the computation of more robust optimal trajectories.
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This page is a summary of: Fast Desensitized Optimal Control for Rocket-Powered Descent and Landing, Journal of Guidance Control and Dynamics, September 2025, American Institute of Aeronautics and Astronautics (AIAA),
DOI: 10.2514/1.g009058.
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