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Discrete on/off constraints are difficult and computationally expensive to include in traditional optimization frameworks. We develop a fast and efficient trajectory optimization algorithm that can handle discrete constraints without introducing binary variables. A realistic case study for Apollo rendezvous is presented.

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This page is a summary of: Fast Homotopy for Spacecraft Rendezvous Trajectory Optimization with Discrete Logic, Journal of Guidance Control and Dynamics, July 2023, American Institute of Aeronautics and Astronautics (AIAA),
DOI: 10.2514/1.g006295.
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