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The space debris poses a potential threat to the spacecraft, and the flyby mission could approach them for inspection or following removal. We develop a fuel-optimal guidance algorithm to ensure necessary mission constraints and the safety of the satellite. In addition, the allowed magnititude of deviation along the nominal flyby trajectory is visualized for estimating the mission risk intuitively.

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This page is a summary of: Guidance Strategy and Fast Robustness Analysis for Space Debris Flyby, Journal of Spacecraft and Rockets, May 2025, American Institute of Aeronautics and Astronautics (AIAA),
DOI: 10.2514/1.a36099.
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