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This paper develops several formulations to use nonlinear approximations of complex spacecraft dynamics to design maneuvers incorporating the effects of state uncertainty. These formulations can enable more flexible and rapid spacecraft maneuver planning in reaction to changing mission priorities, navigation errors, and maneuver execution errors.

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This page is a summary of: Nonlinear Formulations for Spacecraft Maneuver Design Under Uncertainty, Journal of Guidance Control and Dynamics, September 2025, American Institute of Aeronautics and Astronautics (AIAA),
DOI: 10.2514/1.g007854.
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