Robust Space Trajectory Design Using Belief Optimal Control
نویسندگان
چکیده
This paper presents a novel approach to the robust solution of optimal impulsive control problems under aleatory and epistemic uncertainty. The uses belief Markov decision processes reformulate problem in terms uncertainty distributions, called beliefs, rather than realizations system states. formulation leads definition where cost function constraints are functions distributions. encompasses orbit determination arcs as well. optimization is solved with shooting-like transcription nonlinear programming solver optimize resulting discretized problem. Both uncertainties propagated nonintrusive polynomial expansion capture nonlinearities dynamics. Finally, this new applied flyby trajectory Europa Clipper mission scenario characterized by knowledge, execution, observation
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ژورنال
عنوان ژورنال: Journal of Guidance Control and Dynamics
سال: 2022
ISSN: ['1533-3884', '0731-5090']
DOI: https://doi.org/10.2514/1.g005704