A Time Regularization Scheme for Spacecraft Trajectories Subject to Multi-Body Gravity

A time regularization scheme is introduced that facilitates trajectory optimization in multi-body regimes. The time transformation function allows for fixed-step propagation, while eliminating the need for multiple models in patched conic approaches, and mitigating the risk of stepping over unplanne...

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Bibliographic Details
Published inThe Journal of the astronautical sciences Vol. 70; no. 2
Main Authors Leith, James, Russell, Ryan P.
Format Journal Article
LanguageEnglish
Published New York Springer US 21.03.2023
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