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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Published in | The Journal of the astronautical sciences Vol. 70; no. 2 |
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Main Authors | , |
Format | Journal Article |
Language | English |
Published |
New York
Springer US
21.03.2023
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Subjects | |
Online Access | Get full text |
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