The minimum delta-v relative orbit reconfiguration problem with impulsive maneuvers has been formulated and solved in several ways. This problem could have more than a single solution, caused by ambiguity from multiple orbit revolutions. This article introduces an approach to choose a unique solution to improve collision and abort safety, which are important factors for spacecraft proximity operation. Either out-of-plane or in-plane maneuver is modified from the existing calculation based on the given initial and final conditions, and its effectiveness is demonstrated with numerical simulations.
Impulsive Maneuvers Sequencer for Abort-Safety of Formation Flying
Lim, Yeerang;
2024-01-01
Abstract
The minimum delta-v relative orbit reconfiguration problem with impulsive maneuvers has been formulated and solved in several ways. This problem could have more than a single solution, caused by ambiguity from multiple orbit revolutions. This article introduces an approach to choose a unique solution to improve collision and abort safety, which are important factors for spacecraft proximity operation. Either out-of-plane or in-plane maneuver is modified from the existing calculation based on the given initial and final conditions, and its effectiveness is demonstrated with numerical simulations.File in questo prodotto:
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