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- W2393603458 abstract "To implement the rendezvous between two spacecrafts by the initially designed scheme with long-distance guidance under real perturbation conditions,a modified orbital transfer scheme was put forward in this paper.The initial multi-impulse scheme was transformed into finite thrust scheme and was amended.The relative orbit elements between two spacecrafts at guidance finish time were served as object function.The orbit involving J_2,J_3 and J_4 perturbation terms was propagated,which was used in the computation of the object function.The optimization variables were each beginning time,finish time and thrust direction.The optimal solution was obtained by using L-BFGS-B method so that the perturbation model error was corrected.The sample calculation showed that the corrected finite thrust scheme would realize tracing the spacecraft's rendezvous with target spacecraft under real perturbation conditions." @default.
- W2393603458 created "2016-06-24" @default.
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- W2393603458 date "2007-01-01" @default.
- W2393603458 modified "2023-09-22" @default.
- W2393603458 title "Algorithm for Correcting Orbital Transfer Scheme of Long-Distance Guidance" @default.
- W2393603458 hasPublicationYear "2007" @default.
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