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Wu Meiping;Wu Ruilin (National University of Defence Technology,Changsha 410073)
Published:
Abstract: This paper researches correcting the maneuver errors of two spacecraft rendezvous by using two-impulse. Derive the ideal impulse solution of correcting errors,and simulate it in the reference equations of relative motion.The conclusion illustrates that this method is feasible.
Wu Meiping;Wu Ruilin (National University of Defence Technology,Changsha 410073). MANEUVER ERRORS CORRECTION DURING HORIZONTAL IMPULSE MULTI-SEGMENTAL ARC RENDEZVOUS[J]. .
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