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Completion of Spacecraft Rendezvous Under Error Condition

Wu Meiping Wu Ruilin (National University of Defense Technology,Changsha 410073)   

  • Published:2001-12-25

Abstract: While guidance project of the spacecrafts' rendezvous is designed,completion of rendezvous under error condition is considered.Two impules correct method to guide and correct errors during rendezvous is designed,basing on the horizontal impulse multi segmental arcs rendezvous project.Results of simulation shows that guidance is feasible,which doesn't influence advantages of rendezvous project.