In this paper, ADAMS simulation is applied to the separating motion of the several-satellite system in the background of Galileo satellite launched by Long March launch vehicle, in which, the detailed separating model of both satellites and launch vehicle and the procedure control of simulation are described, and the method of affect analysis about all kinds of elements is introduced.
以长征火箭发射伽利略星为应用背景 ,运用ADAMS软件对三星分离的近场情况进行了仿真分析。