仿真计算结果表明，采用脉冲控制模式，本文提出的安全轨迹制导策略能够实现小卫星临近作业的安全机动飞行。
The results of the simulation indicate that the safety trajectory guidance strategy can achieve safety maneuver flying of the small satellite proximity operation when using thrust control method.
追踪航天器在制导机动失效后的飞行轨迹的安全性，是最终平移段标称轨迹设计的主要依据。
The safety mode design of final translation trajectories of space rendezvous is investigated in this paper.
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