论文提出了航天器与空间目标距离较近时的自主规避策略.分析了航天器与目标的相对运动模型,将相对运动分解为视线瞬时旋转平面内的运动与该平面的转动.对视线瞬时平面内的运动进行了分析,推导了航天器的最佳规避方向.探讨了在三维惯性空间中该方向的确定方法.通过仿真分析,对比了航天器具有不同规避加速度和不同探测距离时,通过机动所得脱靶量的大小,验证了航天器近距离自主规避策略的有效性.%The active evasion strategy of spacecraft is discussed when the distance between spacecraft and target is relatively short. Firstly, the relative dynamic model is analyzed. The relative motion can be decomposed into two submotions, viz. , the relative motion in the instantaneous rotation of the line of sight (IRPL) and the rotation of this plane. Secondly, the optimum evasion direction of the spacecraft is proposed, through the analysis of the relative motion in IRPL. Thirdly, the determination of this direction in the inertial space is discussed. Finally, the numerical simulation is conducted with different maneuver accelerations and different detective distance of the spacecraft. The effectiveness of the active evasion strategy is demonstrated with the simulation results.
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