伴随卫星接近绕飞的轨道控制方法研究

针对伴随卫星以共面方式接近目标星飞行、并最终实现共面绕飞这一 问题进行了研究。提出了通过轨道调相控制实现轨道接近，并且兼顾实现绕飞轨道构型参数 的方法。仿真实例表明，提出的接近绕飞轨道控制方法成功地实现了伴随卫星相对目标星的 接近和绕飞，很好地达到了绕飞轨道构型的参数指标要求。

An Orbit Transfer Method for Concomitant Satellite Approaching and Flying-around

This paper investigates that the concomitant satellite approaches and flies around the main satellite in coplanar mode. It brings forward an orbit transfer method which the relative orbit flying-around configuration is achieved coacurrently through the eoncomitant satelhte approaching to and flying around the main satellite. Simulation computations indicate the orbit transfer method for concomitant satellite approaching and flying-around is effective and feasible to the configuration of flying-around formation.