伴随卫星接近绕飞的轨道控制方法研究  

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

作　　者：李革非[1,2] 朱民才[2] 韩潮[1] 

机构地区：[1]北京航空航天大学宇航学院,北京100083 [2]北京航天飞行控制中心,北京100094

出　　处：《宇航学报》2009年第6期2182-2187,共6页Journal of Astronautics

摘　　要：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。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 concurrently through the concomitant satellite 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.

关 键 词：伴随卫星 轨道接近 轨道绕飞 

分 类 号：V448.2[航空宇航科学与技术—飞行器设计]