伴星运动的轨道参数表示  

Expression of the Movement of Accompanying Satellites in Orbital Elements

作　　者：柳仲贵[1] 

机构地区：[1]北京跟踪与通信技术研究所

出　　处：《飞行器测控学报》2010年第4期79-83,共5页Journal of Spacecraft TT&C Technology

摘　　要：以经典开普勒轨道根数的形式对航天器的伴飞运动进行了细致描述,较之C-W形式的表达,该法具有易于理解和应用的特点;继而以其为理论指导,通过算例验证了其正确性及在伴飞轨道设计、维持与分析中的应用方法;指出伴飞构形对地面存在稳定性问题,需采用冻结轨道以消除。This paper presents the expression of the movement of accompanying satellites in orbital elements,and it is easy to understand and convenient for application,compared with those of C-W's form.Examples are given to verify its correctness and to show the way of using it in orbit design,maintenance and analysis.Result shows the formation facing earth is not robust unless a frozen orbit is applied.

关 键 词：伴星 轨道 运动方程 

分 类 号：P135[天文地球—天体力学]