摘要
研究了椭圆轨道卫星编队飞行的构型设计问题。首先给出常用的两类相对运动方程,即基于相对轨道状态的相对运动方程和基于轨道根数的相对运动方程,并推导出两类相对运动方程之间的对应关系。然后,针对卫星编队飞行的构型设计问题,结合两类相对运动方程的优点,提出一种简化的编队飞行构型设计方法,避免了复杂的计算。最后通过数学仿真进行了验证。
The design of satellite formation flying configuration in elliptic orbit is studied in this paper.Firstly,two different equations of relative motion are presented,one equation based on the relative orbit states,another equation based on the orbit elements.The relations between two equations of relative motion are proposed in detail.Secondly,by using the advantages of two equations,a simple design method of formation flying configuration is presented,thus avoiding the complex computation.Simulation results have demonstrated the effectiveness of the proposed method.
出处
《航天控制》
CSCD
北大核心
2010年第2期36-41,共6页
Aerospace Control
关键词
椭圆轨道
编队飞行
构型设计
相对运动
Elliptic orbit
Formation flying
Configuration design
Relative motion
