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考虑轨道摄动影响的多冲量交会规划方法研究
引用本文:宋旭民,范丽,陈勇.考虑轨道摄动影响的多冲量交会规划方法研究[J].航天控制,2011,29(4):71-74.
作者姓名:宋旭民  范丽  陈勇
作者单位:装备指挥技术学院,北京,101416
摘    要:当交会时间较长时需要在轨道规划中考虑摄动的影响,本文基于虚拟瞄准点的思想,研究了考虑轨道摄动情况下的固定时间拦截问题求解方法,并提出了考虑轨道摄动影响的多冲量交会规划方法.通过仿真算例验证了算法的有效性,并对基于二体模型和考虑摄动的规划结果进行了对比.

关 键 词:轨道摄动  多冲量交会  轨道规划

The Research on the Multi-impulse Rendezvous Trajectory Planning with Orbit Perturbation
SONG Xumin,FAN Li,CHEN Yong.The Research on the Multi-impulse Rendezvous Trajectory Planning with Orbit Perturbation[J].Aerospace Control,2011,29(4):71-74.
Authors:SONG Xumin  FAN Li  CHEN Yong
Institution:SONG Xumin FAN Li CHEN Yong The Academy of Equipment Command and Technology,Bejing 101416,China
Abstract:The orbit perturbation must be considered in trajectory planning in case of the long-time duration of rendezvous.Based on the concept of virtual aiming point,the method of the fixed-time interception considering orbit perturbation is studied and the multi-impulse rendezvous planning method with perturvation affection is proposed.The method is valided through the implemention of simulation,and the results between one based on the two-body orbit model and one with the perturbation are compared.
Keywords:Orbit perturbation  Multi-impulse rendzvous  Trajectory planning  
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