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伴随轨道拟合技术

范剑峰;   

  1. 北京空间飞行器总体设计部,
  • 发布日期:1990-06-25

FITTING TECHNICS OF ADJOINT ORBIT

Fan Jianfeng (Beijing Institute of Spacecraft Systems Engineering)   

  • Published:1990-06-25

摘要: 航天器的伴随轨道可以执行各种特殊任务。文中给出一种从伴随轨道确定两个航天器轨道要素的方法,这一方法也可推广应用于多个航天器的情况。

关键词: 伴随轨道, 轨道拟合, 轨道要素

Abstract: Adjoint orbit of spacecraft can perform various specific missions. This paper presents a method by using of which the orbital elements of two spacecrafts can be determined by an adjoint orbit. Also, this method can be used to the condition of multi-spacecraft.