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范剑峰;
发布日期:
Fan Jianfeng (Beijing Institute of Spacecraft Systems Engineering)
Published:
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.
范剑峰;. 伴随轨道拟合技术[J]. .
Fan Jianfeng (Beijing Institute of Spacecraft Systems Engineering). FITTING TECHNICS OF ADJOINT ORBIT[J]. .
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