CALCULATING METHOD OF SERIES FOR TRUE ANOMALY OF A SPACECRAFT ELLIPTIC ORBIT

• 作 者: 顾晓勤 谭朝阳 MA Xing-rui
• 机 构: ZhongshanCollege,不详
• 出 处: 应用数学和力学：英文版
• 发表日期: 2005年11期
• 关键词: 太空轨道 椭圆轨道 不规则性 迭代法 spacecraft orbit true anomaly eccentric anomaly iterative

The transcendental equation of a true anomaly was written in a power series instead of a differential form. When the sufficient condition of the iterative convergence is satisfied, the relationship between the true anomaly and the time was gotten by the i