中国空间科学技术

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冻结轨道的一阶解

杨维廉   

  1. 北京空间飞行器总体设计部 北京100086
  • 发布日期:2002-08-25

A First Order Solution for Frozen Orbit

Yang Weilian (Beijing Institute of Spacecraft System Engineering ,Beijing 100086)   

  • Online:2002-08-25

摘要: 将 Brouwer早期研究所获得的一阶解变换为适用于小偏心率轨道的结果 ,根据这个结果可以清楚地看出冻结轨道就是精确的圆轨道 ,冻结的特性及其机理也可以清楚地显示出来。此外还进一步采用 Hill变量将冻结轨道的一阶解表示成一种非常简单的形式。

关键词: 轨道摄动, 冻结轨道, 遥感卫星, 分析

Abstract: Based on the first order solution of Brouwer's theory for artificial satellite orbit, formulas suitable for near circular orbit are derived. From the formation it is obvious that the frozen orbit is the exact circular one. The feature and the cause of the frozen orbit are easily explained. In addition, a very simple solution for the frozen orbit is also presented by using Hill variables.