中国空间科学技术

中国空间科学技术

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卫星轨道维持方法

张荣保   

  1. 空间飞行器总体设计部
  • 发布日期:1988-02-25

THE METHOD FOR ARTIFICIAL SATELLITE ORBIT MAINTAIN

Zhang Rongbao (Institute of Spacecraft System Engineering)   

  • Online:1988-02-25

摘要： 人造地球卫星的轨道由于大气阻力和地球引力场等因素的摄动,其形状和近地点位置将不断改变。本文提供一种保持轨道形状和近地点位置不变的控制方法。

关键词: 卫星轨道, 轨道控制, 方法

Abstract: The shape and perigee of artificial satellite orbits shall continually variate due to caused by the atmospherical drag and the earth gravity. This paper offers a method which maintain orbital shape and perigee location.

Key words: Satellite orbit, Orbit control, Method