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力学与实践 ›› 1998, Vol. 20 ›› Issue (6): 27-28.doi: 10.6052/1000-0992-1999-361

• 应用研究 • 上一篇    下一篇

Hohmann转移释放绳系卫星的方法研究

顾晓勤 谭朝阳 谭朝阳1   

  1. 河北师范大学机械系 广东中山学院278信箱 528402 guxiaoqinguan@163.net 河北师范大学机械系
  • 收稿日期:2006-08-02 修回日期:1900-01-01 出版日期:1998-12-10 发布日期:1998-12-10

THE DEPLOYMENT OF TETHERED SUBSATELLITE WITH HOHMANN TRANSFER

  • Received:2006-08-02 Revised:1900-01-01 Online:1998-12-10 Published:1998-12-10

摘要: 借助Hohmann轨道转移的思想,研究一种绳系卫星释放方法并进行动力学分析.从轨道方程和Kepler方程导出轨道转移条件.由数值计算对此方法加以说明.

关键词: 绳系卫星, 动力学, Hohmann转移

Abstract: The new strategy for the deployment of tethered satellite is presented, which is similar to the idea of Hohmann transfer. The dynamics is studied, and the transfer condition is derived from the orbital equations and Kepler′s equation. At last, a numerical example is given .

Key words: tethered satellite, dynamics, Hohmann transfer