Hohmann转移释放绳系卫星的方法研究

顾晓勤, 谭朝阳, 谭朝阳. Hohmann转移释放绳系卫星的方法研究[J]. 力学与实践, 1998, 20(6): 27-28. DOI: 10.6052/1000-0992-1999-361

引用本文:

顾晓勤, 谭朝阳, 谭朝阳. Hohmann转移释放绳系卫星的方法研究[J]. 力学与实践, 1998, 20(6): 27-28. DOI: 10.6052/1000-0992-1999-361

THE DEPLOYMENT OF TETHERED SUBSATELLITE WITH HOHMANN TRANSFER[J]. MECHANICS IN ENGINEERING, 1998, 20(6): 27-28. DOI: 10.6052/1000-0992-1999-361

Citation:

THE DEPLOYMENT OF TETHERED SUBSATELLITE WITH HOHMANN TRANSFER[J]. MECHANICS IN ENGINEERING, 1998, 20(6): 27-28. DOI: 10.6052/1000-0992-1999-361

THE DEPLOYMENT OF TETHERED SUBSATELLITE WITH HOHMANN TRANSFER

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．

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 .

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