| 上面级多星部署的轨道设计研究 |
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| 引用本文： | 王俊峰,王月基,申麟,陈新民.上面级多星部署的轨道设计研究[J].导弹与航天运载技术,2011(1):6-9,53. |
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| 作者姓名： | 王俊峰 王月基 申麟 陈新民 |
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| 作者单位： | 中国运载火箭技术研究院研究发展中心;海军飞行学院; |
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| 摘 要： | 以部署4颗中高地球轨道(MEO)卫星为例,对上面级多星部署的轨道设计方法进行研究.首先采用冲量变轨的方法进行上面级多星部署策略研究,并选择了最省能量的多星部署方案;然后通过坐标转换,在轨道坐标系中,用数值计算的方法对选定的上面级多星部署方案进行详细的轨道设计.
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| 关 键 词： | 上面级 多星部署 轨道设计 |
Research on Multi-Satellite Deployment for Upstage |
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| Wang Junfeng,Wang Yueji,Shen Lin,Chen Xinmin.Research on Multi-Satellite Deployment for Upstage[J].Missiles and Space Vehicles,2011(1):6-9,53. |
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| Authors: | Wang Junfeng Wang Yueji Shen Lin Chen Xinmin |
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| Affiliation: | Wang Junfeng,Wang Yueji,Shen Lin,Chen Xinmin(1.Research and Design Center,China Academy of Launch Vehicle Technology,Beijing,100076,2.Naval Flying Academy,Liaoning,125000) |
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| Abstract: | This paper presents the orbit design method for deploying 4 MEO(medium earth orbit) satellites in one orbit.Firstly,the multi-satellite deploying strategy with the theory of impulse maneuver is studied,and then the optimal energy saving scheme is achieved.During the detail design,the traditional design method in launch coordinate system or geocentric equatorial coordinate system is very complicated.Therefore,the orbit coordinate system is defined,and the kinetics equations in it are established as well.The ... |
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| Keywords: | Upstage Multi-satellite deployment Orbit design |
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