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题名: Orbit Control of Fly-around Satellite with Highly Eccentric Orbit by Using Solar Radiation Pressure
作者: Hou Yonggang; Zhao Changyin; Zhang Mingjiang; Sun Rongyu
刊名: Acta Astronomica Sinica
出版日期: 2016
卷号: 57, 期号:1, 页码:52-65
DOI: 0001-5245(2016)57:1<52:LYTYGY>2.0.TX;2-L
英文摘要: The method of controlling highly eccentric fly-around orbit using the solar wing is designed in this paper. The formation is maintained by controlling the follower. The in-plane and the out-of-plane control are separated. The follower is rotating around the inertial principal axis with a constant angular velocity. The controlling of the angular between the solar wings and satellite body is obtained. The orbit is controlled by adjusting the geometrical orientation. The in-plane control is prior to the out-of-plane control. The out-of-plane control force is applied when the error of in-plane is eliminated or the in-plane control force can not be supplied. Three different kinds of numerical simulations including the orbit reconfiguration, the error elimination, and the orbit maintenance are performed. It is shown that the method can keep the error less than 5 m,and it is feasible for the space formation.
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内容类型: 期刊论文
URI标识: http://libir.pmo.ac.cn/handle/332002/16848
Appears in Collections:空间目标与碎片观测研究基地_期刊论文

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