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天基光学监视的GEO空间目标短弧段定轨方法 被引量:10
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作者 李冬 易东云 程洪玮 《中国空间科学技术》 EI CSCD 北大核心 2011年第3期1-7,共7页
利用两个短弧段的天基测角资料实现对GEO空间目标的轨道确定是天基空间目标监视系统需解决的重要问题之一。将短弧段的主要测量信息表示为弧段属性,构造约束空间目标距离和径向速度的容许域,采用桁架平衡法对第一个短弧段的容许域三角... 利用两个短弧段的天基测角资料实现对GEO空间目标的轨道确定是天基空间目标监视系统需解决的重要问题之一。将短弧段的主要测量信息表示为弧段属性,构造约束空间目标距离和径向速度的容许域,采用桁架平衡法对第一个短弧段的容许域三角剖分采样,以这些采样点的轨道预报第二个短弧段的弧段属性,通过分析预报值与实际值的差异,优先选取多个采样点的轨道作为初轨,分别对各初轨进行轨道改进。仿真结果表明,该方法能成功解算最小二乘轨道。 展开更多
关键词 短弧段 桁架平衡法 采样法 最小二乘轨道 轨道确定 空间目标 地球同步轨道
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Photometric analysis of a blue straggler eclipsing binary in the old open cluster NGC 2141
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作者 LUO YangPing WANG Bo +2 位作者 CHEN HaiLiang ZHANG XiaoBin HAN ZhanWen 《Science China(Physics,Mechanics & Astronomy)》 SCIE EI CAS 2012年第8期1500-1504,共5页
To understand the formation mechanism of blue stragglers in open clusters, we conducted a photometric analysis for a blue straggler eclipsing binary in the old open cluster NGC 2141. By using the least square fitting ... To understand the formation mechanism of blue stragglers in open clusters, we conducted a photometric analysis for a blue straggler eclipsing binary in the old open cluster NGC 2141. By using the least square fitting of times of minima, we derived the ephemeris and redetermined the orbital period of this system to be 0.6227 d. We have also done a photometric analysis for light curve with the Wilson-Devinney Code (2003). The photometric solutions reveal a semi-detached binary with the second- ary component filling its Roche lobe. The photometric mass ratio MJMI (secondary/primary) was determined to be 0.190_+0.002 and the ratio of V-band luminosity L2/LI(V) is about 0.033_+0.001, which indicates the secondary component is overluminous. Thus, this blue straggler likely results from a substantial mass exchange between these two components. 展开更多
关键词 open cluster eclipsing binary blue straggler PHOTOMETRY
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Orbit determination using incremental phase and TDOA of X-ray pulsar
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作者 Rong JIAO Lu-ping XU +1 位作者 Hua ZHANG Cong LI 《Frontiers of Information Technology & Electronic Engineering》 SCIE EI CSCD 2016年第6期543-552,共10页
X-ray pulsars offer stable, periodic X-ray pulse sequences that can be used in spacecraft positioning systems. A method using X-ray pulsars to determine the initial orbit of a satellite is presented in this paper. Thi... X-ray pulsars offer stable, periodic X-ray pulse sequences that can be used in spacecraft positioning systems. A method using X-ray pulsars to determine the initial orbit of a satellite is presented in this paper. This method suggests only one detector to be equipped on the satellite and assumes that the detector observes three pulsars in turn. To improve the performance, the use of incremental phase in one observation duration is proposed, and the incremental phase is combined with the time difference of arrival(TDOA). Then, a weighted least squares(WLS) algorithm is formulated to calculate the initial orbit. Numerical simulations are performed to assess the proposed orbit determination method. 展开更多
关键词 Orbit determination algorithm Single X-ray pulsar detector Phase increment Two-body motion equations Weighted least squares method
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