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Orbit Determination Using Satellite-to-Satellite Tracking Data 被引量:9
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作者 ying-chunliu LinLiu 《Chinese Journal of Astronomy and Astrophysics》 CSCD 北大核心 2001年第3期281-286,共6页
Satellite-to-Satellite tricking (SST) data can be used to determine the orbits of spacecraft in two ways. One is combined orbit determination, which combines SST data with ground-based tracking data and exploits the ... Satellite-to-Satellite tricking (SST) data can be used to determine the orbits of spacecraft in two ways. One is combined orbit determination, which combines SST data with ground-based tracking data and exploits the enhanced tracking geometry. The other is the autonomous orbit determination, which uses only SST. The latter only fits some particular circumstances since it suffers the rank defect problem in other circumstances. The proof of this statement is presented. The nature of the problem is also investigated in order to find an effective solution. Several. methods of solution are discussed. The feasibility of the methods is demonstrated by their application to a simulation. 展开更多
关键词 Celestial mechanics: orbit determination - Methods: miscellaneous
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