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《Science of Surveying and Mapping》 2011-03
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GRACE reduced-dynamic orbit determination using zero-difference data

YI Peng-ju①②,ZHAO Chun-mei①,ZHENG Zuo-ya②(①Institute of Geodesy and Geodynamics,Chinese Academy of Surveying and Mapping,Beijing 100830,China;②Geomatics College,Shandong University of Science and Technology,Qingdao 266510,China)  
Based on the basic theory of Precise Orbit Determination,the method of the reduced-dynamic orbit determination using zero-difference data onboard GPS observations was researched in this paper·The orbit of GRACE satellite was determined by the auto-nomic software CASMORD.Compared GRACE orbiting results of reduced-dynamic method’s solutions with JPL’s PSO and SLR measurement,the results showed that the 3D-RMS was better than 7 cm and the direction ofX,Y,Zwas about3~5 cm,to demonstrate the feasibility and practicability of this method.
【Fund】: 国家高技术研究发展计划(2009AA12Z318);; 国家测绘局资源三号卫星项目
【CateGory Index】: P228.4
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【Co-citations】
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