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作 者:Xu Peng Qiang Li'e Bian Xing Dong Peng Ju Peng Gao Wei Gong Xuefei Luo Ziren Shao Mingxue Tang Werilin Wan Xiaoyun Lau Yun-Kau
机构地区:[1]Institute of Applied Mathematics,Academy of Mathematics and Systems Science,Chinese Academy of Sciences [2]Morningside Center of Mathematics,Chinese Academy of Sciences [3]State Key Laboratory of Geodesy and Earth's Dynamics,Institute of Geodesy and Geo-physics,Chinese Academy of Sciences [4]Department of Geophysics,College o/the Geology Engineering and Geomatics,Chang 'an University [5]University of Chinese Academy of Sciences [6]Max-Planck-Institute for Grauitational Physics(Albert Einstein Institute) [7]Aerospace Flight Dynamics Laboratory,Beijing Aerospace Control Center [8]Qian Xuesen Laboratory of Launch Vehicle Technology [9]State Key Laboratory of Scientific and Engineering Computing,Academy of Mathematics and Systems Science,Chinese Academy of Sciences
出 处:《Geodesy and Geodynamics》2015年第5期333-343,共11页大地测量与地球动力学(英文版)
基 金:the project entitled"Advanced Gravity Measurement in Space"supported by the National Space Science Center,Chinese Academy of Sciences Profs.Wenrui Hu and Houze Xu's effort to promote satellite gravity research in China motivated the feasibility study in the first place;Support from National Natural Science Foundation of China(11305255,11171329 and 41404019);funding from State Key Laboratory of Geodesy and Earth's Dynamics,Institute of Geodesy and Geophysics,Chinese Academy of Sciences(SKLGED2013-3-8-E)are acknowledged
摘 要:With the Gravity Recovery and Climate Experiment {GRACE) mission as the prime example, an overview is given on the management and processing of Level IA data of a low-low satellite to satellite tracking mission. To illustrate the underlying principle and algorithm, a detailed study is made on the K-band ranging (KBR) assembly, which includes the measurement principles, modeling of noises, the generation of Level 1A data from that of Level 0 as well as Level IA to Level IB data processing.With the Gravity Recovery and Climate Experiment {GRACE) mission as the prime example, an overview is given on the management and processing of Level IA data of a low-low satellite to satellite tracking mission. To illustrate the underlying principle and algorithm, a detailed study is made on the K-band ranging (KBR) assembly, which includes the measurement principles, modeling of noises, the generation of Level 1A data from that of Level 0 as well as Level IA to Level IB data processing.
关 键 词:Data processingDual-one-way ranging (DOWR)Gravity recovery and climateexperiment (GRACE)K-band ranging (KBR)Satellite to satellite tracking (SST)Noise analysisSatellite gravityUltra stable oscillator (USO)
分 类 号:P223[天文地球—大地测量学与测量工程]
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