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《Chinese Journal of Geophysics》 2009-11
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Demonstration on the optimal design of resolution indexes of high and low sensitive axes from space-borne accelerometer in the satellite-to-satellite tracking model

ZHENG Wei~(1,2), XU Hou-Ze~1, ZHONG Min~1, YUN Mei-Juan~3, ZHOU Xu-Hua~1, PENG Bi-Bo~11 Key Laboratory of Dynamic Geodesy, Institute of Geodesy and Geophysics , Chinese Academy of Sciences , Wuhan 430077, China2 Disaster Prevention Research Institute, Kyoto University, Uji,Kyoto 611-0011, Japan3 Department of Applied Physics, Wuhan University of Science and Technology , Wuhan 430081,China  
The matching relationship of accuracy indexes from GRACE accelerometer, K-band ranging system and GPS receiver is demonstrated by numerical simulation based on the improved energy conservation principle. The results show:Firstly, cumulative geoid height error comes to 19~80 cm and 1. 5°×1. 5° cumulative gravity anomaly error is at the level of 0. 3~1. 3 mGal at degree 120, when the resolution of accelerometer is designed as ACC_X=(1~10)×10~(-9)m/S~2 and ACC_(Y,Z)=(1~10)×10~(-10) m/S~2 combined with other payloads with same accuracy indexes of GRACE; Secondly, it is appropriate to set the three-axis resolutions of accelerometer as ACC_X= (1~5)×10~(-9)m/S~2, ACC_(Y,Z)=(1~5)×10~(-10) m/S~2 in the future satellite gravity measurement in China, which basically matches with GRACE other payloads.
【Fund】: 中国科学院知识创新工程重要方向项目(KZCX2-YW-143 KZCX2-YW-202);; 国家自然科学基金(40674038);; 国家高技术研究发展计划(863)(2009AA12Z138 2006AA09Z153);; 日本JSPS基盘研究项目(B19340129)资助
【CateGory Index】: P228
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