Demonstration on the indexes design of gravity satellite orbit parameters in the low-low satellite-to-satellite tracking mode

Combining with the exigent demand of the development of satellite gravimetry system in China, aiming at the determination of technical indexes of gravity satellite orbit parameters, on the basis of the numerical experiments and results analysis, the design indexes of gravity satellite orbit height,...

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Bibliographic Details
Main Authors: Liu Xiaogang, Li Yingchun, Xiao Yun, Pang Zhenxing
Format: Article
Language:English
Published: KeAi Communications Co., Ltd. 2013-02-01
Series:Geodesy and Geodynamics
Subjects:
Online Access:http://www.sciencedirect.com/science/article/pii/S1674984715300598