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,...

Täydet tiedot

Bibliografiset tiedot

Päätekijät:	Liu Xiaogang, Li Yingchun, Xiao Yun, Pang Zhenxing
Aineistotyyppi:	Artigo
Kieli:	Inglês
Julkaistu:	KeAi Communications Co., Ltd. 2013-02-01
Sarja:	Geodesy and Geodynamics
Aiheet:	low-low satellite-to-satellite tracking (SST-II) satellite orbit height inter-satellite range orbit inclination index design
Linkit:	http://www.sciencedirect.com/science/article/pii/S1674984715300598
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