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Demonstration on the indexes design of gravity satellite orbit parameters in the low-low satellite-to-satellite tracking mode 被引量:1

Demonstration on the indexes design of gravity satellite orbit parameters in the low-low satellite-to-satellite tracking mode
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摘要 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, inter-satellite range and the orbit inclination are analyzed and calculated, and the issues towards twin gravity satellites such as coherence requirement of the orbit semi-major axes, control requirement of the pitch angle and time interval requirement to keep twin satellites formation in mobility are diseussed. Results show that the satellite orbit height is 400 km to 500 km, the inter-satellite range is about 220 km, the satellite orbit inclination is between polar orbit and sun-synchronous orbit, the semi-major axes difference of twin satellites orbit is within ± 70. 146 m, the pitch angle of twin satellites is about 0.9 degree, and the time interval to keep twin satellites formation in mobility is 7 days to 15 days. 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, inter-satellite range and the orbit inclination are analyzed and calculated, and the issues towards twin gravity satellites such as coherence requirement of the orbit semi-major axes, control requirement of the pitch angle and time interval requirement to keep twin satellites formation in mobility are diseussed. Results show that the satellite orbit height is 400 km to 500 km, the inter-satellite range is about 220 km, the satellite orbit inclination is between polar orbit and sun-synchronous orbit, the semi-major axes difference of twin satellites orbit is within ± 70. 146 m, the pitch angle of twin satellites is about 0.9 degree, and the time interval to keep twin satellites formation in mobility is 7 days to 15 days.
出处 《Geodesy and Geodynamics》 2013年第1期29-34,共6页 大地测量与地球动力学(英文版)
基金 supported by the National Natural Science Foundation of China(41174026,41104047,41174017) the Key laboratory Foundation of Geo-space Environment and Geodesy of Ministry of Education(11-01-03)
关键词 low-low satellite-to-satellite tracking (SST-11) satellite orbit height inter-satellite range orbitinclination index design low-low satellite-to-satellite tracking (SST-11) satellite orbit height inter-satellite range orbitinclination index design
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