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Demonstration on the indexes design of gravity satellite orbit parameters in the low-low satellite-to-satellite tracking mode
  • ISSN号:1001-1595
  • 期刊名称:《测绘学报》
  • 时间:0
  • 分类:V412.41[航空宇航科学与技术—航空宇航推进理论与工程;航空宇航科学技术] P223[天文地球—大地测量学与测量工程;天文地球—测绘科学与技术]
  • 作者机构:[1]Xi' an Research Institute of Surveying and Mapping, Xi' an 710054, China, [2]National Key Laboratory of Geo-Information Engineering, Xi' an 710054, China, [3]Key laboratory of G.eo-space Environment and Geodesy of Ministry of Education, Wuhan University, Wuhan 430079, China
  • 相关基金:The research is supported by the National Natural Science Foundation of China(41174026, 41104047, 41174017 ) and the Key laboratory Foun- dation of Geo-space Environment and Geodesy of Ministry of Education (11-01-03).
中文摘要:

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 discussed. 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.

英文摘要:

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.

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期刊信息
  • 《测绘学报》
  • 中国科技核心期刊
  • 主管单位:中国科学技术协会
  • 主办单位:中国测绘地理信息学会
  • 主编:杨元喜
  • 地址:北京市西城区三里河路50号
  • 邮编:100045
  • 邮箱:chxb@periodicals.net.cn
  • 电话:010-68531192
  • 国际标准刊号:ISSN:1001-1595
  • 国内统一刊号:ISSN:11-2089/P
  • 邮发代号:2-224
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  • 被引量:18477