Volume 32 Issue 1
Jan.  2007
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WANG Wei, YAN Jianguo, SHI Xian, PING Jinsong. Numerical Analysis of Lunar Satellite Orbit Revolutionary[J]. Geomatics and Information Science of Wuhan University, 2007, 32(1): 19-23.
Citation: WANG Wei, YAN Jianguo, SHI Xian, PING Jinsong. Numerical Analysis of Lunar Satellite Orbit Revolutionary[J]. Geomatics and Information Science of Wuhan University, 2007, 32(1): 19-23.
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Numerical Analysis of Lunar Satellite Orbit Revolutionary

  • 1 School of Science,Shenyang University of Technology,58 South Xinghua Street,Shenyang 110023,China|2 Shanghai Astronomical Observatory,Chinese Academy of Sciences,80 Nandan Road,Shanghai 200030,China|3 School of Geodesy and Geomatics,Wuhan University,129 Luoyu Road,Wuhan 430079,China|4 Department of Astronomy,Nanjing University,22 Hankou Road,Nanjing 210093, China

Funds: 国家自然科学基金资助项目(40674005);;武汉大学地球空间环境与大地测量教育部重点实验室开放研究基金资助项目;;中国科学院百人计划基金资助项目(804156)
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  • Received Date: October 28, 2006
  • Revised Date: October 28, 2006
  • Published Date: January 04, 2007
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  • By using of GEODYNⅡ from GSFC/NASA/USA and newly lunar gravity model LP165P from JPL/NASA/USA,the effects on the orbit revolutionary from different models by truncation to some degree and order are simulated and computed,the orbit revolutionary and analysis of orbital lifetime under different height,inclination and ellipticity with same lunar gravity model are computed.The results show that high inclination circular high orbit(150 km or 200 km) has better performance,with its orbit lasting more than one year without(alignment,) and its orbit can be computed with gravity model truncated in degree and order 100 without losing its accuracy.
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