Optics and Precision Engineering, Volume. 16, Issue 9, 1688(2008)
Repeat sun-synchronous orbit design method based on Q value selection
References(3)
[3] [3] BOAIN R J.A-B-Cs of sun-synchronous orbit mission design[C].14th AAS/AIAA Space Flight Mechanics Conference,AAS 04-108,2004
[4] [4] BROUWER D.Solution of the problem of artificial satellite theory without drag[J].Astronautical Journal,1959,64(1274):387-397
[5] [5] CASEY D,WAY J.Orbit selection for the EOS mission and its synergism implications[J].IEEE Trans.Geosci.Remote Sensing,1991,29(6):822-835
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Qu Hong-song, ZHANG Ye, JIN Guang. Repeat sun-synchronous orbit design method based on Q value selection[J]. Optics and Precision Engineering, 2008, 16(9): 1688
Paper Information
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Received: Sep. 26, 2007
Accepted: --
Published Online: Feb. 28, 2010
The Author Email: Hong-song Qu (quhongsong@yahoo.com.cn)
CSTR:32186.14.
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