[1] [1] WANG W,YU ZH J. Orbit Determination of Spacecraft-Model and Algorithm［M］.Beijing: Publishing House of National Defence Industry, 2007. (in Chinese)

[2] [2] LI J SH. Orbit Determination of Spacecraft ［M］. Beijing: Publishing House of National Defence Industry, 2003. (in Chinese)

[3] [3] YANG S H, XIANG CH SH, MA J G. Satellite orbit forecast in short arch with single sit ［J］.Opto-Electronic Engineering,2006,33(7):23-27.(in Chinese)

[4] [4] LIU L, WANG X. A method of orbit determination considering the oblatenss of the earth ［J］. Acta Astronomica Sinica, 2003,44(2):175-179.(in Chinese)

[5] [5] JIA P ZH. Development of orbit determination using kalman filter［J］. Journal of Spacecraft TT&C Technology, 2001,20(3):45-50.(in Chinese)

[6] [6] RAOL J R,SINHA N K. On the orbit determination problem ［J］. IEEE Transactions on Aerospace and Electronic Systems:1985, AES-21:274-291.

[7] [7] GAO C, QIAO Y F.Real-time error-correction method for photoelectrical theodolite［J］.Opt. Precision Eng., 2007,15(6):846-851.(in Chinese)

[8] [8] LI CH Y,LI H F,SUN C H.Astronomical calibration method and observation analysis for high-accuracy star sensor［J］.Opt.Precision Eng.,2006,14(4):558-563.(in Chinese)

[9] [9] LIU ZH H,BAI Y,LI H W,et al..Analysis on errors of single axis energy storage/attitude control system with double flywheels［J］.Opt.Precision Eng.,2006,14(1):127-132.(in Chinese)

[10] [10] LIU L SH.Tracking Data Processing［M］.Beijing:National Defense Industry Press,2000.(in Chinese)