[1] [1] LI Y J.The stability condition and gyro installment postion of the inertially stabilized platform ［J］. Piezoelectrics & Acoustooptics, 2011,33(2): 203-206. (in Chinese)

[2] [2] JI W. Research on Servo Control System of Gyro Stabilized and Opto-electronic Tracking Platform［D］. Nanjing: Southeast University, 2006. (in Chinese)

[3] [3] YANG P,LI Q.Design and realization of control system for three-axis gyro stabilized platform［J］.Journal of Chinese Inertial Technology, 2007, 15(2): 171-176. (in Chinese)

[4] [4] WANG F Y, ZHANG X K. Self-stabilization modeling and simulation on ship-sway of a photoelectric tracker ［J］. Opto-Electronic Engineering,2005, 32(7): 11-14. (in Chinese)

[5] [5] WANG F Y.Study on the Self-stabilization Problem of the ShipBorne TV Tracker［D］. ChangChun: Institute of Optics, Fine Mechanics and Physics, Chinese Academy of Sciences, 2004.

[6] [6] XUE X Y, GAO Y G, HAN G Y, et al.. Total correction method of pointing error for level mounting theodolite ［J］. Opt. Precision Eng., 2011, 7(7): 1524-1530. (in Chinese)

[7] [7] QIU ZH A. A Study on the measurement and control technology of the attitude stabilization platform［D］. Changsha: Graduate School of National University of Defense Technology, 2006. (in Chinese)

[8] [8] DAVID H. TITTERTON J L. Strapdown Inertial Navigation Technology, 2rd edition ［M］. Beijing: national Defence industrial press. 2010.

[9] [9] QIN Y Y. Inertial navigation ［M］. Beijing: Science Press, 2006. (in Chinese)

[10] [10] JIN G, WANG J Q. The three-errora axis of theodolite with the utilization of the coordinate to the variation ［J］. Opt. Precision Eng., 1999, 5(10): 89-94. (in Chinese)

[11] [11] DAI Z L. The Modern Shipborne Campaign System［M］. Beijing: The publish of weapon Industry, 2002. (in Chinese)