[2] WANG J D, YU H D, LI Y. Research on the frame structure of small opto-electronic stabilized platform assembled on a UAV [J]. Mechanical Science and Technology for Aerospace Engineering, 2014, 33(10): 1604-1608. (in Chinese)
[4] ZHAO M. Study on Error Analysis and Compensation of Semi-Strapdown Photo-Elec-tricity Stabilized Platform [D]. Beijing: University of Chinese Academy of Sciences, 2014. (in Chinese)
[6] WU H L, JIA H G, WEI Q, et al.. Analysis of mass imbalance for roll-pitch inertial stabilized platform[J]. Journal of Xian Jiaotong University, 2015, 49(5): 108-115.(in Chinese)
[7] ZHANG L L, HUANG Y, L J F. Design and simulation of current-loop for servo of airborne electro-optical pointing and tr-acking platform [J]. Aviation Metrology &Measurement Technology, 2003, 23(6): 15-17, 21.(in Chinese)
[8] WANG F CH, TIAN D P, WANG Y T, Inertial stability and evaluation of photoelectric platform based on a simplified DOB [J].Foreign Electronic Measurement Technology, 2015, 34(12): 13-17.(in Chinese)
[11] CAI L H. Design of control system for high precision photoelectric stabilized platform[J]. Digital Technology and Application, 2015(11): 181-182.(in Chinese)
[13] TAN M, XU D, HOU Z G, et al.. Advanced Robot Control [M]. Beijing: Higher Education Press, 2007: 20-39. (in Chinese)
[14] FAN Y CH, LI J, JING Z Z, et al.. Calibration and compensation method on installation position error of tri-axis accelerometer units used in spinning projectiles [J].Chinese Journal of Sensors and Actuators, 2013, 26(10): 1352-1356. (in Chinese)
[15] YAN L J, ZHAO Y J, GAO ZH Y. Study on installation of piezoelectric acceleration sensor in the airborne test [J]. Electronic Measurement Technology, 2014, 37(7): 130-134. (in Chinese)
[16] LEI Y, QIU Y F. Parameter changes of electron components based on temperature variation[J]. Computer & Digital Engineering, 2015, 43(1): 155-158. (in Chinese)