[1] [1] Savage P G. Strapdown Analytics[M]. Maple Plain, Minnesota: Strapdown Associates, Inc, 2007.

[2] [2] Gamble A E, Jenkins P． Low cost guidance for the multiple launch rocket system(MLRS) artillery rocket[J]. IEEE AES Systems, 2001, 16(1): 33-39．

[3] [3] Robert M Rogers. Applied Mathematics in Integrated Navigation Systems[M]． Second Edition. Reston: AIAA, 2003．

[4] [4] Zhu Yanhua, Liu Jianye, Sun Yongrong, et al. Research onreal time IMU error calibration methods for missile prelaunch preparation[J]. Systems Engineering and Electronics, 2007, 29(4): 618-621. (in Chinese)

[5] [5] You Jinchuan, Qin Yongyuan, Yang Pengxiang, et al. On-launcher calibration of SIMU for the guided multiple launch rocket system(GMLRS)[J]. Chinese Journal of Sensors and Actuators, 2011, 24(7): 1001-1006. (in Chinese)

[6] [6] Li Haiqiang, Shan Lijuan, Qing Li. Research on a method of calibrating SIMU without removal from missile[J]. Tactical Missile Control Technology, 2006(2): 32-36. (in Chinese)

[7] [7] Wu Ping, Lei Humin, Shao Lei, et al. Calibration without opening box for vehicle silo missile′s inertia instrument[J]. Journal of Chinese Inertial Technology, 2010, 18(1): 29-32. (in Chinese)

[8] [8] Syed Z F, Aggarwal P, Goodall C, et al． A new multiposition calibration method for MEMS inertial navigation systems[J]． Measurement Science and Technology, 2007, 18: 1897- 1907．

[9] [9] Jiang Qiyuan, Tang Jianxun, Yuan Baolun, et al. Analysis and compensation for size effect error of laser gyro Strapdown Inertial Navigation System[J]. Infrared and Laser Engineering, 2015, 44(4): 1110-1114. (in Chinese)

[10] [10] High Mobility Artillery Rocket System(HMARS) Program Overview[EB/OL].[2015-01-12]. http://www. army-technology.com/projects/himars/.

[11] [11] Wang Wei, Xiang Zheng, Wang Guodong. Fiber optic gyroscope SINS/GNSS tight integrated navigation based on adaptive Kalman filter[J]. Infrared and Laser Engineering, 2013, 42(3): 686-691. (in Chinese)