• Infrared and Laser Engineering
  • Vol. 45, Issue 2, 217005 (2016)
Wang Zhiwei1、*, Shi Zhiyong1, Qin Junqi1, and Wang Fengjie2
Author Affiliations
  • 1[in Chinese]
  • 2[in Chinese]
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    DOI: 10.3788/irla201645.0217005 Cite this Article
    Wang Zhiwei, Shi Zhiyong, Qin Junqi, Wang Fengjie. Route design of simple calibration of rocket projectile onboard SINS[J]. Infrared and Laser Engineering, 2016, 45(2): 217005 Copy Citation Text show less
    References

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

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

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

    [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)

    Wang Zhiwei, Shi Zhiyong, Qin Junqi, Wang Fengjie. Route design of simple calibration of rocket projectile onboard SINS[J]. Infrared and Laser Engineering, 2016, 45(2): 217005
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