Infrared and Laser Engineering, Volume. 46, Issue 3, 331002(2017)

Effect of disturbance rejection rate on semi-strapdown seeker and on-line compensation of STUKF

Hu Oulei1,2、*, Wang Jiang1, Huang Peng3, Lin Defu1, and Yang Zhe1
Author Affiliations
  • 1[in Chinese]
  • 2[in Chinese]
  • 3[in Chinese]
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    References(14)

    [1] [1] Cheng Dong, Li Jinping, Chen Yun, et al. Light axis stabilization of semi-strapdown infrared imaging seeker[J]. Computer Measurement & Control, 2012, 20(11): 3008-3010. (in Chinese)

    [2] [2] Jianmei S, Gaohua C, Xianxiang C, et al. Stability region analysis of the parasitic loop of the semi-strapdown homing seeker[J]. Proceedings of the Institution of Mechanical Engineers, 2012, 226(4): 550-562.

    [3] [3] Song J, Cai G, Kong L, et al. Precision analysis of the semi-strapdown homing guided system[J]. Journal of Aerospace Engineering, 2012, 27(1): 151-167.

    [4] [4] Sun Gao, Zhu Mingchao, Liu Hui, et al. Optical axis stabilization of semi-strapdown seeker[J]. Infrared and Laser Engineering, 2013, 42(2): 489-494. (in Chinese)

    [5] [5] Zong Rui, Lin Defu, Liu Tairan, et al. Compensation method for scale error of optical strapdown seeker using UKF[J]. Infrared and Laser Engineering, 2014, 43(11): 3577-3584. (in Chinese)

    [6] [6] Xu Jiao, Wang Jiang, Song Tao, et al. A disturbance observer-based inhibition method for disturbance rejection rate of seeker[J]. Acta Armamentar, 2014, 35(11): 1790-1798. (in Chinese)

    [7] [7] Lin C L, Hsiao Y H. Adaptive feedforward control for disturbance torque rejection in seeker stabilizing loop[J]. Control Systems Technology, IEEE Transactions on, 2001, 9(1): 108-121.

    [8] [8] Li M, Zhu B, Wang S, et al. Strong tracking unscented Kalman filtering algorithm based-on satellite attitude determination system[J]. International Journal of Future Generation Communication & Networking, 2014, 7(3): 155.

    [9] [9] Jwo D J, Yang C F, Chuang C H, et al. Performance enhancement for ultra-tight GPS/INS integration using a fuzzy adaptive strong tracking unscented Kalman filter[J]. Nonlinear Dynamics, 2013, 73(1-2): 377-395.

    [10] [10] Han P, Mu R, Cui N. Effective fault diagnosis based on strong tracking UKF[J]. Aircraft Engineering and Aerospace Technology, 2011, 83(5): 275-282.

    [11] [11] Zheng Duo, Lin Defu, Xu Xinghua, et al. Effect of radome and seeker disturbance rejection rate parasitic loop on guidance system[J]. Systems Engineering and Electronics, 2015, 37(7): 1596-1603. (in Chinese)

    [13] [13] Paul Zarchan. Tactical and Strategic Missile Guidance[M]. 6th ed. Virginia: AIAA Inc, 2013: 34-45.

    [14] [14] Hu G, Gao S, Zhong Y, et al. Modified strong tracking unscented Kalman filter for nonlinear state estimation with process model uncertainty[J]. International Journal of Adaptive Control and Signal Processing, 2015, 29(12): 1561-1577.

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    Hu Oulei, Wang Jiang, Huang Peng, Lin Defu, Yang Zhe. Effect of disturbance rejection rate on semi-strapdown seeker and on-line compensation of STUKF[J]. Infrared and Laser Engineering, 2017, 46(3): 331002

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    Paper Information

    Category: 光电导航与控制

    Received: Jul. 5, 2016

    Accepted: Aug. 10, 2016

    Published Online: Jun. 27, 2017

    The Author Email: Oulei Hu (huoulei1215@163.com)

    DOI:10.3788/irla201746.0331002

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