Volume 42 Issue 12
Jan.  2014
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Song Tao, Lin Defu, Qi Zaikang, Sun Baocai. Analysis on the characteristic of seeker disturbance rejection rate parasitical loop[J]. Infrared and Laser Engineering, 2013, 42(12): 3309-3314.
Citation: Song Tao, Lin Defu, Qi Zaikang, Sun Baocai. Analysis on the characteristic of seeker disturbance rejection rate parasitical loop[J]. Infrared and Laser Engineering, 2013, 42(12): 3309-3314.

Analysis on the characteristic of seeker disturbance rejection rate parasitical loop

  • Received Date: 2013-03-04
  • Rev Recd Date: 2013-04-13
  • Publish Date: 2013-12-25
  • The seeker disturbance rejection rate not only severely degrades seeker tracking accuracy, but also has greatly issues for the missile guidance performance. The generation mechanism of disturbance rejection rate was analyzed, and the models of disturbance rejection rate caused by spring torque and damping torque were established. Based on the Routh criterion, the stability zone of parasitical loop was obtained. The effect of the parasitical loop on effective guidance time constant and effective navigation ratio was studied. The result shows that the limits for important guidance parameters should be determined to insure the stability of parasitical loop; both the effective guidance time constant and effective navigation ratio are changed on the action of parasitical loop. The conclusion is helpful for engineers at the preliminary stage of guidance and control system design.
  • [1] Mao Xia, Zhang Junwei. Light axis stabilization of half-strapdown seeker[J]. Infrared and Laser Engineering, 2007, 36(1): 9-12. (in Chinese) 毛峡, 张俊伟. 半捷联导引头光轴稳定的研究[J]. 红外与激光工程, 2007, 36(1): 9-12.
    [2] Mu Hong. The Design of Radar Guider in Aerial Defence Missile[M]. Beijing: China Astronautics Press, 1996. (in Chinese) 穆虹. 防空导弹雷达导引头设计[M]. 北京: 宇航出版社,1996.
    [3] Miao Shaoshuai. Analysis on harmonic frequency and decoupling of seeker servo mechanism[D]. Changsha: National University of Defense Technology, 2008. (in Chinses) 苗少帅. 导引头伺服机构谐振频率与去耦精度分析[D]. 长沙: 国防科学技术大学,2008.
    [4] Zhu Huazheng, Fan Dapeng, Ma Dongxi, et al. Disturbance isolation index of seeker servo system and its test[J]. Optics and Precision Engineering, 2009, 17(8): 1993-1998. (in Chinses) 朱华征,范大鹏,马东玺,等. 导引头伺服系统隔离度与测试[J]. 光学精密工程,2009, 17(8): 1993-1998.
    [5] Lin Chunlian, Hsiao Yihsing. Adaptive feedforward control for disturbance torque rejection in seeker stabilizing loop[J]. IEEE Transactions on Control Systems Technology, 2001, 9(1): 108-121.
    [6] William Nesline F, Paul Zarchan. Radome induced miss distance in aerodynamically controlled homing missiles[D]. AIAA 84-1845.
    [7] Garnell P, East D J. Guidance Weapon Control Systems: chapter 8[M]. Oxford: Pergamon Press, 1977.
    [8] Du Yunli, Xia Qunli, Qi Zaikang. Research on effect of seeker disturbance rejection rate with phase lag on stability of parasitical loop[J]. Acta Armamentarii, 2011, 32(1): 28-32. (in Chinese) 杜运理, 夏群利, 祁载康. 导引头隔离度相位滞后对寄生回路稳定性影响研究[J]. 兵工学报, 2011, 32(1): 28-32.
    [9] Yin Shengli, Jia Hongguang, Zhang Yue, et al. Semi-strapdown Stabilization of optical imaging seeker[J]. Infrared and Laser Engineering, 2011, 40(1): 129-132. (in Chinese)
    [10] Zhang Yinghua, Wan Zhongnan. Error analysis of servo system for IR staring imaging seeker[J]. Infrared and Laser Engineering, 2006, 35(1): 25-30. (in Chinese) 张盈华, 万中南. 红外凝视成像导引头随动系统误差分析[J]. 红外与激光工程, 2006, 35(1): 25-30.
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Analysis on the characteristic of seeker disturbance rejection rate parasitical loop

  • 1. Department of Airospace Engineering,Beijing Institute of Technology,Beijing 100081,China;
  • 2. The Research Institute on General Development and Evaluation of Equipment,EAAF of PLA,Beijing 100085,China

Abstract: The seeker disturbance rejection rate not only severely degrades seeker tracking accuracy, but also has greatly issues for the missile guidance performance. The generation mechanism of disturbance rejection rate was analyzed, and the models of disturbance rejection rate caused by spring torque and damping torque were established. Based on the Routh criterion, the stability zone of parasitical loop was obtained. The effect of the parasitical loop on effective guidance time constant and effective navigation ratio was studied. The result shows that the limits for important guidance parameters should be determined to insure the stability of parasitical loop; both the effective guidance time constant and effective navigation ratio are changed on the action of parasitical loop. The conclusion is helpful for engineers at the preliminary stage of guidance and control system design.

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