Volume 43 Issue 1
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Wen Qiuqiu, Li Ran, Xia Qunli. Disturbance rejection rate and parasitical loop stability for strapdown imaging seeker[J]. Infrared and Laser Engineering, 2014, 43(1): 260-266.
Citation: Wen Qiuqiu, Li Ran, Xia Qunli. Disturbance rejection rate and parasitical loop stability for strapdown imaging seeker[J]. Infrared and Laser Engineering, 2014, 43(1): 260-266.

Disturbance rejection rate and parasitical loop stability for strapdown imaging seeker

  • Received Date: 2013-05-03
  • Rev Recd Date: 2013-06-12
  • Publish Date: 2014-01-25
  • The problems on disturbance rejection rate of strapdown imaging seeker and the stability of disturbance rejection rate parasitical loop were analyzed in this paper. Firstly, two calculation methods of line of sight (LOS) rate were given based on the information from seeker and inertial measurement unit (IMU). The calculation model got simplified in order to analyze the influence to disturbance rejection rate from different disturbance items. Then the magnitude and phase of disturbance rejection rate caused by the aerodynamic model, time delays of signals and graduate scales were analyzed, especially in the low frequency bandwidth. Finally, the disturbance rejection rate parasitical loop model based on strapdown seeker was derived. Through discussing the stability zones of parasitical loop, the permitted maximum values for different disturbances were given. The results present that disturbance sources mention above will cause the terrible disturbance rejection rate problem and make the parasitical loop become unstable, so it is necessary to rectify them when calculating LOS rate.
  • [1]
    [2] Qi Zaikang. Guidancd Munitions Technology [M]. Beijing: Beijing Institute of Technology Press, 2002. (in Chinese) 祁载康. 制导弹药技术[M]. 北京: 北京理工大学出版社, 2002.
    [3]
    [4] Zhou Ruiqing, Lu Shanwei, Liu Xinhua. Comparion of two stabilization methods for airborne strapdown antenna platform[J]. Systems Engineering and Electronics, 2005, 27 (8): 1397-1400. 周瑞青, 吕善伟, 刘新华, 弹载捷联式天线平台两种稳定 实现方法的比较[J]. 系统工程与电子技术, 2005, 27(8): 1397-1400.
    [5]
    [6] Gao Qingfeng, Li Xianglin, Xia Qunli, et al. Proportional navigation guidance law for rolling missiles with strapdown seekers[J]. Modern Defence Technology, 2009, 37 (5): 45-48. (in Chinese) 高庆丰, 李向林, 夏群力, 等. 旋转导弹捷联导引头比例 导引制导律研究[J]. 现代防御技术, 2009, 37(5): 45-48.
    [7]
    [8] Yao Yu, Zhang Guojiang. Discussion on strapdown imaging guidance system[J]. Infrared and Laser Engineering, 2006, 35(1): 1-6. (in Chinese) 姚郁, 章国江. 捷联成像制导系统的若干问题探讨[J]. 红 外与激光工程, 2006, 35(1): 1-6.
    [9]
    [10] Lin Zhe, Yao Yu, Fu Xiaowei. Line-of-sight reconstruction for stapdown imaging seeker [J]. Opto -Electronic Engineering, 2006, 33(3): 40-53. (in Chinese) 林喆, 姚郁, 富小薇. 捷联成像寻的器视线重构[J]. 光电 工程, 2006, 33(3): 40-53.
    [11] Woo Hyun Kim. Stability analysis of strapdown seeker scale factor error and los rate [C]//AIAA GNC Conference, 2007, 6788: 115-122.
    [12]
    [13]
    [14] Se -Ah Jang. Guidance Algorithms for tactical missile with strapdown seeker[C]//SICE Annual Conference, 2008: 2616- 2619.
    [15]
    [16] William Nesline F, Paul Zarchan. Radome induced miss distance in aerodynamically controlled homing missiles [C]// AIAA GNC Conference, 1984: 99-115.
    [17] Cui Yingying, Xia Qunli, Qi Zaikang. Seeker platform disturbance rejection mathematical model. Journal of Projectiles[J]. Rockets, Missiles and Guidance, 2006, 26(1): 22-25. (in Chinese) 崔莹莹, 夏群力, 祁载康. 导引头稳定平台隔离度模型研 究[J]. 弹箭与制导学报, 2006, 26(1): 22-25.
    [18]
    [19] 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, 祁载康, 夏群力. 导引头隔离度相滞后对隔离度 寄生回路稳定的影响[J]. 兵工学报, 2011, 32(1): 28-32.
    [20]
    [21] Gao Zhijie, Wang Shicheng, Shi Guohua. Hardware in -the-loop simulation of aerodynamically stabilized laser -guided aerial bomb [J]. Infrared and Laser Engineering, 2007, 36: 376-377. (in Chinese) 高智杰, 王仕成, 史国华. 风标式激光制导炸弹半实物仿 真研究[J]. 红外与激光工程, 2007, 36: 376-377.
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Disturbance rejection rate and parasitical loop stability for strapdown imaging seeker

  • 1. Department of Aerospace,Beijing Institute of Technology,Beijing 100081,China;
  • 2. China Research and Development Academy of Machinery,Beijing 100089,China

Abstract: The problems on disturbance rejection rate of strapdown imaging seeker and the stability of disturbance rejection rate parasitical loop were analyzed in this paper. Firstly, two calculation methods of line of sight (LOS) rate were given based on the information from seeker and inertial measurement unit (IMU). The calculation model got simplified in order to analyze the influence to disturbance rejection rate from different disturbance items. Then the magnitude and phase of disturbance rejection rate caused by the aerodynamic model, time delays of signals and graduate scales were analyzed, especially in the low frequency bandwidth. Finally, the disturbance rejection rate parasitical loop model based on strapdown seeker was derived. Through discussing the stability zones of parasitical loop, the permitted maximum values for different disturbances were given. The results present that disturbance sources mention above will cause the terrible disturbance rejection rate problem and make the parasitical loop become unstable, so it is necessary to rectify them when calculating LOS rate.

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