Volume 44 Issue 9
Nov.  2015
Turn off MathJax
Article Contents
Article Navigation >  Infrared and Laser Engineering  > 2015  >  44(9): 2854-2857

Wang Wei, Lin Defu, Xu Ping. Disturbance rejection program induced by strap-down seeker time delay[J]. Infrared and Laser Engineering, 2015, 44(9): 2854-2857.
Citation: Wang Wei, Lin Defu, Xu Ping. Disturbance rejection program induced by strap-down seeker time delay[J]. Infrared and Laser Engineering, 2015, 44(9): 2854-2857.
shu

Disturbance rejection program induced by strap-down seeker time delay

  • 1.

    School of Aerospace Engineering,Beijing Institute of Technology,Beijing 100081,China

  • Received Date: 2015-01-07
  • Rev Recd Date: 2015-02-12
  • Publish Date: 2015-09-25
  • The disturbance rejection rate problem caused by strap-down seeker was studied, the parasitical loop model induced by strap-down seeker time delay was established, the principium of how time delay causes disturbance rejection was analyzed, and the function of disturbance rejection rate induced by strap-down seeker time delay was deduced. Moreover, stability of the parasitical loop caused by time delay was investigated and of the parasitical loop with different guidance parameters was illustrated. The simulation result shows that, if the guidance system lag increases relatively to the missile aerodynamic time constant, the system can overcome larger seeker time delay; if the missile aerodynamic time constant is reduced, the guidance can tolerate larger seeker time delay. Disturbance rejection rate problem discussed in the paper is significant in the practical utilization.
  • [1] Zhou Ruiqing, Liu Xinhua, Shi Shouxia, et al. Strap-down Seeker Stability and Track Technology[M]. Beijing: National Defence Industry Press, 2010. (in Chinese)
    [2]
    [3]
    [4] Captain Thomas, Callen R. Guidance law design for tactical weapons with strapDown seekers[C]//AIAA-79-1732.
    [5] Qi Zaikang, Xia Qunli. Guided Weapon Control System[M]. Beijing: Beijing Institute of Technology Press, 2003. (in Chinese)
    [6]
    [7] Dong Jingxin, Zhao Changde, Xiong Shenshu, et al. Control Engineering Basic[M]. Beijing: Tsinghua University Press, 2003. (in Chinese)
    [8]
    [9] Meng Xiuyun. Missile Guidance and Control System Principle[M]. Beijing: Beijing Institute of Technology, 2003. (in Chinese)
  • 加载中
通讯作者: 陈斌, bchen63@163.com
  • 1. 

    沈阳化工大学材料科学与工程学院 沈阳 110142

  1. 本站搜索
  2. 百度学术搜索
  3. 万方数据库搜索
  4. CNKI搜索
Get Citation
PDF
XML

Article Metrics

Article views(332) PDF downloads(141) Cited by()

Related
Proportional views

Disturbance rejection program induced by strap-down seeker time delay

  • 1. School of Aerospace Engineering,Beijing Institute of Technology,Beijing 100081,China
  • Received Date: 2015-01-07
  • Rev Recd Date: 2015-02-12
  • Publish Date: 2015-09-25

Abstract: The disturbance rejection rate problem caused by strap-down seeker was studied, the parasitical loop model induced by strap-down seeker time delay was established, the principium of how time delay causes disturbance rejection was analyzed, and the function of disturbance rejection rate induced by strap-down seeker time delay was deduced. Moreover, stability of the parasitical loop caused by time delay was investigated and of the parasitical loop with different guidance parameters was illustrated. The simulation result shows that, if the guidance system lag increases relatively to the missile aerodynamic time constant, the system can overcome larger seeker time delay; if the missile aerodynamic time constant is reduced, the guidance can tolerate larger seeker time delay. Disturbance rejection rate problem discussed in the paper is significant in the practical utilization.

    HTML

Reference (9)

Catalog

    版权所有 © 2019 《红外与激光工程》编辑部｜ Address: 58 Zhonghuan West Road, Tianjin Airport Economic Zone｜ Post Code: 300308

    津ICP备19007885号-1

    Supported by: Beijing Renhe Information Technology Co. Ltd  

    /

    DownLoad:  Full-Size Img  PowerPoint
    Return
    Return