• 中国科技核心期刊
  • Scopus收录期刊
  • DOAJ收录期刊
  • JST收录期刊
  • Euro Pub收录期刊
LIU Yang, LI Zong-Ji, ZHANG Xi-Yong. Design of Guidance Law for Anti-torpedo Torpedo Based on Variable Structure Control[J]. Journal of Unmanned Undersea Systems, 2013, 21(1): 039-42. doi: 10.11993/j.issn.1673-1948.2013.01.009
Citation: LIU Yang, LI Zong-Ji, ZHANG Xi-Yong. Design of Guidance Law for Anti-torpedo Torpedo Based on Variable Structure Control[J]. Journal of Unmanned Undersea Systems, 2013, 21(1): 039-42. doi: 10.11993/j.issn.1673-1948.2013.01.009

Design of Guidance Law for Anti-torpedo Torpedo Based on Variable Structure Control

doi: 10.11993/j.issn.1673-1948.2013.01.009
  • Received Date: 2012-05-18
  • Rev Recd Date: 2012-06-29
  • Publish Date: 2013-02-20
  • Aiming at the low hitting precision and big normal overload of traditional torpedo guidance law, a guidance law for an anti-torpedo torpedo(ATT) based on variable structure control is designed. This ATT guidance law is on the basis of a mathematical model of movement relation between an ATT and a target torpedo. A variable structure control model is established taking course angle as control parameter and angular speed of line-of-sight as sliding mode surface. The proposed model needs a few parameters, and the parameters can be self-adaptively adjusted. Theoretical analysis and simulation show that the ATT guidance law is very robust for model parameters and environmental interference, and can gain high hitting precision and stable trajectory.

     

  • loading
  • [1]
    Shtessel Y B, Shkolnikov I A, Levant A. Guidance and Con-trol of Missile Interceptor Using Second-order Sliding Modes[J]. IEEE Transactions on Aerospace and Electronic System, 2009, 45(1): 110-124.
    [2]
    Wu Peng, Yang Ming. Integrated Guidance and Control De-sign for Missile with Terminal Impact Angle Constraint Based on Sliding Model Control[J]. Journal of Systems Engineering and Electronics, 2010, 16(4): 56-60.
    [3]
    高为炳.变结构控制理论基础[M]. 北京: 中国科学技术出版社, 1990.
    [4]
    禹春来, 许化龙, 刘云峰, 等. 导弹姿态控制系统快速输出采样离散变结构自适应控制[J]. 弹箭与制导学报, 2008, 28(2): 77-80.

    Yu Chun-lai, Xu Hua-long, Liu Yun-feng, et al. Discrete Variable Structure Control for Missile Attitude Control with Fast Output Sampling Feedback and Adaptive Control[J]. Journal of Projectiles, Rockets, Missiles and Guidance, 2008, 28(2): 77-80.
    [5]
    高磊, 徐德民, 任章.被动式鱼雷的自适应变结构制导律设计[J]. 兵工学报, 2001, 22(2): 280-283

    Gao Lei, Xu De-min, Ren Zhang. Adaptive Variable Structure Guidance Law For Passive Torpedo[J]. Acta Armamentarii, 2001, 22(2): 280-283.
    [6]
    詹致祥.鱼雷制导规律及命中精度[M]. 西安: 西北工业大学出版社, 1995: 116-232.
    [7]
    Cheng S S. Nonlinear Robust Digital Controller Based on Fuzzy Model for Homing Missiles [J]. Chaos, Solutions and Fractals, 2008(38): 192-198.
  • 加载中

Catalog

    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

    Article Metrics

    Article Views(1462) PDF Downloads(557) Cited by()
    Proportional views
    Related
    Service
    Subscribe

    /

    DownLoad:  Full-Size Img  PowerPoint
    Return
    Return