• DocumentCode
    2543206
  • Title

    Research of cooperation guidance scheme based on multiple missiles engagement

  • Author

    Ye, Jikun ; Lei, Humin ; Wang, Fei ; Li, Jiong

  • Author_Institution
    Dept. of Control Sci. & Eng., Missile Inistitude of Air Force Eng. Univ., Sanyuan, China
  • fYear
    2010
  • fDate
    16-18 April 2010
  • Firstpage
    73
  • Lastpage
    77
  • Abstract
    This paper discusses the development of guidance scheme for multiple missiles co-operation engagement. Firstly, based on the intercept point, the mid-course guidance out of the aerosphere is studied to obtain the shutdown condition. Secondly, using the the linearization of the control model and error feedback loop in the mid-course guidance out of the aerosphere, a new guidance law called ITCG (Impact-Time-Control Guidance) law is analyzed. The new guidance law can be used to guide multiple missiles co-operate to hit the target simultaneously with the desired time. Thirdly, based on the minimum information set theory, the procedure of information interchanging of mulitiple missiles engagement is designed, which solves the problem of communication among missiles in ITCG law. Finally, simulations for the proposed co-operation engagement scheme are conducted to validate the effectiveness, and doable performance.
  • Keywords
    feedback; information theory; linearisation techniques; missile guidance; set theory; cooperation guidance scheme; error feedback loop; impact-time-control guidance; information set theory; multiple missiles cooperation engagement; Acceleration; Control systems; Error correction; Feedback loop; Force control; Linear feedback control systems; Missiles; Optimal control; Tellurium; Velocity control; cooperation; guidance; information set; mid-course; proportional guidance;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Information Management and Engineering (ICIME), 2010 The 2nd IEEE International Conference on
  • Conference_Location
    Chengdu
  • Print_ISBN
    978-1-4244-5263-7
  • Electronic_ISBN
    978-1-4244-5265-1
  • Type

    conf

  • DOI
    10.1109/ICIME.2010.5477588
  • Filename
    5477588