• DocumentCode
    2933289
  • Title

    Synchronous Detonation Control Technique on Rocket Based on Induction Setting

  • Author

    Bo, Li ; Ya, Zhang

  • Author_Institution
    Mech. & Electron. Eng. Inst., North Univ. of China, Taiyuan, China
  • Volume
    3
  • fYear
    2009
  • fDate
    21-22 Nov. 2009
  • Firstpage
    471
  • Lastpage
    472
  • Abstract
    Taking the breaking obstacle warfare as background, according to the maximum delay time and the error of synchronous detonation of rocket, based on the dynamic setter system with a unified timing starting point, it is discussed the working principle of the muzzle inductive setting system, and the transmission principle of the setting data is analyzed, then coding and decoding principle of the grouping pulse are designed, furthermore the circuit of grouping pulse encoding and the scheme of decoding are given, which would improve the broken-barrier ability of the rocket.
  • Keywords
    detonation; military systems; rockets; decoding principle; dynamic setter system; grouping pulse encoding; induction setting; muzzle inductive setting system; obstacle warfare; rocket; synchronous detonation control; Coils; Control systems; Data communication; Decoding; Design engineering; Error correction; Frequency; Pulse circuits; Rockets; Timing; Rocket; circuit design; grouping pulse coding; muzzle induction setting; synchronous detonation;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Intelligent Information Technology Application, 2009. IITA 2009. Third International Symposium on
  • Conference_Location
    Nanchang
  • Print_ISBN
    978-0-7695-3859-4
  • Type

    conf

  • DOI
    10.1109/IITA.2009.477
  • Filename
    5370360