• DocumentCode
    3388456
  • Title

    Data transmission of inductive setting for fuze in hard target penetrating rocket during muzzle

  • Author

    Li Bo ; Zhang Ya ; Zhang Hongxiang

  • Author_Institution
    Mech. & Electron. Eng. Inst., North Univ. of China, Taiyuan, China
  • Volume
    2
  • fYear
    2009
  • fDate
    19-20 Dec. 2009
  • Firstpage
    401
  • Lastpage
    402
  • Abstract
    Hard target penetrating fuzes can effectively enhance the penetrating effect for rockets from gun-launched platform, one of the key technologies for the fuzes is inductive setting. In this paper, the form of data code, the method of data transmission and the error control in transmission are discussed. Furthermore, the data transmission practical scheme to set the fuzes during muzzle is also given, which can make fuzes receive more than 5 frame data in muzzle setting windows by asynchronous serial communication with 16-bit binary encoding, and can reduce the error by out of step of the clock caused by high mechanical overload.
  • Keywords
    aircraft communication; binary codes; data communication; rockets; 16-bit binary encoding; asynchronous serial communication; data transmission; hard target penetrating fuzes; hard target penetrating rocket; high mechanical overload; inductive setting; muzzle setting; muzzles; Coils; Data communication; Demodulation; Electronic mail; Electrons; Fires; Frequency shift keying; Fuses; Intelligent transportation systems; Rockets; Hard target penetrating fuzes; data transmission; inductive setting;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Power Electronics and Intelligent Transportation System (PEITS), 2009 2nd International Conference on
  • Conference_Location
    Shenzhen
  • Print_ISBN
    978-1-4244-4544-8
  • Type

    conf

  • DOI
    10.1109/PEITS.2009.5406756
  • Filename
    5406756