• DocumentCode
    3189022
  • Title

    Simulation on the Inner Trajectory Motion of Projectile in a Three-Stage Synchronous Inductive

  • Author

    Ruifeng Li ; Wenbiao Liu ; Chongwei Shang ; Jie Wu ; Yanjie Cao

  • Author_Institution
    Naval Aeronaut. & Astronaut. Univ., Yantai
  • fYear
    2008
  • fDate
    10-13 June 2008
  • Firstpage
    1
  • Lastpage
    4
  • Abstract
    Numerical model of the multi-stage synchronous inductive coilgun is built in this paper. Flow chart of the simulation code for the numerical model is drawn. The simulation code is programmed with the calculation method of the axisymmetric magnetic field and the forward difference procedure of differential equation. The inner trajectory motion course of a three-stage synchronous inductive coilgun is simulated. The relation curves between the parameters of system and time is obtained.
  • Keywords
    differential equations; electromagnetic launchers; magnetic fields; axisymmetric magnetic field; differential equation; flow chart; forward difference procedure; inner trajectory motion; three-stage synchronous inductive coilgun; Acceleration; Coilguns; Equivalent circuits; Inductance; Magnetic fields; Numerical models; Power supplies; Projectiles; Switches; Switching circuits;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Electromagnetic Launch Technology, 2008 14th Symposium on
  • Conference_Location
    Victoria, BC
  • Print_ISBN
    978-1-4244-1832-9
  • Electronic_ISBN
    978-1-4244-1833-6
  • Type

    conf

  • DOI
    10.1109/ELT.2008.75
  • Filename
    4657635