• DocumentCode
    2254876
  • Title

    Three dimensional motions control simulation for radial in vertical-type PM LSM rocket launcher

  • Author

    Yoshida, Kinjiro ; Cao, Yi

  • Author_Institution
    Dept. of Electr. & Electron. Syst. Eng., Kyushu Univ., Fukuoka, Japan
  • Volume
    2
  • fYear
    2004
  • fDate
    14-16 Aug. 2004
  • Firstpage
    761
  • Abstract
    In our previous papers, we proposed a vertical-type permanent magnet (PM) linear synchronous motor (LSM) rocket launcher system of which four acceleration guide-ways with armature-windings are arranged symmetrically along a shaft of about 3.8 m. We analyzed the characteristics of propulsion, levitation and guidance forces of PM LSM in the derived vertical-type PM LSM rocket launcher system by using two-dimensional interpolation method. This paper presents the three dimensional motions control simulation for radial displacements in vertical-type PM LSM rocket launcher. We derived the three dimensional motions equation of launcher and simulated three dimensional motions control of launcher when it starts with radial displacements. The stability of three dimensional motions control and the effectiveness of two-dimensional interpolation method have been verified numerically by the simulation results.
  • Keywords
    aerospace propulsion; interpolation; linear synchronous motors; machine control; motion control; permanent magnet motors; rockets; stability; three-term control; PID control method; armature-winding; guidance forces characteristic; levitation characteristic; permanent magnet linear synchronous motor rocket launcher; propulsion characteristic; radial displacement; three dimensional motions control simulation; two-dimensional interpolation method;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Power Electronics and Motion Control Conference, 2004. IPEMC 2004. The 4th International
  • Conference_Location
    Xi´an
  • Print_ISBN
    7-5605-1869-9
  • Type

    conf

  • Filename
    1375812