• DocumentCode
    1795265
  • Title

    Research on response characteristic of moving-mass controlled flying vehicle

  • Author

    Shenghong Xu ; Wenjing Cao ; Ruitao Li

  • Author_Institution
    Dept. of Control Eng., Naval Aeronaut. & Astronaut. Univ., Yantai, China
  • fYear
    2014
  • fDate
    8-10 Aug. 2014
  • Firstpage
    2161
  • Lastpage
    2165
  • Abstract
    The response characteristics of the moving-mass controlled flying vehicle is researched based on the moving-mass control system model of the flying saucer. Simulation results show that when the vehicle flies in the thick atmosphere at low altitude, the states of the vehicle are disturbed by the movement of the sliding mass block, but the disturbance does not appear when the vehicle flies at superhigh altitude or in the outer space. The cause of the difference is analyzed, and the influencing factors of the disturbance are studied with simulation.
  • Keywords
    aircraft control; flying saucer; moving-mass control system model; moving-mass controlled flying vehicle; sliding mass block; vehicle response characteristics; Aerodynamics; Aerospace electronics; Control systems; Equations; Force; Mathematical model; Vehicles;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Guidance, Navigation and Control Conference (CGNCC), 2014 IEEE Chinese
  • Conference_Location
    Yantai
  • Print_ISBN
    978-1-4799-4700-3
  • Type

    conf

  • DOI
    10.1109/CGNCC.2014.7007509
  • Filename
    7007509