• DocumentCode
    2677550
  • Title

    Research on lever loop in two-loop autopilot design by pole placement

  • Author

    He, Jing ; Xia, Qun-Li ; Cui, Xiao-Xi

  • Author_Institution
    Dept. of Flight Vehicle Design, Beijing Inst. of Technol., Beijing, China
  • Volume
    6
  • fYear
    2010
  • fDate
    24-26 Aug. 2010
  • Firstpage
    138
  • Lastpage
    141
  • Abstract
    The effect of lever loop on the two-loop autopilot has been often neglected in the traditional analysis and design, actually it has a great effect on the performance of the two-loop autopilot, because it brings the body angular acceleration into the main loop. Firstly, the method of two-loop autopilot pole placement is presented in the paper, when the dynamic performance of fin actuator, angular rate gyro, filter and accelerometer are neglected. Secondly, the effect of lever loop on the two-loop autopilot important parameters is analyzed. We find that the lever loop obviously decreases the increasing velocity of the autopilot undamped natural frequency and open loop crossover frequency along with open loop gain. In the condition we can design a high enough open loop gain autopilot without compensation in engineering. Finally, the principle of lever loop effect on the performance of two-autopilot is analyzed by root-locus.
  • Keywords
    acceleration control; aerospace control; control system synthesis; autopilot undamped natural frequency; body angular acceleration; lever loop; open loop gain; pole placement; traditional analysis; two-loop autopilot design; Gold; Topology; lever loop; open loop gain; pole placement; root-locus; two-loop autopilot;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Computer, Mechatronics, Control and Electronic Engineering (CMCE), 2010 International Conference on
  • Conference_Location
    Changchun
  • Print_ISBN
    978-1-4244-7957-3
  • Type

    conf

  • DOI
    10.1109/CMCE.2010.5609896
  • Filename
    5609896