• DocumentCode
    3396199
  • Title

    Attitude control for unmanned helicopter using h-infinity loop-shaping method

  • Author

    Mingyun Lv ; Yanpeng Hu ; Peng Liu

  • Author_Institution
    Sch. of Aeronaut. Sci. & Technol., Beihang Univ., Beijing, China
  • fYear
    2011
  • fDate
    19-22 Aug. 2011
  • Firstpage
    1746
  • Lastpage
    1749
  • Abstract
    The aim of this paper is to design an attitude controller of an unmanned helicopter using h-infinity and loop-shaping methods. A pre-compensator and a post-compensator are selected to modify the singular values of the normal system to get a desired loop shape. The h-infinity feedback controller is synthesized and the stability margin is calculated. The simulation results show that the attitude controller designed with robust performance has a good response performance, and h-infinity and loop-shaping methods can make unmanned helicopter have an excellent decoupling and dynamic performance.
  • Keywords
    H control; aerospace robotics; aircraft control; attitude control; compensation; control system synthesis; feedback; helicopters; mobile robots; remotely operated vehicles; stability; attitude controller design; h-infinity feedback controller synthesis; h-infinity loop-shaping method; post-compensator; precompensator; stability margin; unmanned helicopter; Attitude control; Control systems; H infinity control; Helicopters; Robustness; Shape; Stability analysis; controller; h-infinity; loop-shaping; simulation; unmanned helicopter;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Mechatronic Science, Electric Engineering and Computer (MEC), 2011 International Conference on
  • Conference_Location
    Jilin
  • Print_ISBN
    978-1-61284-719-1
  • Type

    conf

  • DOI
    10.1109/MEC.2011.6025819
  • Filename
    6025819