• DocumentCode
    2282058
  • Title

    Design of autopilot with Pole placement and State-Observer Feedback

  • Author

    Lei, Wang ; Xiu-yun, Meng ; Qun-li, Xia ; Guo Tao

  • Author_Institution
    Sch. of Aerosp. Eng., Beijing Inst. of Technol., Beijing, China
  • Volume
    4
  • fYear
    2011
  • fDate
    10-12 June 2011
  • Firstpage
    53
  • Lastpage
    56
  • Abstract
    A autopilot designing method with Pole placement Method and State-Observer Feedback is proposed. State feedback gain via pole placement is designed by selecting a suitable root of closed-loop transfer function. With poles placement method full-order state observer with one or two measurable outputs are designed respectively. By comparing time-domain outputs of the two observers, It is concluded that, observer with two measurable outputs can be more accurate in the observation on the original system state under the condition of guaranteeing Filter characteristics.
  • Keywords
    closed loop systems; missile guidance; observers; state feedback; transfer functions; autopilot design; closed-loop transfer function; missile; pole placement method; state feedback gain; state-observer feedback; Damping; Equations; Extraterrestrial measurements; Mathematical model; Observers; State feedback; Time domain analysis; autopilot; pole placement; state-observer; statefeedback;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Computer Science and Automation Engineering (CSAE), 2011 IEEE International Conference on
  • Conference_Location
    Shanghai
  • Print_ISBN
    978-1-4244-8727-1
  • Type

    conf

  • DOI
    10.1109/CSAE.2011.5952802
  • Filename
    5952802