• DocumentCode
    2098346
  • Title

    High Gain Observer Design for Eth Helicopter

  • Author

    Ullah, Naeem ; Qayyum Khan, A. ; Mustafa, Ghulam ; Yousuf, M.

  • Author_Institution
    Dept. of Electr. Eng., Pakistan Inst. of Eng. & Appl. Sci., Islamabad
  • fYear
    2006
  • fDate
    13-14 Nov. 2006
  • Firstpage
    330
  • Lastpage
    333
  • Abstract
    This paper deals with the design of a high gain observer (HGO) for the ETH helicopter laboratory process. The standard format of high gain observer is used and the parameters of the observer are selected in such away that the observer gain matrix H0 becomes Hurwitz. The observer not only estimates the angular positions and velocities of the system but also rejects the disturbance and the measurement noise. The simulation results show the effectiveness of the HGO
  • Keywords
    control system synthesis; helicopters; nonlinear control systems; observers; robust control; ETH helicopter; angular position estimation; disturbance rejection; high gain observer design; noise measurement; observer gain matrix; Control systems; Helicopters; Linear feedback control systems; Noise measurement; Nonlinear control systems; Nonlinear dynamical systems; Nonlinear systems; Observers; Position measurement; Velocity measurement;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Emerging Technologies, 2006. ICET '06. International Conference on
  • Conference_Location
    Peshawar
  • Print_ISBN
    1-4244-0502-5
  • Electronic_ISBN
    1-4244-0503-3
  • Type

    conf

  • DOI
    10.1109/ICET.2006.335980
  • Filename
    4136947
    • Link To Document
    https://search.isc.ac/dl/search/defaultta.aspx?DTC=49&DC=2098346