• DocumentCode
    487576
  • Title

    Robust Control Strategy for Take-Off Performance in a Windshear

  • Author

    Chen, Y.H. ; Pandey, S.

  • Author_Institution
    Department of Mechanical and Aerospace Engineering, Syracuse University, Syracuse, New York 13244
  • fYear
    1988
  • fDate
    15-17 June 1988
  • Firstpage
    2244
  • Lastpage
    2249
  • Abstract
    A robust control strategy has been studied for an aircraft during take-off. Effect of different windshear intensities have been analyzed for different models. As the complexity of the model increases and as more complete model is taken into account the survivability of the aircraft degrades. However, the robust control strategy yields results which are comparable to the best known results. The robust control is designed via a deterministic approach. The only information it utilizes is the upperbound value of the allowable control magnitude. The resulting system behavior is also described in a deterministic way, namely, the stability.
  • Keywords
    Aerodynamics; Aerospace control; Aerospace electronics; Aerospace engineering; Air accidents; Aircraft propulsion; Degradation; Instruments; Robust control; Stability;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    American Control Conference, 1988
  • Conference_Location
    Atlanta, Ga, USA
  • Type

    conf

  • Filename
    4790097