• DocumentCode
    622557
  • Title

    Aircraft control surface failure accommodation utilizing linear regulation and switching control

  • Author

    Salman, Mishah Uzziel ; Chang, Bo-Yan

  • Author_Institution
    Dept. of Mech. Eng. & Mech., Drexel Univ., Philadelphia, PA, USA
  • fYear
    2013
  • fDate
    12-14 June 2013
  • Firstpage
    1561
  • Lastpage
    1566
  • Abstract
    An actuator jam failure is mitigated using a servomechanism formulation where the failed control surface is modeled as an exogenous input to the degraded plant. The approach exploits switching control, linear output regulation, H2 control theory, and an outer-loop PI control algorithm to track a desired reference input. Application is demonstrated using the nonlinear NASA AirSTAR Generic Transport Model (GTM).
  • Keywords
    H2 control; PI control; aircraft control; nonlinear control systems; servomechanisms; time-varying systems; GTM; H2 control theory; actuator jam failure mitigation; aircraft control surface failure accommodation; exogenous input; linear output regulation; nonlinear NASA AirSTAR Generic Transport Model; outer-loop PI control algorithm; servomechanism; switching control; Actuators; Aerospace control; Aircraft; Elevators; Equations; Mathematical model; Steady-state;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Control and Automation (ICCA), 2013 10th IEEE International Conference on
  • Conference_Location
    Hangzhou
  • ISSN
    1948-3449
  • Print_ISBN
    978-1-4673-4707-5
  • Type

    conf

  • DOI
    10.1109/ICCA.2013.6564984
  • Filename
    6564984
    • Link To Document
    https://search.isc.ac/dl/search/defaultta.aspx?DTC=49&DC=622557