We consider the problem of designing stabilizing control laws for flight over a broad range of angles-of-attack which also serve to signal the pilot of impending stall. The paper employs bifurcation stabilization coupled with more traditional linear control system design. To focus the discussion, a detailed analysis is given for a model of the longitudinal dynamics of an F-8 Crusader.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Nonlinear Stabilization of High Angle-of-Attack Flight Dynamics Using Bifurcation Control


    Contributors:
    E. H. Abed (author) / H. Lee (author)

    Publication date :

    1990


    Size :

    11 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English