This paper presents results from an application of H(infinity) control design methodology to a centralized integrated flight/propulsion control (IFPC) system design for a supersonic STOVL fighter aircraft in transition flight. The overall design methodology consists of a centralized IFPC design with controller partitioning. Design and evaluation vehicle models are summarized, and insight is provided into formulating the H(infinity) control problem such that it reflects the IFPC design objective. The H(infinity) controller is shown to provide decoupled command tracking for the design model. The controller order could be significantly reduced by modal residualization of the fast controller modes without any deterioration in performance.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    H-infinity based integrated flight/propulsion control design for a STOVL aircraft in transition flight


    Contributors:

    Conference:

    AIAA Guidance, Navigation and Control Conference ; 1990 ; Portland, OR, United States


    Publication date :

    1990-01-01


    Type of media :

    Conference paper


    Type of material :

    No indication


    Language :

    English





    H-infinity based integrated flight-propulsion control design for a STOVL aircraft in transition flight

    Garg, Sanjay / Mattern, Duane L. / Bright, Michelle M. et al. | NTRS | 1990


    H-infinity based integrated flight/propulsion control design for a STOVL aircraft in transition flight

    GARG, SANJAY / MATTERN, DUANE / BRIGHT, MICHELLE et al. | AIAA | 1990


    Integrated flight/propulsion control for supersonic STOVL aircraft

    Franklin, James A. / Stortz, Michael W. / Mihaloew, James R. | NTRS | 1990