Results of a NASA sponsored study of V/STOL Propulsion Control Analysis are presented. The study involved propulsion control requirements, design concepts and procedures, and control designs for supersonic V/STOL. A variable cycle engine with a remote augmented lift system was used as a basis for establishing typical operating requirements and control concepts, and a nonlinear engine model was developed for control development as a precursor to a real-time simulation capability. A simplified aircraft model was also used to investigate transition requirements, and a long-range technology plan was developed to define subsequent program requirements for achieving a real-time piloted simulation capability.


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    Title :

    V/STOL propulsion control technology


    Contributors:
    Brown, H. (author)

    Conference:

    V/STOL Conference ; 1981 ; Palo Alto, CA


    Publication date :

    1981-12-01


    Type of media :

    Conference paper


    Type of material :

    No indication


    Language :

    English







    V/STOL propulsion

    Diedrich, J. H. / Hassell, J. L., Jr. / Hickey, D. H. et al. | NTRS | 1971


    STOL propulsion systems

    Denington, R. J. / Koenig, R. W. / Vanco, M. R. et al. | NTRS | 1972