Results of study of propulsion system/control system interface for several V/STOL hover control concepts in aircraft using lift plus lift-cruise propulsion concept; control concepts included are proportional reaction controls using lift engine compressor bleed air, engine thrust modulation, and engine thrust vectoring; effects on control system performance of reaction control thrust augmentation by duct burning are shown; concepts are applied to three subsonic V/STOL strike-reconnaissance fighter aircraft of different gross weights, and comparison of concepts on basis of bleed air requirements, thrust-to-weight ratio penalties, and lift engine operating limitations is made.


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    Titel :

    V/STOL hover control system analysis


    Weitere Titelangaben:

    J Aircraft


    Beteiligte:

    Erschienen in:

    Erscheinungsdatum :

    1966


    Format / Umfang :

    9 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    V/STOL Hover Control System Analysis

    WILLIAM T. STEILS | AIAA | 1966


    V/STOL hover control system analysis

    STEILS, JR., W. | AIAA | 1965


    V/STOL hover stability impact on hover control task

    Whitaker, A. B. / Kelly, C. P. / Wittman, R. B. et al. | NTRS | 1977



    A unique facility for V/STOL aircraft hover testing

    Culpepper, Richard G. | TIBKAT | 1979