Approach to VTOL aircraft initial response criteria presented involves objective maneuver requirements based on mission of aircraft; example maneuver criterion, found to be valid for roll and pitch axes, is defined for helicopter-type operation; results are compared with accepted control requirements and flight and simulator data relating to pilot acceptance; 2 strong single-rotor configuration effects are discussed in relation to control criteria and test data interpretation; possible origin of minimum damping value is shown to relate to precision flight maneuver and pilot response time.


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    Titel :

    New control criteria for VTOL aircraft


    Weitere Titelangaben:

    Aerospace Eng


    Beteiligte:
    Lynn, R.R. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    1962


    Format / Umfang :

    10 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    Downwash Design Criteria for VTOL Aircraft

    Stanzione, K. / American Helicopter Society | British Library Conference Proceedings | 1993



    Research on vtol aircraft handling qualities criteria

    CLARK, J. W. / MILLER, D. P. | AIAA | 1965


    Research on VTOL aircraft handling qualities criteria

    Miller, D.P. / Clark, J.W. | Engineering Index Backfile | 1965


    Downwash Impingement Design Criteria for VTOL Aircraft

    M. M. George / A. A. Perlmutter / L. J. Butler | NTIS | 1964