Control power requirements are made up of stabilization and control of external disturbances, and basic maneuvering; stabilization required decreases with increasing design weight; maneuvering control required, however, is essentially independent of weight and may be installed in airplane as angular or as linear translation control; effect of gust environment on hovering VTOL transport is examined; factors to consider in control system design that affect performance and penalties associated with various control levels are outlined.


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    Titel :

    Control requirements and control methods for large V/STOL aircraft


    Weitere Titelangaben:

    SAE -- Paper


    Beteiligte:
    Lollar, T.E. (Autor:in) / Bus, F.J. (Autor:in) / Dolliver, D.M. (Autor:in)

    Kongress:

    SAE Meeting ; 1965



    Erscheinungsdatum :

    1965


    Format / Umfang :

    9 pages


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    Control Requirements and Control Methods for Large V/STOL Aircraft

    Dolliver, David M. / Bus, Frank J. / Lollar, Thomas E. | SAE Technical Papers | 1965



    V/STOL aircraft gas turbine requirements

    Robbins, O.G. | Engineering Index Backfile | 1967


    Control of V/STOL aircraft

    Franklin, J. A. | NTRS | 1986


    STOL Aircraft

    NTRS | 1988