VTOL configurations are divided into single engine, centrally grouped lift engines, and distributed lift engines; precise control of flight is needed because of small landing areas and complex control required for and transition to wingborne flight; general requirement for artificial stability augmentation of VTOL aircraft supported by relatively concentrated flow of lifting air; attitude, height and speed control; details of flight director which provides all data requiring prompt response by pilot; data are presented by means of flight-path ball, which moves relative to horizon line in response to angle of descent.


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    Titel :

    Control of VTOL aircraft


    Weitere Titelangaben:

    Sperry Eng Rev


    Beteiligte:
    Sullivan, N. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    1963


    Format / Umfang :

    8 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


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