A perturbation guidance scheme is developed to keep a tilt-rotor VTOL aircraft close to a predetermined nominal flight path during take-off and landing. A simulation of the guidance scheme applied to the Bell Model 266 tilt-rotor VTOL gave satisfactory behavior in the presence of initial errors and wind disturbances. (Author)


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    Titel :

    Guidance for a Tilt Rotor VTOL Aircraft During Takeoff and Landing


    Beteiligte:
    N. K. Gupta (Autor:in) / A. E. Bryson (Autor:in)

    Erscheinungsdatum :

    1972


    Format / Umfang :

    116 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




    Guidance for a tilt rotor VTOL aircraft during takeoff and landing

    Gupta, N. K. / Bryson, A. E., Jr. | NTRS | 1972


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