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.


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    Title :

    Guidance for a tilt rotor VTOL aircraft during takeoff and landing


    Contributors:

    Publication date :

    1972-12-01


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English


    Keywords :



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