A flight control system for an aircraft includes a flight control computer operatively interconnected with a main rotor system and a translational thrust system of the aircraft. A selectively enabled integrated target and flight control system arranged in communication with the flight control computer. The integrated target flight and control system is configured to control pitch attitude and heading of the aircraft. When the integrated target and flight control system is enabled, at least partial operation of the aircraft is controlled in response to a pilot input via the flight control computer.


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    Titel :

    ATTITUDE-COUPLED TARGETING SYSTEM FOR ROTARY WING AIRCRAFT


    Beteiligte:
    LUSZCZ MATTHEW T (Autor:in) / ADAMS DAVID L (Autor:in) / ALBER MARK R (Autor:in)

    Erscheinungsdatum :

    2017-12-07


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    G05D SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES , Systeme zum Steuern oder Regeln nichtelektrischer veränderlicher Größen / B64C AEROPLANES , Flugzeuge / F41G Zielvorrichtungen für Waffen , WEAPON SIGHTS



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