A tail sitter aircraft is capable of forward flight and hover operations. The tail sitter aircraft includes a wing and first and second prop-nacelles supportively disposed on the wing. Each of the first and second prop-nacelles includes an articulable rotor, which is rotatable about variable rotational axes and which includes blades that are collectively and cyclically controllable in both forward flight and hover regimes.


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    Titel :

    CONTROL SYSTEM AND STRATEGY FOR TAIL SITTER


    Beteiligte:
    KUBIK STEPHEN (Autor:in) / DRISCOLL JOSEPH T (Autor:in) / D'ANNA FRANK P (Autor:in) / ALBER MARK R (Autor:in) / LAUDER TIMOTHY FRED (Autor:in) / FEGELY CODY (Autor:in)

    Erscheinungsdatum :

    26.01.2017


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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