A tail sitter aircraft (10) is capable of forward flight and hover operations. The tail sitter aircraft (10) includes a wing (12, 13) and first (14) and second (15) prop-nacelles supportively disposed on the wing. Each of the first and second prop-nacelles includes an articulable rotor (20), which is rotatable about variable rotational axes and which includes blades (22) that are collectively and cyclically controllable in both forward flight and hover regimes.


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    Title :

    CONTROL SYSTEM AND STRATEGY FOR TAIL SITTER


    Additional title:

    STEUERUNGSSYSTEM UND -STRATEGIE FÜR EINEN AUF DEM HECK STEHENDEN SENKRECHTSTARTER
    SYSTÈME DE COMMANDE ET STRATÉGIE POUR PERSONNE ASSISE À L'ARRIÈRE


    Contributors:

    Publication date :

    2019-05-22


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

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



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