A fly by wire system in the collective control system for XV-15 Tilt Rotor Research Aircraft was evaluated. The collective control system was selected because it requires a system tracking accuracy between right and left rotors of approximately 0.1%. The performance characteristics of the collectors axel provide typical axis control response data. The demonstrator is bread boarded as a dual system instead of the triplex system.


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    Title :

    Xv-15 Tilt Rotor Fly-by-Wire Collective Control Demonstrator Development Specifications


    Contributors:

    Publication date :

    1981


    Size :

    34 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English





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