Requirements established for control about each of 3 axes became more restrictive when simultaneous control about 2 axes at time was evaluated; for VTOL aircraft in hovering flight, there was good correlation of 2 axes requirements with flight determined pilot ratings of controllability; gyroscopic coupling between pitch and yaw axes reduced controllability.


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    Title :

    Attitude control requirements for hovering determined through use of piloted flight simulator


    Additional title:

    NASA -- Tech Note


    Contributors:


    Publication date :

    1961


    Size :

    20 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :