Augmentation theory is discussed; prototype hover-augmentation system that reduces pilot's task in maintaining position with respect to inertial reference; system modifies response characteristic of aircraft by feedback of inertially derived acceleration and velocity information to reduce number of integrations between command and aircraft position change.


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    Title :

    Path-damping system for VTOL aircraft


    Additional title:

    Sperry Eng Rev


    Contributors:

    Published in:

    Publication date :

    1967


    Size :

    7 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :


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