Program used subsonic jet propelled fighter aircraft to investigate capabilities of normal acceleration command control system, pitch rate command control system, and pitch damper system; with given stability characteristics pilots doubted that any type of military mission could be accomplished; it was found that with any of three systems flying qualities were definitely superior to those of basic aircraft.


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    Title :

    Flight investigations of automatic stabilization of airplane having static longitudinal instability


    Additional title:

    NASA -- Tech Note


    Contributors:


    Publication date :

    1959


    Size :

    32 pages


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :