Integration of suitable flight controls into X-15 was task of using analytical methods of flight dynamics and analog computing equipment and flight-control simulators to formulate system providing satisfactory control characteristics throughout flight envelope; operating characteristics of rate command, tandem, single motor, and solenoid bypass system; evaluation of proposed configuration and block diagram showing final solenoid bypass system; rate damping integrated. (p 36-37, 74, 76, 78, 80)


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    Title :

    Systems approach to flight controls


    Additional title:

    Astronautics


    Contributors:

    Published in:

    Astronautics ; 7 , n 5


    Publication date :

    1962


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English




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