New design philosophy is that controls and other functional systems, formerly designed separately or by different subcontractors, must be treated as one complete flight control system with aircraft itself to insure acceptable flying conditions over entire mission profile; requirements of automatic systems designed on this basis; consideration of piloted and of automatic loop.


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    Title :

    Automatic flight control systems requirements for high performance fighter aircraft


    Additional title:

    Soc Automotive Engrs -- Paper


    Contributors:

    Conference:

    Society of Automotive Engineers -- Meeting ; 1957 Control equipment



    Publication date :

    1957


    Size :

    6 pages


    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English


    Keywords :




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