Fluidic flight control system has been flight tested to develop and evaluate vortex rate sensors, fluidic amplifiers, dynamic shaping techniques and system accuracy; results which have confirmed applicability of conventional control theory and projected high reliability; stabilization system featuring electropneumatic servo actuator with variable transfer function and unique characteristics for application to range of stabilization problems; recent electronic system studies have been substantial improvement in reliability, maintainability, size, weight and cost reduction by use of microelectronic functional modules as alternates to individually-mounted discrete components.


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    Title :

    Automatic flight control development for general aviation


    Additional title:

    SAE -- Paper


    Contributors:

    Conference:

    SAE Meeting ; 1967 Control equipment



    Publication date :

    1967


    Size :

    11 pages


    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English


    Keywords :


    Automatic Flight Control Development for General Aviation

    Vetter, Lee J. | SAE Technical Papers | 1967



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