A new computational method was developed that enables preliminary tuning of Auto Pilot System internal parameters based on time response analysis of the aircraft and its auto pilot. This method main purpose is to reduce flight tests during Auto Pilot calibration procedure.


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    Title :

    Autopilot System Tuning


    Additional title:

    Sae Technical Papers


    Contributors:

    Conference:

    SAE Brasil ; 1993



    Publication date :

    1993-10-01




    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English




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