A brief overview of the (DAP) Dynamic Autopilot is given. Results of the dynamic interaction study of the Orbiter with the General Dynamics Beam are presented. Preliminary results of the three degree of freedom payload parametric study are also presented.


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    Title :

    Shuttle flight control and structure interaction


    Contributors:


    Publication date :

    1983-04-01


    Type of media :

    Conference paper


    Type of material :

    No indication


    Language :

    English




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