Abstract The laws of longitudinal motion control without data on the pitch angle are proposed. A procedure for analytical selection of the optimal gain in the elevator channel is proposed. The results of simulating the aircraft-autopilot system are presented.


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    Title :

    Aircraft longitudinal control without a pitch command in the autopilot


    Contributors:

    Published in:

    Publication date :

    2014-10-01


    Size :

    7 pages




    Type of media :

    Article (Journal)


    Type of material :

    Electronic Resource


    Language :

    English




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