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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    Titel :

    Aircraft longitudinal control without a pitch command in the autopilot


    Beteiligte:

    Erschienen in:

    Erscheinungsdatum :

    2014-10-01


    Format / Umfang :

    7 pages




    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch




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