Abstract The laws of lateral motion control without data on the roll angle are proposed for aircraft with a single plane of symmetry. A procedure for analytical selection of the optimal gain in the aileron and rudder channels is proposed. The results of simulating the aircraft-autopilot system are presented.


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    Title :

    Aircraft lateral-directional control without a roll command in the autopilot


    Contributors:

    Published in:

    Publication date :

    2014-04-01


    Size :

    7 pages




    Type of media :

    Article (Journal)


    Type of material :

    Electronic Resource


    Language :

    English




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