Abstract Problems associated with determining the angular attitude of the unmanned aerial vehicle (UAV) with an inertial navigation system are considered. Some ways of its practical implementation using special test benches are proposed.


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    Title :

    Numerical and Experimental Analysis in Adjustment of the VTOL UAV Control Hardware



    Published in:

    Russian Aeronautics ; 61 , 4 ; 605-612


    Publication date :

    2018-10-01


    Size :

    8 pages




    Type of media :

    Article (Journal)


    Type of material :

    Electronic Resource


    Language :

    English




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