The paper describes the computational and experimental investigation in selecting the design parameters of control surfaces and characteristics of the lift engines of a VTOL unmanned aerial vehicle. The general structural scheme of equations to roll, pitch and yaw control and stabilization is analyzed. Results of numerical simulation of the point-to-point autonomous flight are given.


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    Title :

    Numerical and Experimental Design Parameter Analysis of VTOL Airframe Control Elements


    Additional title:

    Russ. Aeronaut.


    Contributors:

    Published in:

    Russian Aeronautics ; 63 , 1 ; 1-6


    Publication date :

    2020-01-01


    Size :

    6 pages




    Type of media :

    Article (Journal)


    Type of material :

    Electronic Resource


    Language :

    English





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