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.
Numerical and Experimental Design Parameter Analysis of VTOL Airframe Control Elements
Russ. Aeronaut.
Russian Aeronautics ; 63 , 1 ; 1-6
2020-01-01
6 pages
Article (Journal)
Electronic Resource
English
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