Numerical and Experimental Design Parameter Analysis of VTOL Airframe Control Elements

Abstract

© 2020, Allerton Press, Inc. 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.