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.

中文翻译：

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VTOL机体控制元件的数值和实验设计参数分析

本文介绍了选择VTOL无人机的操纵面设计参数和升力发动机特性的计算和实验研究。分析了侧倾，俯仰和偏航控制和稳定方程的一般结构方案。给出了点对点自主飞行的数值模拟结果。