可转换垂直起降飞行器的运动方程与纵向控制

2020 7th International Conference on Control, Decision and Information Technologies (CoDIT) Pub Date : 2020-06-29 DOI:10.1109/CoDIT49905.2020.9263980

R. Czyba, Grzegorz Kronhof

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引用次数: 1

摘要

本研究的目的是对垂直起降飞机由垂直向前飞过渡过程中的飞行动力学、稳定与控制进行数学建模。主要研究区域被简化为垂直平面上的二维情况。在Matlab/Simulink环境下对仿真飞行器进行了设计、分析和验证试验，为实际飞行垂直起降模型的建立提供了起点。

本文章由计算机程序翻译，如有差异，请以英文原文为准。

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Motion Equations and Longitudinal Control of a Convertible VTOL Aircraft

The purpose of this research is the mathematical modelling of flight dynamics, stabilizing and control of the Vertical Take-Off and Landing aircraft during its transition from vertical to forward flight. The main investigated area is reduced to a two-dimensional case in a vertical plane. The design, analysis and the validation tests have been undertaken on the simulation aerial vehicle in the Matlab/Simulink environment to provide starting point for real flying VTOL model build.

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2020 7th International Conference on Control, Decision and Information Technologies (CoDIT)

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