迷你飞机:设计、气动建模和稳定性

2014 11th International Conference on Electrical Engineering, Computing Science and Automatic Control (CCE) Pub Date : 2014-12-08 DOI:10.1109/ICEEE.2014.6978297

F. Guerrero, V. Martinez, O. García, D. Martinez-Vazquez

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引用次数: 0

摘要

本文介绍了一种小型飞机无人机的研制，重点介绍了其气动设计、建模和稳定性。采用欧拉-拉格朗日公式建立了飞行器的数学模型，并包含了设计的气动参数。为了保证系统的稳定性，提出了一种考虑气动参数和传感器带宽的经典控制律。最后给出了整车闭环系统的仿真结果。最后，气动设计和航空电子设备是基于飞行和操纵质量，以使迷你飞机执行可靠和稳定的飞行。

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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Mini airplane: Design, aerodynamic modeling and stability

This paper presents the development of a mini airplane UAV, focusing on the aerodynamic design, modeling and stability. Mathematical model of the vehicle is obtained using the Euler-Lagrange formulation and includes aerodynamic parameters of the design. For the stability, a classic control law is proposed taking in account the aerodynamic parameters and the sensors bandwidth implemented in the aircraft. Simulation results are shown for the closed-loop system of the vehicle. Finally, aerodynamic design and avionics are based on flying and handling qualities for having a mini airplane that performs a reliable and stable flight.

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2014 11th International Conference on Electrical Engineering, Computing Science and Automatic Control (CCE)

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