低成本固定翼无人机控制规律的发展

Proceedings of the 16th International Conference on Mechatronics - Mechatronika 2014 Pub Date : 2014-12-01 DOI:10.1109/MECHATRONIKA.2014.7018264

D. Kraus, J. Němeček

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引用次数: 0

摘要

该项目侧重于模拟和真实无人机平台的发展，用于测试飞行控制算法。本文的目的是在Matlab/Simulink环境下开发一个利用无人机非线性和线性化模型进行控制器初始设计的平台。一旦控制器经过设计、调试和仿真验证，就可以使用自动代码生成将其加载到低成本的无人机平台上。在真实环境下的真实平面上对该方法进行了验证。

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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Low cost fixed wing UAV for development of control laws

The project is focused on the development of both simulated and real UAV platform for testing of flight control algorithms. The aim of this paper was to develop a platform that allows initial design of controllers using non-linear and linearized model of UAV in Matlab/Simulink environment. Once the controllers are designed, tuned and verified in simulation, it can then be loaded into low cost UAV platform using automated code generation. The approach was verified on real plane in real environment.

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Proceedings of the 16th International Conference on Mechatronics - Mechatronika 2014

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