| 四轴飞行器控制系统设计与实现 |
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| 引用本文： | 茹岩,张欣. 四轴飞行器控制系统设计与实现[J]. 电子测试, 2022, 0(3): 42-45,49. DOI: 10.3969/j.issn.1000-8519.2022.03.012 |
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| 作者姓名： | 茹岩 张欣 |
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| 作者单位： | 柳州铁道职业技术学院,广西柳州,545616 |
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| 基金项目： | 基于变论域模糊PID的四轴飞行器控制系统设计与实现(2020KY44011)。 |
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| 摘 要： | 设计了一种基于捷连贯性导航的四轴飞行器控制策略,采用串级PID控制方法,在惯性导航学的基础上,综合比较了在运用互补滤波和卡尔曼滤波融合算法情况下飞行器的平衡效果和动态响应性能.实验结果表明运用互补滤波的串级PID平衡控制策略能够较好的控制四轴飞行器的平衡性,有较强的鲁棒性和抗干扰性.
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| 关 键 词： | 姿态检测 数据融合 串级PID |
Design and implementation of four axis aircraft control system |
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| Ru Yan,Zhang Xin. Design and implementation of four axis aircraft control system[J]. Electronic Test, 2022, 0(3): 42-45,49. DOI: 10.3969/j.issn.1000-8519.2022.03.012 |
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| Authors: | Ru Yan Zhang Xin |
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| Affiliation: | (Liuzhou Railway Vocational Technical College,Liuzhou Guangxi,545616) |
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| Abstract: | A four axis aircraft control strategy based on agile coherent navigation is designed.The cascade PID control method is adopted.On the basis of inertial navigation,the balance effect and dynamic response performance of the aircraft are comprehensively compared when the fusion algorithm of complementary filter and Kalman filter is used.The experimental results show that the cascade PID balance control strategy using complementary filter can better control the balance of four-axis aircraft,and has strong robustness and anti-interference. |
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| Keywords: | attitude detection Data fusion Cascade PID |
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