带有比例导数控制器的四旋翼模型

H. A. Rozi, E. Susanto, Ig. Prasetya Dwibawa
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引用次数: 3

摘要

跟踪系统的自动控制器设计通常可以通过分析响应输出系统来实现。然而,在许多情况下,特别是在复杂的动力学系统,如四旋翼控制器,这是不平凡的结束。四旋翼飞行器的控制设计可以通过动力学系统建模来完成。当动力学系统的建模能够接近实际系统特性时,就可以方便地进行准确的分析和系统修改。提出了四元数方法对四旋翼飞行器姿态进行建模。仿真结果表明了比例导数控制器设计方法对该模型的有效性。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Quadrotor model with proportional derivative controller
To design an automatic controller of a tracking system usually can be built by analyzing response output system. However in many cases especially in complex dynamics system for example quadrotor controller, it is not trivial to end this. Control design for quadrotor can be done by modeling the dynamics system. When dynamics system can be modeled close to real system characteristics, then accurate analysis and system modification will be obtained easily. The work proposed quaternion method to model the quadrotor attitude. The simulation shows the effectiveness method for proportional derivative controller design to the model.
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