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首页> 外文期刊>Journal of Intelligent & Robotic Systems: Theory & Application >PID and LQ Regulation of a Multirotor Attitude: Mathematical Modelling, Simulations and Experimental Results
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PID and LQ Regulation of a Multirotor Attitude: Mathematical Modelling, Simulations and Experimental Results

机译:多旋翼姿态的PID和LQ调节:数学建模,仿真和实验结果

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摘要

Multirotors have been recognized to be particularly interesting for surveillance, search and rescue, imaging and more, because of their several advantages as the high maneuverability and the vertical take off and landing capability. This paper presents the experimental results of the application of a Proportional Integral Derivative control law and a Linear Quadratic Regulation technique to the attitude of a multirotor. The reader is driven through all the main steps required to reach this goal, starting from the derivation of the mathematical model and the control laws, to the simulations and the experimental tests.
机译:多旋翼飞机由于具有高机动性和垂直起降能力等诸多优势,因此被认为对于监视,搜索和救援,成像等特别感兴趣。本文介绍了将比例积分微分控制律和线性二次调节技术应用于多旋翼姿态的实验结果。从数学模型和控制律的推导,到仿真和实验测试,读者将被驱动完成此目标所需的所有主要步骤。

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