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Dynamic modeling-based flight PD controller applied to an unmanned hexarotor helicopter

机译:基于动态建模的飞行PD控制器应用于无人六旋翼直升机

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In this paper, we describe the design and performance of a prototype multi-rotor unmanned aerial vehicle (UAV) platform featuring autonomous flying based on an inertial measurement unit (IMU) for use in bluetooth communication environments. Although there has been a fair amount of study on free-flying UAVs with multiple rotors, the more recent trend has been to outfit hexarotor UAVs with gimbals to support various services. This paper introduces the hardware and software systems for very compact and autonomous hexarotors, which can be used for search & rescue and surveillance missions without external assistance systems like ground station computers, high-performance remote control devices, or vision systems. This study included the construction of the test hexarotor platform, the implementation of an IMU, mathematical modeling, and simulation of the UAV. Furthermore, the hexarotor UAV with the implemented IMU was connected to a microcontroller unit (ARM-cortex) board. The microcontroller was able to control the rotational speed of the rotors and used the IMU measurements as input signals. A control simulation and experiment with the real system were implemented for the test platform, and the results were evaluated and compared.
机译:在本文中,我们描述了基于惯性测量单元(IMU)的具有自主飞行功能的原型多旋翼无人机(UAV)平台的设计和性能,该平台用于蓝牙通信环境。尽管对具有多旋翼的自由飞行无人机进行了大量研究,但最近的趋势是为六旋翼无人机配备万向架以支持各种服务。本文介绍了用于非常紧凑和自主的六旋翼飞机的硬件和软件系统,无需外部辅助系统(如地面站计算机,高性能远程控制设备或视觉系统),即可用于搜救和监视任务。这项研究包括测试六旋翼平台的构建,IMU的实现,数学建模以及无人机的仿真。此外,带有已实现IMU的六旋翼无人机被连接到微控制器单元(ARM-cortex)板上。微控制器能够控制转子的转速,并将IMU测量值用作输入信号。在测试平台上进行了真实系统的控制仿真和实验,并对结果进行了评估和比较。

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