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Mechatronics Application Using Characteristics Polynomial Control Approach With Case Study: Development of A Simulated Air Speed Indicator for Helicopter Simulator

机译:使用特征多项式控制方法的机电一体化应用案例研究:用于直升机模拟器的模拟风速指示器的开发

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摘要

A helicopter simulator has to be built to fully resemble the real cockpit environment including its instrument indicating air speed. This paper is aimed to apply mechatronics technology in development of a Simulated Air Speed Indicator (SASI) that can be used for a helicopter simulator. This indicator has a pointer which indicates a certain value at the dial depending on the simulated air speed signal sent by the host computer. The driving mechanism of this mechatronics system is composed mainly of dc motor, reduction gear, pointer and potentiometer. An analog positioning controller has been developed based on characteristics polynomial control approach. The performance of the developed instrument was validated through step response and precision repetitive experiments. From the experimental results, it is obtained that the controller with proportional gain of K_p = 30 gives steady state error of 0.14% and repetition error of 0.3 (knots).
机译:必须建造直升机模拟器,使其完全类似于真实的驾驶舱环境,包括其指示风速的仪器。本文旨在将机电一体化技术应用于可用于直升机模拟器的模拟空速指示器(SASI)的开发中。该指示器具有一个指针,该指针根据主机发送的模拟风速信号在刻度盘上指示某个值。该机电一体化系统的驱动机构主要由直流电动机,减速齿轮,指针和电位计组成。已经基于特征多项式控制方法开发了模拟定位控制器。通过阶跃响应和精密重复实验验证了所开发仪器的性能。从实验结果可以看出,比例增益为K_p = 30的控制器的稳态误差为0.14%,重复误差为0.3(节)。

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