Novel Op-Amp based Hardware Design of Analog PID Circuit to Control the Altitude of Quadcopter

Blesson Easo Varghese, A. Swarup
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Abstract

Proportional Integral and Derivative (PID) control is a widely used control technique that can be used almost in all control applications. However, the practical implementation of the most often used digital PID control loop involves several aspects such as input signal sampling, Nyquist criterion, programming the control system on a microcontroller platform. On the other hand, processing of control signals on an analog continuous-time hardware platform overcomes the complexity of digital control synthesis, inaccuracies arising out of conversions between continuous and discrete time domains and are very much handy for simple control system design. Being aware that many electronic components can mimic the performance of real-world physical systems, this paper presents the design of an analog PID control system directly on the actual hardware to be used, with only limited electronic components and its application to a joystick controller for controlling the altitude of a quadcopter under varying load conditions and uncertainties. As the simulation of the design is carried out on the actual electronic circuit, various parameters like constraints, and propagation delay are considered from the initial stage of design, thereby giving a more practical, simple and straight forward approach.
基于运放的四轴飞行器高度控制模拟PID电路硬件设计
比例积分与导数(PID)控制是一种应用广泛的控制技术,几乎可以应用于所有的控制领域。然而,最常用的数字PID控制回路的实际实现涉及到输入信号采样、奈奎斯特准则、在单片机平台上对控制系统进行编程等几个方面。另一方面,在模拟连续时间硬件平台上处理控制信号,克服了数字控制合成的复杂性和连续与离散时域转换带来的不准确性,对简单的控制系统设计非常方便。意识到许多电子元件可以模仿现实世界物理系统的性能,本文提出了一个模拟PID控制系统的设计直接在实际硬件上使用,只有有限的电子元件及其应用于操纵杆控制器,用于控制四轴飞行器在不同负载条件和不确定性下的高度。由于设计的仿真是在实际的电子电路上进行的,因此从设计的初始阶段就考虑了约束、传播延迟等各种参数,从而使设计方法更加实用、简单和直接。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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