Cascaded Control System Design for Quadrotor UAV through Relay with Embedded Integrator-Based Automatic Tuning Approach

IF 1.1 4区 工程技术 Q3 ENGINEERING, AEROSPACE International Journal of Aerospace Engineering Pub Date : 2023-10-10 DOI:10.1155/2023/6651286
Ayaz Ahmed Hoshu, Ghulam E Mustafa Abro, Musaed Alhussein, Irfan Ali Tunio, Khursheed Aurangzeb, Anwar Ali
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Abstract

Due to their enormous characteristics and applicability, quadrotor unmanned aerial vehicles (UAVs) have enjoyed much popularity lately. However, designing a stable control strategy for quadrotors still remains one of the major concerns mainly due to the requirement of an accurate system model. They are naturally underactuated systems, with complex and nonlinear dynamics as well as interaxes couplings. Considering the dynamical complexities of these vehicles, one of the efficient methods is to utilize the relay feedback experiments and automatic tuning approach to tackle these issues. This paper investigates the employment of the relay with embedded integrator approach, wherein the quadrotor dynamics are estimated effectively with minimal parameters as compared to previously utilized relay with hysteresis technique. Frequency sampling filter (FSF) is further utilized for the extraction of the needful data through the signals obtained using the relay experiments, followed by the estimation of the plant dynamics. PID controllers have then been developed using the approximated quadrotor models. Which are used in the proposed cascade control structure for the quadrotor. The demonstrated results and analysis present the efficacy of designed control system technique for the quadrotor UAV.
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基于嵌入式积分器的四旋翼无人机继电器级联控制系统设计
四旋翼无人机(uav)由于其巨大的特性和适用性,近年来受到了广泛的欢迎。然而,由于需要精确的系统模型,设计稳定的控制策略仍然是四旋翼飞行器的主要关注点之一。它们是自然欠驱动系统,具有复杂的非线性动力学和轴间耦合。考虑到这些车辆的动力学复杂性,利用继电器反馈实验和自动调谐方法来解决这些问题是有效的方法之一。本文研究了采用嵌入式积分器方法的继电器,其中四旋翼动力学有效地估计与最小参数相比,以前使用的继电器与滞后技术。利用频率采样滤波器(FSF)从继电器实验得到的信号中提取所需的数据,然后对被测对象进行动态估计。然后使用近似的四旋翼模型开发了PID控制器。将其应用于四旋翼飞行器的串级控制结构中。仿真结果和分析表明,所设计的四旋翼无人机控制系统技术是有效的。
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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来源期刊
CiteScore
2.70
自引率
7.10%
发文量
195
审稿时长
22 weeks
期刊介绍: International Journal of Aerospace Engineering aims to serve the international aerospace engineering community through dissemination of scientific knowledge on practical engineering and design methodologies pertaining to aircraft and space vehicles. Original unpublished manuscripts are solicited on all areas of aerospace engineering including but not limited to: -Mechanics of materials and structures- Aerodynamics and fluid mechanics- Dynamics and control- Aeroacoustics- Aeroelasticity- Propulsion and combustion- Avionics and systems- Flight simulation and mechanics- Unmanned air vehicles (UAVs). Review articles on any of the above topics are also welcome.
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