Mathematical modelling and PID control system implementation for quadcopter frame Tarot FY650

IF 1.2 4区工程技术 Q3 ENGINEERING, AEROSPACE

Aircraft Engineering and Aerospace Technology Pub Date : 2024-01-12 DOI:10.1108/aeat-06-2023-0154

Gowtham G., Jagan Raj R.

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引用次数: 0

Abstract

Purpose

The purpose of this study is to find the suitable trajectory path of the Numerical model of the Quadcopter. Quadcopters are widely used in various applications due to their compact size and ease of assembly. Because they are quite unstable, autonomous control systems would be used to overcome this problem. Modelling autonomous control is predominant as the research scope faces challenges because of its highly non-linear, multivariable system with 6 degree of freedom.

Design/methodology/approach

Quadcopters with antonym systems can operate in an unknown environment by overcoming unexpected disturbances. The first objective when designing such a system is to design an accurate mathematical model to describe the dynamics of the system. Newton’s law of motion was used to build the mathematical model of the system.

Findings

Establishment of the mathematical model and the physics behind a four propeller drone for the frame TAROT 650 carbon was done. Simulink model was developed based on the mathematical model for simulating the complete dynamics of the drone as well as location and gusts were included to check the stability.

Originality/value

The control response of the system was simulated numerically results are discussed. The trajectory path was found. The phases with their own parameters can be used to implement the mathematical model for another type of quadcopter model and achieve quick development.

查看原文本刊更多论文

四旋翼飞行器 Tarot FY650 的数学建模和 PID 控制系统实现

目的本研究的目的是找到四旋翼飞行器数值模型的合适轨迹路径。四旋翼飞行器因其体积小巧、易于组装而被广泛应用于各种领域。由于它们相当不稳定，因此需要使用自主控制系统来克服这一问题。由于其高度非线性、多变量系统具有 6 个自由度，因此自主控制建模是研究范围面临的主要挑战。设计此类系统的首要目标是设计一个精确的数学模型来描述系统的动态。研究结果建立了数学模型和 TAROT 650 碳框架四螺旋桨无人机背后的物理学原理。在数学模型的基础上开发了 Simulink 模型，用于模拟无人机的完整动态以及位置和阵风，以检查稳定性。找到了轨迹路径。各阶段的参数可用于为其他类型的四旋翼模型建立数学模型，实现快速开发。

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

Aircraft Engineering and Aerospace Technology 工程技术-工程：宇航

CiteScore

3.20

自引率

13.30%

发文量

168

审稿时长

8 months

期刊介绍： Aircraft Engineering and Aerospace Technology provides a broad coverage of the materials and techniques employed in the aircraft and aerospace industry. Its international perspectives allow readers to keep up to date with current thinking and developments in critical areas such as coping with increasingly overcrowded airways, the development of new materials, recent breakthroughs in navigation technology - and more.