Quadcopter Prototype Stability Assessment With Pid Controller And Euler-Lagrange Approach-Reference-Cited by-同舟云学术

Quadcopter Prototype Stability Assessment With Pid Controller And Euler-Lagrange Approach

Published:2023-09-01 Issue:1 Volume:23 Page:15-20
ISSN:2286-2455
Container-title:The Scientific Bulletin of Electrical Engineering Faculty
language:en
Short-container-title:

Author:

Djizi Hamza¹²,Zahzouh Zoubir³,Bouzaouit Azzedine⁴

Affiliation:

1. Department of Mechanical Engineering , Mohamed Cherif Messaadia University , P.O. Box 1553, Souk-Ahras , , Algeria

2. INFRA-RES Laboratory , Mohamed Cherif Messaadia University , Algeria

3. Laboratoire de Recherche en Électromécanique et Sûreté de Fonctionnement, LRESF Laboratory , Mohamed Chérif Messaadia University , P.O. Box 1553 , Souk-Ahras , , Algeria

4. University of 20 August 1955 Skikda , Algeria

Abstract

Abstract The increasing use of drones in various fields has led to their popularity in developed countries due to their ease of use and manufacture. This Miniature Pilotless Aircraft has numerous beneficial usages such as express shipping, gathering information, crop monitoring, cargo transport, storm tracking, geographic mapping of inaccessible terrain, search and rescue operations, among others. This study aims to investigate the stability of a quadcopter through simulations based on the mathematical model that describes the quadcopter’s dynamic and flight mechanics, using the Euler-Lagrange approach. It conducts simulations in MATLAB and present the principles that govern quadcopter stability, focusing on setting the PID coefficients to achieve optimal stability. This study provides insights into the principles of drone mechanics and stability, enabling us to better understand the quadcopter’s behavior and performance.

Publisher

Walter de Gruyter GmbH

Subject

General Medicine

Link

https://www.sciendo.com/pdf/10.2478/sbeef-2023-0003

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