TEKF.21.12
Quadrotor, which is used in many fields and is still a challenge to control, has a complex kinematic and dynamic system, and its flight performance depends on many variables that need to be controlled simultaneously. In this study, the effective determination of PID parameters for altitude control of quadrotors, which presents a complex control problem, has been tested comparatively with innovative metaheuristic approaches. Among the strong metaheuristic algorithms, Crow Search Algorithm (CSA), Particle Swarm Optimization Algorithm (PSO), Golden Jackal Optimization Algorithm (GJO), and Jellyfish Search Algorithm (JSA) were comparatively analyzed for the determination of PID parameters. The parameters obtained with CSA caused the minimum steady-state error with the value of 6.9580e-04 in the closed-loop control system. A minimum overshoot was also obtained with the parameters optimized with CSA. When these results are evaluated, it can be said that CSA performs better than other altitude control algorithms, considering the quadrotor's stable and accurate positioning performance.
Crow Search Algorithm Golden Jackal Optimization Algorithm Jellyfish Search Algorithm Parameter Optimization Particle Swarm Optimization Algorithm quadrotor
This Study Does Not Need Ethics Committee Approval
FUBAP
TEKF.21.12
This study was derived from Master's thesis numbered 836713 of Muhammed Kıvanc KURNAZ under the supervision of Assoc. Dr. Gonca OZMEN KOCA. This study was also supported by Scientific Research Unit of Firat University (FUBAP) under the Grant Number TEKF.21.12. The authors thank to FUBAP for their supports.
Primary Language | English |
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Subjects | Electrical Engineering (Other) |
Journal Section | Articles |
Authors | |
Project Number | TEKF.21.12 |
Early Pub Date | June 30, 2025 |
Publication Date | June 30, 2025 |
Submission Date | October 14, 2024 |
Acceptance Date | February 24, 2025 |
Published in Issue | Year 2025 Volume: 9 Issue: 1 |
This work is licensed under CC BY-NC 4.0