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Journals / European Mechanical Science / 2023 / Cilt: 7 Sayı: 4

Metaheuristic algorithm-based cascade PID controller design for fixed wing unmanned aerial vehicle

Mehmet DURMAZ
Kenan CİCİ
Muhammet SARIKAYA
Mesut BİLİCİ
Hasan Hüseyin BİLGİÇ
Pages
230–237
Publication Date
2023-12-20
DOI
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AI Summary & Key Takeaways

AI Insight
⚡ TL;DR(Too Long; Didn't Read)

Controller performances were tested in simulation environment for unit step input responses., Considering the longitudinal dynamics of the aircraft, among the ITAE, ISE, MSE, and IAE fitness functions, IAE can be shown as the optimum result for altitude control.

📌 3 Key Takeaways

🎯
Objective & Hypothesis:In this study, the nonlinear model of the longitudinal motion and altitude of a fixed-wing unmanned aerial vehicle with assured geometrical features and aerodynamic parameters is linearized under certain conditions.
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Key Findings & Data:A cascade Proportional Integral Differential Controller is designed on the linear model.
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Conclusion & Impact:Controller performances were tested in simulation environment for unit step input responses., Considering the longitudinal dynamics of the aircraft, among the ITAE, ISE, MSE, and IAE fitness functions, IAE can be shown as the optimum result for altitude control.
🔬Design:Modeling & Simulation
📍Scope:Comprehensive Sample
⚙️Variables:Cascade PID · UAV · ABC Algorithm

Abstract

In this study, the nonlinear model of the longitudinal motion and altitude of a fixed-wing unmanned aerial vehicle with assured geometrical features and aerodynamic parameters is linearized under certain conditions. A cascade Proportional Integral Differential Controller is designed on the linear model. The controller coefficients that applied to the model of the UAV were optimized with an artificial intelligence technique, which is based on a metaheuristic search algorithm. The four different controller gains in the system are optimized using four different objective functions. Controller performances were tested in simulation environment for unit step input responses., Considering the longitudinal dynamics of the aircraft, among the ITAE, ISE, MSE, and IAE fitness functions, IAE can be shown as the optimum result for altitude control.

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Cite This Article

DURMAZ, M., CİCİ, K., SARIKAYA, M., BİLİCİ, M., BİLGİÇ, H. H. (2023). Metaheuristic algorithm-based cascade PID controller design for fixed wing unmanned aerial vehicle. European Mechanical Science, Cilt: 7 Sayı: 4, 230–237. https://ajindex.com/articles/1022515

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