Journals / Makine Teknolojileri Elektronik Dergisi (elektronik) / 2010 / Cilt: 7 - Sayı: 1

Effects of aircraft roll control system design with classical and fuzzy controllers

Bir uçağın yatış kontrol sistem tasarımında klasik ve bulanık denetleyici etkileri

Pages
31–42
DOI
—
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AI Summary & Key Takeaways

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

In classical controllers, the outputs having the preferred performance can be obtained by adjusting the gain; whereas, for the fuzzy controllers better values can be obtained by increasing the number of input and output functions and the number of the rules.

📌 3 Key Takeaways

🎯
Objective & Hypothesis:The aim of the controller of the closed loop control systems is to produce an output following the input.
📊
Key Findings & Data:PD, PI, and PID controllers are widely used for this aim with some variations according to the system structure.
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Conclusion & Impact:In classical controllers, the outputs having the preferred performance can be obtained by adjusting the gain; whereas, for the fuzzy controllers better values can be obtained by increasing the number of input and output functions and the number of the rules.
🔬Design:Research Article
📍Scope:Comprehensive Sample
⚙️Variables:Domain Parameters

Abstract

The aim of the controller of the closed loop control systems is to produce an output following the input. PD, PI, and PID controllers are widely used for this aim with some variations according to the system structure. The fuzzy controllers can be used for this aim, for which the membership functions and the choice of the rules are essential. In this study, the comparison of the PD, PI, PID, and fuzzy controllers are realized for the roll control system of an airplane. In classical controllers, the outputs having the preferred performance can be obtained by adjusting the gain; whereas, for the fuzzy controllers better values can be obtained by increasing the number of input and output functions and the number of the rules.

Özet

Kapalı çevrim kontrol sistemlerinde denetleyicinin amacı, girişe takip eden bir çıktı üretmektir. Sistem yapısına bağlı olarak bir takım ayarlamalar ile PD, PI ve PID denetleyiciler, bu amaçla sıklıkla kullanılırlar. Bulanık denetleyiciler de bu amaçla kullanılabilir olup, üyelik fonksiyonları ve kuralların seçimi önem kazanmaktadır. Bu çalı mada, bir uçağın yatış kontrol sistemi için PD, PI, PID ve bulanık denetleyici kar ıla tırmaları yapılmaktadır. Klasik denetleyiciler için kazanç ayarlamalarıyla istenen performansta çıktılar elde edilebilir. Bulanık denetleyiciler için ise, kullanılacak giri ve çıkı fonksiyonlarının sayısının ve kural sayısının arttırılmasıyla yoluyla daha iyi değerler elde edilebilir.

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Cite This Article

KIYAK, E. (2010). Effects of aircraft roll control system design with classical and fuzzy controllers. Makine Teknolojileri Elektronik Dergisi (elektronik), Cilt: 7 - Sayı: 1, 31–42. https://ajindex.com/articles/282096

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References (2)

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