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Journals / Gazi Üniversitesi Mühendislik Mimarlık Fakültesi Dergisi / 2017 / Cilt: 32 - Sayı: 1

Fault tolerant flight control system design to a rotary wing aircraft

Bir döner kanata arıza toleranslı uçuş kontrol sistemi tasarımı

Ahmet ERMEYDAN
Emre KIYAK
Pages
21–34
Publication Date
2022-10-18
DOI
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AI Summary & Key Takeaways

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

When the simulation results are analyzed, the performance of the designed control system shows a robust behavior under various conditions.

📌 3 Key Takeaways

🎯
Objective & Hypothesis:In this study, fault tolerant control is made using improved PID controller approach with different motor fault scenarios in a quadrotor.
📊
Key Findings & Data:A realistic simulation was set up by obtaining dynamics equations of aircraft and modeling motor dynamics.
💡
Conclusion & Impact:When the simulation results are analyzed, the performance of the designed control system shows a robust behavior under various conditions.
🔬Design:Modeling & Simulation
📍Scope:Comprehensive Sample
⚙️Variables:Domain Parameters

Abstract

In this study, fault tolerant control is made using improved PID controller approach with different motor fault scenarios in a quadrotor. A realistic simulation was set up by obtaining dynamics equations of aircraft and modeling motor dynamics. By linearizing nonlinear model suitable controller is formed and this controller scheme is used in nonlinear models. Finally, designed control structure over different motor fault scenarios is tested whether a robust control structure is built. When the simulation results are analyzed, the performance of the designed control system shows a robust behavior under various conditions.

Özet

Bu çalışmada bir döner kanatın farklı motor arıza senaryolarının geliştirilmiş PID denetleyici yaklaşımıyla arıza toleranslı kontrolü yapılmıştır. Denklemleri verilen hava aracının motor dinamikleri de modellenerek gerçekçi bir benzetim elde edilmiştir. Doğrusal olmayan model doğrusallaştırılarak uygun denetleyici yapıları oluşturulmuş, sonrasında bu yapı doğrusal olmayan modelde kullanılmıştır. Son olarak farklı motor arıza senaryoları üzerinden tasarlanan kontrol yapısının gürbüz bir yapı oluşturup oluşturmadığı sınanmıştır. Benzetim sonuçları incelendiğinde, tasarlanan kontrol sisteminin değişik şartlar altında gürbüz bir davranış sergilediği görülmüştür.

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Cite This Article

ERMEYDAN, A., KIYAK, E. (2022). Fault tolerant flight control system design to a rotary wing aircraft. Gazi Üniversitesi Mühendislik Mimarlık Fakültesi Dergisi, Cilt: 32 - Sayı: 1, 21–34. https://ajindex.com/articles/523591

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