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Dergiler / Journal of Aviation / 2026 / Volume: 8 Issue: 2

Redundancy in Automatic Flight Control System Design for A General Purpose Helicopter

Mutullah Eşer(ANKARA ÜNİVERSİTESİ, MÜHENDİSLİK FAKÜLTESİ)0009-0009-4847-7522
Berk Akın Yıldız(HACETTEPE ÜNİVERSİTESİ)0009-0000-5919-0417
Umut Türe(Türk Havacılık ve Uzay Sanayii)0009-0003-5380-1194
Sayfa
—
Yayın Tarihi
2024-06-27
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⚡ TL;DR(1 Cümlede Hızlı Çıkarım)

The results of these tests verify the proposed design, ensuring the safety of the flight under different failure scenarios.

📌 3 Maddede Bu Makale

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Amaç & Hipotez:Redundancy is a popular concept among autopilot design engineers due to the importance of safety in aviation.
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Temel Bulgular & Veri:The main goal of redundancy in autopilot design is to eliminate or minimize the loss of a system in case of single point failures.
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Sonuç & Katkı:The results of these tests verify the proposed design, ensuring the safety of the flight under different failure scenarios.
🔬Tür:Research Article
📍Kapsam:Genişletilmiş Akademik Örneklem
⚙️Değişkenler:Automatic flight control system · Redundancy management · Sensor fault detection

Abstract

Redundancy is a popular concept among autopilot design engineers due to the importance of safety in aviation. The main goal of redundancy in autopilot design is to eliminate or minimize the loss of a system in case of single point failures. In this study, the designed autopilot flight control system with redundancy for a general purpose helicopter is presented, along with the simulator and flight test results of the design. The designed system combines the elements of direct and functional redundancy to achieve a full redundant system. The simulator tests were done in the flight control simulator in Turkish Aerospace Industries (TAI) in Ankara, and the flight tests were done with the general purpose helicopter over Ankara Mürted airspace. The results of these tests verify the proposed design, ensuring the safety of the flight under different failure scenarios.

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Bu Makaleye Atıf Yap

Eşer, M., Yıldız, B. A., Türe, U. (2024). Redundancy in Automatic Flight Control System Design for A General Purpose Helicopter. Journal of Aviation, Volume: 8 Issue: 2. https://doi.org/10.30518/jav.1468684

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