Multiple fault-based FDI and reconfiguration for aircraft engine sensors

---

Atıf İçin Kopyala

YAZAR I., Çalışkan F., Kiyak E.

AIRCRAFT ENGINEERING AND AEROSPACE TECHNOLOGY, cilt.89, sa.3, ss.397-405, 2017 (SCI-Expanded)

• Yayın Türü: Makale / Tam Makale
• Cilt numarası: 89 Sayı: 3
• Basım Tarihi: 2017
• Doi Numarası: 10.1108/aeat-04-2015-0100
• Dergi Adı: AIRCRAFT ENGINEERING AND AEROSPACE TECHNOLOGY
• Derginin Tarandığı İndeksler: Science Citation Index Expanded (SCI-EXPANDED), Scopus
• Sayfa Sayıları: ss.397-405
• İstanbul Teknik Üniversitesi Adresli: Evet

Özet

Purpose - Condition monitoring and health management of an aircraft engine is of importance due to engine's critical position in aircraft. Missions require uninterrupted and safer conditions during the flight or taxi operations. Hence, the deviations, abnormal situations or failures have to be under control. This paper aims to propose a cascade connected approach for an aircraft engine fault tolerant control.