Multiple fault-based FDI and reconfiguration for aircraft engine sensors

YAZAR I., Çalışkan F., KIYAK E.

AIRCRAFT ENGINEERING AND AEROSPACE TECHNOLOGY, vol.89, no.3, pp.397-405, 2017 (SCI-Expanded) identifier identifier

  • Publication Type: Article / Article
  • Volume: 89 Issue: 3
  • Publication Date: 2017
  • Doi Number: 10.1108/aeat-04-2015-0100
  • Journal Name: AIRCRAFT ENGINEERING AND AEROSPACE TECHNOLOGY
  • Journal Indexes: Science Citation Index Expanded (SCI-EXPANDED), Scopus
  • Page Numbers: pp.397-405
  • Keywords: Fault tolerant control, Aircraft engine control, Fault detection/diagnosis
  • Anadolu University Affiliated: Yes

Abstract

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.