Sensor and control surface/actuator failure detection and isolation applied to F-16 flight dynamic

Hajiyev, Cengiz; CALISKAN, Fikret

doi:10.1108/00022660510585992

Sensor and control surface/actuator failure detection and isolation applied to F-16 flight dynamic

Atıf İçin Kopyala

Hajiyev C., CALISKAN F.

AIRCRAFT ENGINEERING AND AEROSPACE TECHNOLOGY, cilt.77, sa.2, ss.152-160, 2005 (SCI-Expanded)

Yayın Türü: Makale / Tam Makale
Cilt numarası: 77 Sayı: 2
Basım Tarihi: 2005
Doi Numarası: 10.1108/00022660510585992
Dergi Adı: AIRCRAFT ENGINEERING AND AEROSPACE TECHNOLOGY
Derginin Tarandığı İndeksler: Science Citation Index Expanded (SCI-EXPANDED), Scopus
Sayfa Sayıları: ss.152-160
İstanbul Teknik Üniversitesi Adresli: Evet

Özet

Purpose - The purpose of the paper is to present an approach to detect and isolate the aircraft sensor and control surface/actuator failures affecting the mean of the Kalman filter innovation sequence.