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

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Copy For Citation

Hajiyev C., CALISKAN F.

AIRCRAFT ENGINEERING AND AEROSPACE TECHNOLOGY, vol.77, no.2, pp.152-160, 2005 (SCI-Expanded)

• Publication Type: Article / Article
• Volume: 77 Issue: 2
• Publication Date: 2005
• Doi Number: 10.1108/00022660510585992
• Journal Name: AIRCRAFT ENGINEERING AND AEROSPACE TECHNOLOGY
• Journal Indexes: Science Citation Index Expanded (SCI-EXPANDED), Scopus
• Page Numbers: pp.152-160
• Istanbul Technical University Affiliated: Yes

Abstract

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.