EKF based surface fault detection and reconfiguration in aircraft control systems

Caliskan F., Hajiyev C.

2000 American Control Conference (ACC 2000), Illinois, Amerika Birleşik Devletleri, 28 - 30 Haziran 2000, ss.1220-1224 identifier identifier

  • Yayın Türü: Bildiri / Tam Metin Bildiri
  • Cilt numarası:
  • Doi Numarası: 10.1109/acc.2000.876694
  • Basıldığı Şehir: Illinois
  • Basıldığı Ülke: Amerika Birleşik Devletleri
  • Sayfa Sayıları: ss.1220-1224
  • İstanbul Teknik Üniversitesi Adresli: Evet

Özet

In this paper, a surface fault detection algorithm based on the Extended Kalman Filter (EKF) is presented. The innovation- the difference between the actual plant states and the plant states identified by the EKF are evaluated for the fault detection and identification, and the control reconfiguration procedure is executed by considering the identified control distribution matrix.