Integrated sensor/actuator FDI and reconfigurable control for fault-tolerant flight control system design

Hacızade C., Çalışkan F.

AERONAUTICAL JOURNAL, vol.105, no.1051, pp.525-533, 2001 (SCI-Expanded) identifier identifier

  • Publication Type: Article / Article
  • Volume: 105 Issue: 1051
  • Publication Date: 2001
  • Doi Number: 10.1017/s0001924000017966
  • Journal Name: AERONAUTICAL JOURNAL
  • Journal Indexes: Science Citation Index Expanded (SCI-EXPANDED), Scopus
  • Page Numbers: pp.525-533
  • Istanbul Technical University Affiliated: No

Abstract

In this paper an approach to fault-tolerant flight control system design based on the integration of sensor/actuator fault detection and isolation (FDI) and reconfigurable control is presented. The effects of the sensor and actuator faults in the innovation process of the Kalman filter are investigated, and a decision approach to isolate the sensor and actuator faults is proposed.