Sensor/Control Surface Fault Diagnosis and Reconfiguration in Aircraft Control Systems


Hacızade C., Çalışkan F.

Engineering, Construction and Operations in Challenging Environments - Earth and Space 2004: Proceedings of the Ninth Biennial ASCE Aerospace Division International Conference, League City/Houston, TX, United States Of America, 7 - 10 March 2004, pp.176-183 identifier identifier

  • Publication Type: Conference Paper / Full Text
  • Doi Number: 10.1061/40722(153)25
  • City: League City/Houston, TX
  • Country: United States Of America
  • Page Numbers: pp.176-183
  • Istanbul Technical University Affiliated: Yes

Abstract

In this paper, an approach to detect and isolate the aircraft sensor/control surface faults affecting the mean of the Kalman filter innovation sequence is proposed, and a new structure for a fault tolerant aircraft control system is presented In the simulations, the longitudinal and lateral dynamics of an F-16 aircraft model is considered, and detection and isolation of pitch rate gyro faults and control surface faults are examined The principal block diagram of a fault tolerant aircraft control system is illustrated.