Author:
Caliskan Fikret,Hacizade Cengiz
Reference15 articles.
1. Experimental Test of a Two-Stage Kalman Filter for Actuator Fault Detection and Diagnosis of an Unmanned Quadrotor Helicopter;Amoozgar;J. Intelligent Robot Systems,2013
2. Boskovic, J.D. and R.K. Mehra (2001). A robust adaptive reconfigurable flight control scheme for accommodation of control effector failures. Proceedings of the American Control Conference, Arlington, VA, 1127-1132.
3. Caliskan F., Y. Zhang, N.E. Wu and J. Y. Shin (2009) Estimation of actuator fault parameters in a nonlinear Boeing 747 model using a linear Two-Stage Kalman Filter. Preprints of the 7th IFAC Symposium on Fault Detection, Supervision and Safety of Technical Processes, Barcelona, Spain, 1408-1413.
4. Fault Diagnosis and Reconfiguration in Flight Control Systems;Hajiyev,2003
5. Sensor and control surface/actuator failure detection and isolation applied to F-16 flight dynamic;Hajiyev;Aircraft Engineering and Aerospace Technology,2005
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