| Fault diagnosis and reconfiguration in flight control systems C Hajiyev, F Caliskan Springer Science & Business Media, 2003 | 243 | 2003 |
| A review of in-flight detection and identification of aircraft icing and reconfigurable control F Caliskan, C Hajiyev Progress in Aerospace Sciences 60, 12-34, 2013 | 108 | 2013 |
| Sensor and control surface/actuator failure detection and isolation applied to F‐16 flight dynamic C Hajiyev, F Caliskan Aircraft Engineering and aerospace technology 77 (2), 152-160, 2005 | 107 | 2005 |
| Sensor/actuator fault diagnosis based on statistical analysis of innovation sequence and robust Kalman filtering C Hajiyev, F Caliskan Aerospace science and technology 4 (6), 415-422, 2000 | 71 | 2000 |
| Integrated sensor/actuator FDI and reconfigurable control for fault-tolerant flight control system design CM Hajiyevt, F Caliskan The Aeronautical Journal 105 (1051), 525-533, 2001 | 46 | 2001 |
| A robust fault detection and isolation method in load frequency control loops F Caliskan, I Genc IEEE Transactions on Power Systems 23 (4), 1756-1767, 2008 | 45 | 2008 |
| Active fault-tolerant control of UAV dynamics against sensor-actuator failures F Caliskan, C Hajiyev Journal of Aerospace Engineering 29 (4), 04016012, 2016 | 43 | 2016 |
| Aircraft icing detection, identification, and reconfigurable control based on Kalman filtering and neural networks F Caliskan, R Aykan, C Hajiyev Journal of Aerospace Engineering 21 (2), 51-60, 2008 | 41 | 2008 |
| Kalman filter and neural network‐based icing identification applied to A340 aircraft dynamics R Aykan, C Hajiyev, F Çalişkan Aircraft Engineering and Aerospace Technology 77 (1), 23-33, 2005 | 39 | 2005 |
| Innovation sequence application to aircraft sensor fault detection: comparison of checking covariance matrix algorithms F Caliskan, CM Hajiyev ISA transactions 39 (1), 47-56, 2000 | 39 | 2000 |
| Aircraft icing detection, identification and reconfigurable control based on Kalman filtering and neural networks R Aykan, C Hadjiyev, F Caliskan AIAA Atmospheric Flight Mechanics Conference and Exhibit, 6220, 2005 | 31 | 2005 |
| Aircraft sensor and actuator fault detection, isolation, and accommodation E Kiyak, A Kahvecioglu, F Caliskan Journal of Aerospace Engineering 24 (1), 46-58, 2011 | 30 | 2011 |
| Simulation-based dynamic model and speed controller design of a small-scale turbojet engine I Yazar, E Kiyak, F Caliskan, TH Karakoc Aircraft Engineering and Aerospace Technology 90 (2), 351-358, 2018 | 28 | 2018 |
| Actuator and sensor fault detection and diagnosis of quadrotor based on two-stage kalman filter M Moghadam, F Caliskan 2015 5th Australian Control Conference (AUCC), 182-187, 2015 | 25 | 2015 |
| Sensor and actuator FDI applied to an UAV dynamic model F Caliskan, C Hacizade IFAC Proceedings Volumes 47 (3), 12220-12225, 2014 | 20 | 2014 |
| Aircraft sensor fault diagnosis based on Kalman filter innovation sequence F Caliskan, CM Hajiyev Proceedings of the 37th IEEE Conference on Decision and Control (Cat. No …, 1998 | 20 | 1998 |
| Actuator fault diagnosis in a Boeing 747 model via adaptive modified two-stage Kalman filter F Caliskan, Y Zhang, NE Wu, JY Shin International Journal of Aerospace Engineering 2014, 2014 | 19 | 2014 |
| Actuator failure detection and reconfigurable control for F-16 aircraft model F Caliskan, C Hajiyev IFAC Proceedings Volumes 36 (7), 53-58, 2003 | 19 | 2003 |
| EKF based surface fault detection and reconfiguration in aircraft control systems F Caliskan, CM Hajiyev Proceedings of the 2000 American Control Conference. ACC (IEEE Cat. No …, 2000 | 18 | 2000 |
| Fault detection in flight control systems via innovation sequence of Kalman filter CM Hajiyev, F Caliskan Progress in system and robot analysis and control design, 63-74, 2007 | 17 | 2007 |
