| Fault diagnosis and reconfiguration in flight control systems C Hajiyev, F Caliskan Springer Science & Business Media, 2003 | 243 | 2003 |
| Pico satellite attitude estimation via robust unscented Kalman filter in the presence of measurement faults HE Soken, C Hajiyev ISA transactions 49 (3), 249-256, 2010 | 159 | 2010 |
| Robust adaptive Kalman filter for estimation of UAV dynamics in the presence of sensor/actuator faults C Hajiyev, HE Soken Aerospace Science and Technology 28 (1), 376-383, 2013 | 151 | 2013 |
| Robust adaptive unscented Kalman filter for attitude estimation of pico satellites C Hajiyev, HE Soken International Journal of Adaptive Control and Signal Processing 28 (2), 107-120, 2014 | 118 | 2014 |
| 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 |
| Robust Kalman filtering for small satellite attitude estimation in the presence of measurement faults HE Soken, C Hajiyev, S Sakai European Journal of Control 20 (2), 64-72, 2014 | 98 | 2014 |
| LQR controller with Kalman estimator applied to UAV longitudinal dynamics C Hajiyev, SY Vural Scientific Research Publishing, 2013 | 77 | 2013 |
| Review on gyroless attitude determination methods for small satellites C Hajiyev, DC Guler Progress in Aerospace Sciences 90, 54-66, 2017 | 71 | 2017 |
| 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 |
| Gyro-free attitude and rate estimation for a small satellite using SVD and EKF C Hajiyev, D Cilden, Y Somov Aerospace Science and Technology 55, 324-331, 2016 | 65 | 2016 |
| Integration of navigation systems for autonomous underwater vehicles M Dinc, C Hajiyev Journal of Marine Engineering & Technology 14 (1), 32-43, 2015 | 61 | 2015 |
| UKF-based reconfigurable attitude parameters estimation and magnetometer calibration HE Soken, C Hajiyev IEEE Transactions on Aerospace and Electronic Systems 48 (3), 2614-2627, 2012 | 58 | 2012 |
| Fault detection in sensor information fusion Kalman filter A Okatan, C Hajiyev, U Hajiyeva AEU-International Journal of Electronics and Communications 63 (9), 762-768, 2009 | 54 | 2009 |
| Robust estimation of UAV dynamics in the presence of measurement faults C Hajiyev, HE Soken Journal of Aerospace Engineering 25 (1), 80-89, 2012 | 51 | 2012 |
| State estimation and control for low-cost unmanned aerial vehicles C Hajiyev, HE Soken, SY Vural Springer International Publishing, 2015 | 50 | 2015 |
| Adaptive unscented Kalman filter with multiple fading factors for pico satellite attitude estimation HE Soken, C Hajiyev 2009 4th International Conference on Recent Advances in Space Technologies …, 2009 | 49 | 2009 |
| Adaptive fading UKF with Q-adaptation: application to picosatellite attitude estimation HE Soken, C Hajiyev Journal of Aerospace Engineering 26 (3), 628-636, 2013 | 47 | 2013 |
| Nanosatellite attitude estimation using Kalman-type filters with non-Gaussian noise D Cilden-Guler, M Raitoharju, R Piche, C Hajiyev Aerospace Science and Technology 92, 66-76, 2019 | 44 | 2019 |
| 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 |
