Chingiz Hajiyev
Cited by
Cited by
Fault diagnosis and reconfiguration in flight control systems
C Hajiyev, F Caliskan
Springer Science & Business Media, 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
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
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
Sensor and control surface/actuator failure detection and isolation applied to F‐16 flight dynamic
C Hajiyev, F Caliskan
Aircraft Engineering and aerospace technology, 2005
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
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
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
LQR controller with Kalman estimator applied to UAV longitudinal dynamics
C Hajiyev, SY Vural
Scientific Research Publishing, 2013
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
Review on gyroless attitude determination methods for small satellites
C Hajiyev, DC Guler
Progress in Aerospace Sciences 90, 54-66, 2017
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
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
Integration of navigation systems for autonomous underwater vehicles
M Dinc, C Hajiyev
Journal of Marine Engineering & Technology 14 (1), 32-43, 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
Adaptive fading UKF with Q-adaptation: application to picosatellite attitude estimation
HE Soken, C Hajiyev
Journal of Aerospace Engineering 26 (3), 628-636, 2013
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
Robust estimation of UAV dynamics in the presence of measurement faults
C Hajiyev, HE Soken
Journal of Aerospace Engineering 25 (1), 80-89, 2012
State estimation and control for low-cost unmanned aerial vehicles
C Hajiyev, HE Soken, SY Vural
Springer, 2015
Fuzzy logic‐based automated engine health monitoring for commercial aircraft
S Demirci, C Hajiyev, A Schwenke
Aircraft engineering and aerospace technology, 2008
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