| 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 | 160 | 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 | 157 | 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 | 120 | 2014 |
| 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 | 97 | 2014 |
| 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 | 60 | 2012 |
| State estimation and control for low-cost unmanned aerial vehicles C Hajiyev, HE Soken, SY Vural Springer International Publishing, 2015 | 53 | 2015 |
| Adaptive fading UKF with Q-adaptation: application to picosatellite attitude estimation HE Soken, C Hajiyev Journal of Aerospace Engineering 26 (3), 628-636, 2013 | 50 | 2013 |
| Robust estimation of UAV dynamics in the presence of measurement faults C Hajiyev, HE Soken Journal of Aerospace Engineering 25 (1), 80-89, 2012 | 49 | 2012 |
| 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 |
| Attitude estimation and magnetometer calibration using reconfigurable TRIAD+ filtering approach HE Soken, S Sakai Aerospace Science and Technology 99, 105754, 2020 | 42 | 2020 |
| A survey of calibration algorithms for small satellite magnetometers HE Soken Measurement 122, 417-423, 2018 | 32 | 2018 |
| Fault tolerant attitude estimation for small satellites C Hajiyev, HE Soken CRC Press, 2020 | 29 | 2020 |
| Nanosatellite attitude estimation from vector measurements using SVD-aided UKF algorithm D Cilden, HE Soken, C Hajiyev Metrology and Measurement Systems, 2017 | 28 | 2017 |
| Real-time attitude-independent magnetometer bias estimation for spinning spacecraft HE Söken, S Sakai Journal of Guidance, Control, and Dynamics 41 (1), 276-279, 2018 | 27 | 2018 |
| In-orbit estimation of time-varying residual magnetic moment HE Soken, S Sakai, R Wisniewski IEEE Transactions on Aerospace and Electronic Systems 50 (4), 3126-3136, 2014 | 27 | 2014 |
| Robust attitude estimation using IMU-only measurements B Candan, HE Soken IEEE Transactions on Instrumentation and Measurement 70, 1-9, 2021 | 26 | 2021 |
| Adaptive tuning of the unscented Kalman filter for satellite attitude estimation HE Soken, S Sakai Journal of Aerospace Engineering 28 (3), 04014088, 2015 | 24 | 2015 |
| Attitude and attitude rate estimation for a nanosatellite using SVD and UKF D Cilden, C Hajiyev, HE Soken 2015 7th International Conference on Recent Advances in Space Technologies …, 2015 | 23 | 2015 |
| In flight magnetometer calibration via unscented Kalman filter HE Soken, C Hajiyev Proceedings of 5th International Conference on Recent Advances in Space …, 2011 | 23 | 2011 |
| UKF based in‐flight calibration of magnetometers and rate gyros for pico satellite attitude determination HE Söken, C Hajiyev Asian Journal of Control 14 (3), 707-715, 2012 | 22 | 2012 |
Chingiz HajiyevIstanbul Technical University在 itu.edu.tr 的电子邮件经过验证
