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| 1 | REKF and RUKF for pico satellite attitude estimation in the presence of measurement faults显示文摘When a pico satellite is under normal operational conditions, whether it is extended or unscented, a conventional Kalman filter gives sufficiently good estimation results. However, if the measurements are not reliable because of any kind of malfunctions in the estimation system, the Kalman filter gives inaccurate results and diverges by time. This study compares two different robust Kalman filtering algorithms, robust extended Kalman filter(REKF) and robust unscented Kalman filter(RUKF), for the case of measurement malfunctions. In both filters, by the use of defined variables named as the measurement noise scale factor, the faulty measurements are taken into the consideration with a small weight, and the estimations are corrected without affecting the characteristic of the accurate ones. The proposed robust Kalman filters are applied for the attitude estimation process of a pico satellite, and the results are compared. | Halil Ersin Sken Chingiz Hajiyev | 2014 | Journal of Systems Engineering and Electronics2014，25，2： | 9 |
| 2 | Pico satellite attitude estimation via robust unscented Kalman filter in the presence of measurement faults 显示文摘 | SOKEN H E HAJIYEV C | 2010 | ISA Transactions2010，49，3： | 1 |
| 3 | Kalman filter and neural network-based icing identification applied to A340 aircraft dynamics显示文摘 | Aykan R Hajiyev C Galiskan F | 2005 | Aircraft Engineering and Aerospace Tech- nology2005，77，1： | 1 |
| 4 | Robust Kalman filtering for small satellite attitude estimation in the presence of measurement faults显示文摘 | Soken H E Hajiyev C Sakai S I | 2014 | European Journal of Control2014，20，2： | 1 |
| 5 | Tracy-widom distribution based fault detection approach:Application to aircraft sensor/actuator fault detection显示文摘 | Hajiyev C | 2012 | ISA Transactions2012，51，1： | 1 |
| 6 | Robust Estimation of UAV D ynam ics in the Presence of M easurem ent Faults显示文摘 | Hajiyev C Soken HE | 2012 | Journal of A erospace Engineering2012，25，1： | 1 |
| 7 | Fault tolerant integrated radar/inertial altime- ter based on nonlinear robust adaptive Kalman filter显示文摘 | Hajiyev C | 2012 | Aerospace Science and Technology2012，17，1： | 1 |
| 8 | Fauh detection in sensor information fusion Kalman filter显示文摘 | Okatan A Hajiyev C Hajiyeva U | 2009 | International Journal of Electronics and Com munieations2009，63，9： | 1 |
| 9 | Kalman filter innovation sequence based fault detection in LEO satellite attitude determination and control system 显示文摘 | OKATAN A HAJIYEV C H | 2008 | IEEE transac- tions2008，20，： | 1 |
| 10 | The effect of aerobic exercise on glycosylated hemoglobin values in type 2 diabetes patients显示文摘 | YAVARI A HAJIYEV AM NAGHIZADEH F | 2010 | J Sports Med Phys Fitness2010，50，4： | 1 |
| 11 | Kalman filter innovation sequence based fault detection in LEO satellite attitude determination and control system 显示文摘 | OKATAN A HAJIYEV C H | 2007 | IEEE transac- tions2007，1，： | 1 |
| 12 | Sensor and Control Surface/Actuator Failure Detection and Isolation Applied to F-16 Flight Dynamic 显示文摘 | Hajiyev C Caliskan F | 2005 | Aircraft Engineering and Aerospace Technology2005，77，2： | 1 |
| 13 | Adaptive fading UKF with Q-Adapta- tion: application to picosatellite attitude estimation显示文摘 | Soken H E Hajiyev C | 2011 | Journal of Aerospace Engineering2011，26，3： | 1 |
| 14 | Innovation Approach Based Measurement Error Self-Correction in Dynamic Systems 显示文摘 | Hajiyev C | 2006 | Measurement2006，39，： | 1 |
| 15 | Innovation sequence application to aircraft sensor fault detection:comparison of checking covariance matrix algorithms显示文摘 | Caliskan F Hajiyev C M | | 0，，01： | 1 |
| 16 | Sensor and control surface/actuator failure detection and isolation applied to F-16 flight dynamic显示文摘 | Hajiyev C Caliskan F | | 0，，02： | 1 |
| 17 | Does structured withdrawal of desmo- pressin improve relapse rates in patients with monosymptomatic enure- sis?显示文摘 | Kge Mi Hajiyev P Siier E | 2014 | J Urol2014，192，2： | 1 |
| 18 | Pico satellite attitude estimation via ro- bust unscented Kalman filter in the presence of measurement faults 显示文摘 | Soken H E Hajiyev C | 2010 | ISA Transactions2010，49，3： | 1 |
| 19 | Adaptive filtration algorithm with the filter gain correction applied to integrated INS/Radar altimeter显示文摘 | Hajiyev C | 2007 | Proceedings of the Institution of Mechanical Engineers Part G : Journal of Aerospace Engineering2007，221，5： | 1 |
| 20 | Robust Adaptive Kalman Filter for estimation of UAV dynamics in the pres- ence of sensor/actuator faults 显示文摘 | CHINGIZ Hajiyev HALIL Ersin Soken | 2013 | Aerospace Science and Technology2013，1，28： | 1 |
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