SCI, SSCI ve AHCI İndekslerine Giren Dergilerde Yayınlanan Makaleler
Attitude filtering with uncertain process and measurement noise covariance using SVD-aided adaptive UKF
International Journal of Robust and Nonlinear Control
, cilt.33, sa.17, ss.10512-10531, 2023 (SCI-Expanded)
Integration of barometric and GPS altimeters via adaptive data fusion algorithm
INTERNATIONAL JOURNAL OF ADAPTIVE CONTROL AND SIGNAL PROCESSING
, cilt.35, sa.1, ss.2-14, 2021 (SCI-Expanded)
Robust adaptive unscented Kalman filter for attitude estimation of pico satellites
INTERNATIONAL JOURNAL OF ADAPTIVE CONTROL AND SIGNAL PROCESSING
, cilt.28, sa.2, ss.107-120, 2014 (SCI-Expanded)
Two-stage Kalman filter-based actuator/surface fault identification and reconfigurable control applied to F-16 fighter dynamics
INTERNATIONAL JOURNAL OF ADAPTIVE CONTROL AND SIGNAL PROCESSING
, cilt.27, sa.9, ss.755-770, 2013 (SCI-Expanded)
Identification of Orbital Measurements
Measurement Techniques
, cilt.55, sa.11, ss.1234-1239, 2013 (SCI-Expanded)
UKF-Based Reconfigurable Attitude Parameters Estimation and Magnetometer Calibration
IEEE TRANSACTIONS ON AEROSPACE AND ELECTRONIC SYSTEMS
, cilt.48, sa.3, ss.2614-2627, 2012 (SCI-Expanded)
Testing the covariance matrix of the innovation sequence with sensor/actuator fault detection applications
INTERNATIONAL JOURNAL OF ADAPTIVE CONTROL AND SIGNAL PROCESSING
, cilt.24, sa.9, ss.717-730, 2010 (SCI-Expanded)
Fault detection in sensor information fusion Kalman filter
AEU-INTERNATIONAL JOURNAL OF ELECTRONICS AND COMMUNICATIONS
, cilt.63, sa.9, ss.762-768, 2009 (SCI-Expanded)
Determining the Operating Conditions of Floating Marine Plotforms Based on the Predicted Motion Control Under Conditions of Wind and Wave Disturbances
Measurement Techniques
, cilt.51, sa.1, ss.28-33, 2008 (SCI-Expanded)
A Sequential Method of Calibrating Measurement Instruments with a Kalman filter
MEASUREMENT TECHNIQUES
, cilt.49, sa.4, ss.357-366, 2006 (SCI-Expanded)
Attitude Determination and Control System Design of the ITU UUBF LEO1 Satellite
ACTA ASTRONAUTICA
, cilt.52, ss.493-499, 2003 (SCI-Expanded)
An Approach to Improve the Offshore Platform Coordinates Accuracy by Using Multichannel Kalman Filtering
ISA Transactions, Journal of Automation and Measurement
, cilt.42, sa.1, ss.53-61, 2003 (SCI-Expanded)
Optimization of the allowed drilling area in the operation of offshore platforms
MEASUREMENT TECHNIQUES
, cilt.44, sa.6, ss.590-593, 2001 (SCI-Expanded)
Integrated sensor actuator FDI and reconfigurable control for fault tolerant flight control system design
The Aeronautical Journal
, cilt.105, sa.1051, ss.525-533, 2001 (SCI-Expanded)
A recurrent algorithm for estimating a linear regression model with account of the regression vector error
Industrial Laboratory
, cilt.66, sa.7, ss.486-489, 2000 (SCI-Expanded)
A optimal plan for locating extension wells when prospecting for oil deposits
MEASUREMENT TECHNIQUES
, cilt.43, sa.3, ss.222-228, 2000 (SCI-Expanded)
Sensor Fault Detection in Flight Control Systems Based on the Kalman Filter Innovation Sequence
IMechE Proceedings , Part I, J.Systems & Control Engineering
, cilt.213, ss.243-248, 1999 (SCI-Expanded)
Distributions of scalar measures of a Wishart random matrix
Industrial Laboratory
, cilt.0, sa.5, ss.340-341, 1999 (SCI-Expanded)
Experimental Design in Problems Involving Measurement of the Mass of Petroleum Products in Storage Tanks
MEASUREMENT TECHNIQUES
, cilt.39, sa.6, ss.629-632, 1996 (SCI-Expanded)
Multidimensional Dynamical System Mathematical Model Adequacy Operative Verifying
AUTOMATION AND REMOTE CONTROL
, cilt.56, sa.7, ss.949-955, 1995 (SCI-Expanded)
Sequential Method for Verifying Adequacy of Mathematical Models for Multidimensional Dynamical Systems with Biased Measurements
MEASUREMENT TECHNIQUES
, cilt.38, sa.10, ss.1082-1088, 1995 (SCI-Expanded)
Problems in Analyzing Hydrostatic Measurements of the Mass of Petroleum Products by Data Measurement Systems
MEASUREMENT TECHNIQUES
, cilt.37, sa.12, ss.1063-1067, 1994 (SCI-Expanded)
Diğer Dergilerde Yayınlanan Makaleler
Active fault tolerant flight control for UAV actuator failures
Mathematıcs In Engıneerıng, Scıence And Aerospace
, cilt.10, sa.4, ss.657-670, 2019 (Scopus)
Two-Stage Kalman Filter for Estimation of Wind Speed and UAV States by using GPS, IMU and Air Data System
WSEAS Transactions On Electronics
, cilt.10, ss.60-65, 2019 (Hakemli Dergi)
SVD-Aided UKF for Estimation of Nanosatellite Rotational Motion Parameters
WSEAS Transactions on Signal Processing
, cilt.14, ss.27-35, 2018 (Hakemli Dergi)
Sensor Actuator Fault Detection Isolation and Accommodation Applied to UAV Model
Journal of Aeronautics and Space Technologies
, cilt.9, sa.2, ss.1-12, 2016 (Hakemli Dergi)
Nontraditional Approach to Satellite Attitude Estimation
International Journal of Control Systems and Robotics
, cilt.1, ss.19-28, 2016 (Hakemli Dergi)
Data Collectıon System Identıfıcatıon of Multıcopter Vehıcle
Machines, Technologies, Materials International Virtual Journal
, sa.2, ss.51-55, 2014 (Hakemli Dergi)
Robust UKF Insensitive to Measurement Faults for Pico Satellite Attitude Estimation
World Academy of Science, Engineering and Technology
, cilt.68, ss.650-655, 2010 (Hakemli Dergi)
Hakemli Kongre / Sempozyum Bildiri Kitaplarında Yer Alan Yayınlar
Two stage kalman filter based fault tolerant control of uav longitudinal dynamicsagainst actuator failures
COIA’20, 26 - 28 Ağustos 2020
Assessment of Fault Tolerant Estimation for Light Utility Helicopter Dynamics
8th Asian/Australian Rotorcraft Forum, 30 Ekim - 02 Kasım 2019
Parçacık Sürü Optimizasyon Güdümü ve Performans Karşılaştırması
TOK’xx2019 Otomatik Kontrol Ulusal Toplantısı, Türkiye, 11 - 14 Eylül 2019, ss.398-403
Performance Comparison of Guidance Algorithms for Planetary Landing, Asteroid Intercept and Rendezvous
9th International Conference on Recent Advances in Space Technologies “Space for the Sustainable Development Goals” (RAST-2019), 11 - 14 Haziran 2019, ss.915-925
Two-Stage Kalman Filter for Estimation of Wind Speed and UAV States by using GPS, IMU and Air Data System
WSEAS Conferences 2019, Lizbon, Portekiz, 12 - 14 Nisan 2019
Passive Fault Tolerant Lateral Controller Design For an UAV
18th IFAC International Conference ”International Stability, Technology and Culture”, 13 Ağustos - 15 Eylül 2018
Robust Kalman Filter Based Estimation of AUV Dynamics in the Presence Of Sensor Faults
18th IFAC International Conference ”International Stability, Technology and Culture”, 13 - 15 Eylül 2018
Gyroless Nanosatellite Attitude Estimation in Loss of Sun Sensor Measurements
18th IFAC International Conference ”International Stability, Technology and Culture”, 13 - 15 Eylül 2018
An Innovation Approach Based Model Change Detection Applied to UAV Actuator/Surface FDI
18th IFAC International Conference ”International Stability, Technology and Culture”, 13 - 15 Eylül 2018
UD Factorization Based Non-Traditional Attitude Estimation of Nanosatellite with Rate Gyros FDI
18th IFAC International Conference ”International Stability, Technology and Culture”, 13 - 15 Eylül 2018
Reconfigurable Fault Tolerant Flight Control for UAV with Pseudo-Inverse Technique
18th IFAC International Conference ”International Stability, Technology and Culture”, 13 - 15 Eylül 2018
Fault tolerant estimation of light utility helicopter dynamics against sensor faults
International Eurasian Conference on Science, Engineering and Technology, 22 - 23 Kasım 2018
Attitude Estimation of Small Satellites in Consideration of Geomagnetic Field Anomalies
42nd COSPAR Scientific Assembly, Pasadena, California, Amerika Birleşik Devletleri, 14 - 22 Temmuz 2018
Attitude Estimation by SVD/EKF using Reformed Measurements and Decomposed Noise Covariance
9th International Conference on Mechanical and Aerospace Engineering, 10 - 13 Temmuz 2018
Test Platform for Small Satellite Attitude Determination and Control System
9th International Conference on Mechanical and Aerospace Engineering, 10 - 13 Temmuz 2018
Kalman Filter Based Sensor Fault Detection And Isolation Algorithms Applied To Helicopter Dynamics
International Conference on Mathematics and Mathematics Education, 27 - 29 Haziran 2018
Reconfigurable Kalman Filter For Estimation Of Helicopter Flight Dynamics
International Conference on Mathematics and Mathematics Education, 27 - 29 Haziran 2018
Attitude and Rate Estimation for Nanosatellite from Vector Measurements Using SVD-Aided UKF Algorithm
4th International Conference on Aeronautical and Mechanical Engineering (AEME ’xx17), 15 - 17 Aralık 2017
Kalman Filter Based Loosely-Coupled GPS/INS Integration for Boeing-747 Aircraft Model
9th Ankara International Aerospace Conference, 20 - 22 Eylül 2017
Integrated SVD/EKF for Nano-satellite AttitudeDetermination in case of Magnetometer Faults
7TH EUROPEAN CONFERENCE FOR AERONAUTICS AND SPACE SCIENCES (EUCASS)Copyright , Milan, İtalya, 3 - 06 Temmuz 2017
Fault Tolerant Integrated Barometric-Inertial-GPS Altimeter
7th European Conference for Aeronautics and Space Sciences (EUCASS), 3 - 06 Temmuz 2017
Fault Tolerant Control of Attitude Dynamics ofNanosatellites
8th International Conference on Recent Advances in Space Technologies - RAST 2017, 19 - 22 Haziran 2017
Attitude Determination of Nanosatellitesin the Sun-Eclipse Phases
8th International Conference on Recent Advances in Space Technologies - RAST 2017, 19 - 22 Haziran 2017
Non-Traditional Robust UKF against Attitude Sensors Faults
31st International Symposium on Space Technology and Science(ISTS), 3 - 09 Haziran 2017
Uydunun Dönme Hareketinin Arıza Toleranslı Kontrolü
Otomatik Kontrol Ulusal Toplantısı (TOK), Türkiye, 29 Eylül - 01 Ekim 2016
An Innovation Approach Based Sensor Fault Detection and Isolation
20th IFAC Symposium on Automatic Control in Aerospace, Sherbrooke, Kanada, 21 - 25 Ağustos 2016
Measurement Differencing Approach Based Kalman Filter Applied to INS Error Compensation
20th IFAC Symposium on Automatic Control in Aerospace, Sherbrooke, Sherbrooke, Kanada, 21 - 25 Ağustos 2016
Estimation of UAV Dynamics Using Two Stage Kalman Filter
International Symposium On Sustainable Aviation, İstanbul, Türkiye, 29 Mayıs - 01 Haziran 2016, ss.418-421
Integrated Barometric Inertial GPS Altimeter
International Symposium on Sustainable Aviation, İstanbul, Türkiye, 29 Mayıs - 01 Haziran 2016, ss.386-389
In flight Management for Attitude Control System with Animation of Satellite Motion
IFAC Conference on Manufacturing Modelling, Management and Control, Troyes, Fransa, 28 - 30 Mayıs 2016, ss.872-877
Attitude Determination and Uncertainty Analysis in Eclipse of Small LEO Satellites
SIAM Conference on Uncertainty Quantification, 5 - 08 Nisan 2016
Nontraditional Approach to Satellite Attitude Estimation
16th International Conference onRobotıcs, Control And Manufacturıng Technology (ROCOM '16), 18 - 20 Mart 2016
Sensor eyleyici arızalarına karşı insansız hava aracının yeniden şekillendirilebilir kontrolü
Otomatik Kontrol Ulusal Toplantısı, TOK'2015, Türkiye, 10 - 12 Eylül 2015, ss.206-211
Error Analysis of the Vector Measurements Based Attitude Determination Methods for Small Satellites
30th International Symposium on Space Technology and Science (ISTS), Kobe-Hyogo, Japonya, 4 - 10 Temmuz 2015
Attitude Estimation for Nanosatellites Using Singular Value Decomposition and Unscented Kalman Filter
30th International Symposium on Space Technology and Science (ISTS), Kobe-Hyogo, Japonya, 4 - 10 Temmuz 2015
Integrated SVD EKF for Small Satellite Attitude and Rate Estimation
6th European Conference for Aeronautics and Space Sciences (EUCASS), 29 Haziran - 02 Temmuz 2015
Fault Detection Isolation and Accommodation in Flight Control System of A340 Airbus Aircraft
International Symposium on Sustainable Aviation, 31 Mayıs - 03 Haziran 2015, ss.44-47
Robust Estimation of F 16 Fighter Dynamics in Presence of Sensor Faults
The First International Symposium on Sustainable Aviation, 31 Mayıs - 03 Haziran 2015, ss.40-43
KÜÇÜK UYDULARDA İKİLİ VE ÜÇLÜ VEKTÖR GÖZLEMLERİ İLE YÖNELİMİN BELİRLENMESİ
V. ULUSAL HAVACILIK VE UZAY KONFERANSI, Kayseri, Türkiye, 8 - 10 Eylül 2014
Yersabit Yörünge Uydusunun Tek Anten Ölçüm Verisi ile Yörüngesinin Belirlenmesinin Hata Analizi
Ulusal Havacılık ve Uzay Konferansı (UHUK-2012), Türkiye, 12 - 14 Temmuz 2012
İHA Hava Verileri Sisteminde Arıza Tespiti Ayıklanması ve Tümleştirilmiş Süzme
Ulusal Havacılık ve Uzay Konferansı (UHUK-2012), Türkiye, 12 - 14 Temmuz 2012
A novel adaptive unscented Kalman filter for pico satellite attitude estimationHE Soken
PHYSCON, 2011, 5 - 08 Eylül 2011
Development of Autonomous Underwater Vehicle NavigationSystem Based on Kalman Filtering Technique
18th St.Petersburg International Conference on Integrated Navigation Systems (ICINS- 2011), 30 Mayıs - 01 Haziran 2011, ss.238-242
Development of Integrated INS GPS Navigation System for Unmanned Air Vehicle Based on Kalman Filtering Technique
5th International Conference on Recent Advances in Space Technologies, 9 - 11 Haziran 2011
Nonlinear Robust Adaptive EKF for Identification of EMAs Parameters in the Presence of Sensor Faults
5th International Scientific Conference on Physics and Control (PhysCon 2011), İspanya, 5 - 08 Eylül 2011
Manyetometre Ölçümlerine Göre Küçük Uydu Yönelim Dinamiğinin Genişletilmiş Kalman Süzgeci Temelli Kestirimi İTÜpSAT II Projesi
III. Ulusal Havacılık ve Uzay Konferansı (UHUK-2010), 16 - 18 Eylül 2010
Adaptıve Robust Estımatıon of the Electro Mechanıcal Actuator Parameters in the Presence of Sensor Faults
Sixth International Conference on Technical and Physical Problems of Power Engineering (ICTPE-2010), 14 - 16 Eylül 2010, ss.122-126
LQR Controller With Kalman Estimator Applied To UAV Longitudinal Dynamics
International Workshop on Unmanned Vehicles -UVW2010, 10 - 12 Haziran 2010, ss.162-166
Development of Autonomous Underwater Vehicle Navigation System Based on Kalman Filtering Technique
International Workshop on Unmanned Vehicles -UVW2010, 10 - 12 Haziran 2010
An Adaptive Sensor Fusion Method Applied to UAV Dynamics
International Workshop on Unmanned Vehicles -UVW2010, 10 - 12 Haziran 2010, ss.57-62
Attitude Determination and Control of Future Small Satellites
NATO Workshop AVT-171 “Multifunctional Structures and System Technologies for Small Spacecraft”, 12 - 15 Nisan 2010
Design and Comparison of Controllers for the Lateral Motion of Autonomus UAV
International Symposium on Engineering and Architectural Sciences of Balkan, Caucasus and Turkic Republics, 22 - 24 Ekim 2009, ss.136-141
Adaptive Fading Kalman Filters with UAV Flight Control System Applications
International Symposium on Engineering and Architectural Sciences of Balkan, Caucasus and Turkic Republics, 22 - 24 Ekim 2009, ss.58-64
An adaptive unscented Kalman filter applied for the identification of attitude dynamics parameters of a pico satellite
6th IFAC Int. Workshop Knowledge Technol. Transfer Developing Countries: Automation and Infrastructure-DECOM-09, Makedonya, 26 - 29 Eylül 2009, ss.335-340
Design and Comparison of Controllers for the Longitudinal Motion of the UAV
5th Ankara International Aerospace Conference, 17 - 19 Ağustos 2009
Adaptive Kalman Filter with the Filter Gain Correction Applied to UAV Flight Dynamics
17th Mediterranean Conference on Control and Automation. Thessaloniki, Yunanistan, 24 - 26 Haziran 2009
Adaptive Kalman Filter with the Filter Gain Correction Applied to UAV Flight Dynamics
17th Mediterranean Conference on Control and Automation, 24 - 26 Haziran 2009
UKF for the Identification of the Pico Satellite Attitude Dynamics Parameters and the ExternalTorques on IMU and Magnetometer Measurements
4th International Conference on Recent Advances in Space Technologies (RAST 2009), 11 - 13 Haziran 2009, ss.547-552
ITU pSAT I Istanbul Technical University Student Pico Satellite Program
Recent Advances in Space Technologies, 2007, 14 - 16 Haziran 2007
Aircraft sensor fault diagnosis based on kalman filter innovation sequence
37th IEEE Conference on Decision and Control, Amerika Birleşik Devletleri, 18 Aralık 1998
Aircraft sensor fault diagnosis based on Kalman filter innovation sequence
37th IEEE Conference on Decision and Control, 16 - 18 Aralık 1998
Kitap & Kitap Bölümleri
Integration of Baro-Inertial-GPS Altimeter via Complementary Kalman Filter
Advances in Sustainable Aviation, Karakoç T., Colpan C., Şöhret Y., Editör, Springer, ss.251-268, 2018
Gyroless Attitude Determination of Nanosatellites
LAP LAMBERT Academic Publishing, Saarbrücken, 2017
Diagnosis and Fault Tolerant Control in Dynamic Systems
Far Eastern Federal University, Vladivostok, 2016
State Estimation and Control for Low cost Unmanned Aerial Vehicles
Springer International Publishing Switzerland, 2015
Robust Kalman Filtering with Single and Multiple Scale Factors for Small Satellite Attitude Estimation
Advances in Estimation Navigation and Spacecraft Control, Choukroun, D., Oshman, Y., Thienel, J., Idan, M., Editör, Springer-Verlag Berlin Heidelberg, ss.391-411, 2015
Aircraft icing detection, identification and reconfigurable control
Lambert, Saarbrücken, 2011
Fault diagnosis and reconfiguration in flight control systems
Springer Science+Business Media, 2003