Best Practices for Hardware-in-the-Loop Testing of Minisatellite Optimal Attitude Control
Journal of Aeronautics and Space Technologies, Vol. 17, Mayıs 2024, s. 262-273, ISSN: 1304-0448
SAYIN EMRE,BAYEZİT İSMAİL,YILMAZ SERHAT
|
Design and control of ground test set-up for attitude control of nano-sized satellite
Lisansüstü Eğitim Enstitüsü, İstanbul Teknik Üniversitesi, 2021
ABDURRAHİM BİLAL ÖZCAN
|
Nonlinear model predictive control with real time iteration for F-16 attitude control
Fen Bilimleri Enstitüsü, İstanbul Teknik Üniversitesi, 2024
SİYAMİ GÜRKAN KUZUCU
|
Are External Magnetic Disturbances Suppressed by Magnetometer Noise when Estimating a Nanosatellite’s Rotational Motion?
21st International Federation of Automatic Control World Congress (IFAC-V 2020), Berlin/ALMANYA, 11 Temmuz 2020, s. 15093-15098
ÇİLDEN GÜLER DEMET, KAYMAZ ZEREFŞAN, HACIZADE CENGİZ
|
Novel CubeSat Test Setup Validating Satellite Attitude Determination and Control
74th International Astronautical Congress, BAKÜ/AZERBAYCAN, 2 Ekim 2023
ÖZCAN ABDURRAHİM BİLAL, BAYEZİT İSMAİL
|
Design, analysis and development of optimal satellite attitude control system
Lisansüstü Eğitim Enstitüsü, İstanbul Teknik Üniversitesi, 2023
EMRE SAYIN
|
Cold gas thruster and controller development for satellite attitude control
Lisansüstü Eğitim Enstitüsü, İstanbul Teknik Üniversitesi, 2024
HÜDA SEDAKİ
|
A design of a test bed for cubesat attitude determination and control system
Fen Bilimleri Enstitüsü, İstanbul Teknik Üniversitesi, 2016
MEHMET ŞEVKET ULUDAĞ
|
Magnetic attitude control of a nanosatellite
Lisansüstü Eğitim Enstitüsü, İstanbul Teknik Üniversitesi, 2022
MEHMET FATİH ERTÜRK
|
Attitude estimation and reaction wheels based control of an earth-pointing small satellite
Lisansüstü Eğitim Enstitüsü, İstanbul Teknik Üniversitesi, 2024
HAKAN GÜRSOY
|
Attitude estimation and magnetic attitude control of a LEO satellite
Lisansüstü Eğitim Enstitüsü, İstanbul Teknik Üniversitesi, 2022
MEHMET EŞİT
|
Gyroless attitude and rate estimation of small satellites using singular value decomposition and extended Kalman filter
Proceedings of the 2015 16th International Carpathian Control Conference (ICCC), Szilvasvarad/MACARİSTAN, 27 Mayıs 2015, s. 159-164
HACIZADE CENGİZ,ÇİLDEN DEMET,SOMOV YEVGENY
|
Test Platform for Small Satellite Attitude Determination and Control System
9th International Conference on Mechanical and Aerospace Engineering, 10 Temmuz 2018
KUTLU AYKUT,ÇİLDEN GÜLER DEMET,HACIZADE CENGİZ
|
Integrated SVD EKF for Small Satellite Attitude Determination and Rate Gyro Bias Estimation
2015 IFAC Workshop on Advanced Control and Navigation for Autonomous Aerospace Vehicles, Sevilya/İSPANYA, 10 Haziran 2015
HACIZADE CENGİZ,ÇİLDEN DEMET,SOMOV YEVGENY
|
Nontraditional Approach to Satellite Attitude Estimation
International Journal of Control Systems and Robotics, Vol. 1, Mart 2016, s. 19-28, ISSN: 2367-8917
HACIZADE CENGİZ,ÇİLDEN DEMET
|
Fault tolerant control of attitude dynamics of nanosatellites
International Journal Of Sustainable Aviation, Vol. 4, No. 2, 2018, s. 99-113, ISSN: 2050-0467
ÇİLDEN GÜLER DEMET,HACIZADE CENGİZ,DAŞDEMİR JANSET
|
Integrated SVD/EKF for small satellite attitude determination and rate gyro bias estimation
IFAC Workshop on Advanced Control and Navigation for Autonomous Aerospace Vehicles ACNAAV’15, Vol. 48, No. 9, 10 Haziran 2015, s. 233-238, ISSN: 24058963
HACIZADE CENGİZ,ÇİLDEN GÜLER DEMET,SOMOV YEVGENY
|
Q-Adaptation of SVD-aided UKF Algorithm for Nanosatellite Attitude Estimation
The 20th World Congress of the International Federation of Automatic Control,, TOULOUSE/FRANSA, 9 Temmuz 2017
HACIZADE CENGİZ,HALIL ERSIN SOKEN,ÇİLDEN GÜLER DEMET
|
Nontraditional Approach to Satellite Attitude Estimation
International Conference on. ROBOTICS, CONTROL and MANUFACTURING TECHNOLOGY (ROCOM '16), 18 Mart 2016
HACIZADE CENGİZ,ÇİLDEN GÜLER DEMET
|
Fault Tolerant Control of Attitude Dynamics ofNanosatellites
8th International Conference on Recent Advances in Space Technologies - RAST 2017, 19 Haziran 2017
ÇİLDEN GÜLER DEMET,HACIZADE CENGİZ,DAŞDEMİR JANSET
|