Urmăriți
Javad Tayebi
Javad Tayebi
Assistant Professor
Adresă de e-mail confirmată pe nuaa.edu.cn
Titlu
Citat de
Citat de
Anul
A comparative study of CMG and FMC actuators for nano satellite attitude control system-pyramidal configuration
J Tayebi, A Soleymani
2015 7th International Conference on Recent Advances in Space Technologies …, 2015
222015
Dynamics and control of flexible satellite using reaction sphere actuators
J Tayebi, T Chen, H Wang
Space: Science & Technology 3, 0077, 2023
172023
LQR/LQG attitude stabilization of an agile microsatellite with CMG
J Tayebi, AA Nikkhah, J Roshanian
Aircraft Engineering and Aerospace Technology 89 (2), 290-296, 2017
142017
Disturbance observer backstepping sliding mode agile attitude control of satellite based on the anti-saturation hybrid actuator of the magnetorquer and magnetically suspended wheel
J Tayebi, C Han, Y Yu
Proceedings of the Institution of Mechanical Engineers, Part G: Journal of …, 2022
22022
Designing and Implemntation of PID and Feed back Quaternion Control Strategies for Three Axis Satellite Simulator Equipped With Control Moment Gyros Actiatprs
A Aghalari, J Tayebi
Journal of Space Science and Technology 9 (1), 13-23, 2016
12016
Attitude Stability Testing of an Agile Satellite Simulator with Single-Gimbal Control-Momentum-Gyros
A Aghalari, J Tayebi, A Kalhor
Journal of Space Science and Technology 5 (4), 61-68, 2013
12013
Test Mass Capture Control for Drag-Free Satellite Based on State-Dependent Riccati Equation Method
Y Chen, Y Wang, T Chen, Z Wei, J Tayebi
Actuators 13 (11), 434, 2024
2024
High accuracy disturbance observer-based agile attitude stabilization with three-dimensional MSW
J Tayebi, C Han, Y Yu
Aircraft Engineering and Aerospace Technology 93 (5), 862-869, 2021
2021
Sistemul nu poate realiza operația în acest moment. Încercați din nou mai târziu.
Articole 1–8