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 | 22 | 2015 |
Dynamics and control of flexible satellite using reaction sphere actuators J Tayebi, T Chen, H Wang Space: Science & Technology 3, 0077, 2023 | 17 | 2023 |
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 | 14 | 2017 |
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 | 2 | 2022 |
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 | 1 | 2016 |
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 | 1 | 2013 |
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 |