Comparative Study Between Fractional Linear Quadratic Regulator (Frac-LQR) and Sliding Mode Controller for the Stabilization the Three-Axis Attitude Control System of LEO Satellite Using Reaction Wheels
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Publisher
Springer Nature Switzerland
Link
https://link.springer.com/content/pdf/10.1007/978-3-031-48573-2_22
Reference4 articles.
1. Avanzini, G., et al.: Attitude control of low earth orbit satellites by reaction wheels and magnetic torquers. Acta Astronaut. 160, 625–634 (2019)
2. Ennaciri, T., Abbassi, A.E., Mrani, N., Foshi, J.: Attitude Control of LEO satellite via LQR based on reaction wheels versus magnetorquer. In: ICAISE 2022. Lecture Notes in Networks and Systems, vol. 635. Springer, Cham (2023). https://doi.org/10.1007/978-3-031-26254-8_36
3. Ennaciri, T., Mrani, N., El Abbassi, A., Foshi, J.: Comparative Study Between Linear Quadratic Regulator and Fractional-Order Robust Controller for the Three Axis Attitude Control System of LEO Satellite Using Reaction Wheels, pp. 1–5. IRASET, Meknes, Morocco (2022). https://doi.org/10.1109/IRASET52964.2022.9738361
4. Yadegari, H., Beyramzad, J., Khanmirza, E.: Magnetorquers-based satellite attitude control using interval type-II fuzzy terminal sliding mode control with time delay estimation. Adv. Space Res. 69(8), 3204–3225 (2022)
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