علوم، فناوری و کاربردهای فضایی

علوم، فناوری و کاربردهای فضایی

Adaptive Fuzzy Sliding Mode Control of Pointing Maneuvers of an Uncertain LEO Communication Satellite

نوع مقاله : مقاله پژوهشی برتر

نویسندگان
1 School of Mechanical Engineering, Iran University of Science and Technology,
2 School of Mechanical Engineering, Iran University of Science and Technology
3 Iranian Space Research Center
چکیده
Precise pointing of a Low Earth Orbit or LEO satellite is vital to maintain the antenna, gimbaled cameras, and solar panels in the correct direction. To tackle the complexities and uncertainties in the dynamics of a typical low Earth orbit (LEO) satellite equipped with a Ka-band transmitter, and to overcome the external disturbances, this study introduces an Adaptive Fuzzy Sliding Mode Control (AFSMC) approach, which is shown to be robust against uncertainties with unknown upper bounds. The control input is directly generated by applying a sliding-mode controller, in which an adaptive method is used to estimate the upper bound of the uncertainty. In contrast to traditional Sliding Mode Control (SMC), AFSMC integrates an online-estimated fuzzy controller, obviating the need for model-based linearization. The stability of the closed-loop system is rigorously ensured through Lyapunov stability analysis. Comparative simulations against Proportional-Derivative (PD) and SMC controllers highlight the AFSMC's superior pointing accuracy and reduced energy consumption, demonstrating its effectiveness.
کلیدواژه‌ها
موضوعات

[1] K. Nobuaki, N. Keiken, and S. Shigebumi, “Accuracy Improvement of Three-Axis Stabilization Using an Onboard Computer,” Acta Astronautica, vol. 4, no. 9-10, pp. 1041-1058, 1977, https://doi.org/10.1016/0094-5765(77)90005-4
[2] T. Zwartbol, R. F. Van den Dam, A. P. Terpstra, and P. Th. L. M. Van Woerkom, “Attitude Estimation and Control of Manoeuvring Spacecraft,” Automatica, vol. 21, no. 5, pp. 513-526, 1985, https://doi.org/10.1016/0005-1098(85)90001-9.
[3] F. F. Mobley, W. E. Radford, and L. R. Kennedy, “MSX Attitude Determination and Control Hardware,” Johns Hopkins APL Technical Digest, vol. 17, no. 2, pp. 153-160, 1996.
[4] L.-H. Geng, D.-Y. Xiao, Q. Wang, T. Zhang, and J.-Y. Song, “Attitude-control model identification of on-orbit satellites actuated by reaction wheels,” Acta Astronautica, vol. 66, no. 5-6, pp. 714-721, 2010, https://doi.org/10.1016/j.actaastro.2009.08.013.
[5] M. R. Alipour, F. Fani Saberi, and M. Kabganian, “Modelling, Design, and Experimental Implementation of Non-linear Attitude Tracking with Disturbance Compensation Using Adaptive Sliding Control Based on Quaternion Algebra,” The Aeronautical Journal, vol. 122, no. 1247, pp. 1-24, 2017, https://doi.org/10.1017/aer.2017.122.
[6] Erjiang Liu, Yueneng Yang, Ye Yan, “Spacecraft attitude tracking for space debris removal using adaptive fuzzy sliding mode control”, Aerospace Science and Technology, vol. 107, 2020, https://doi.org/10.1016/j.ast.2020.106310.
[7] A. E. S. Ibrahimi, A. M. Taboli, and M. A. Sultan, “Satellite Attitude Maneuver using Sliding Mode Control under Body Angular Velocity Constraints,” International Journal of Computer Applications, vol. 50, no. 13, pp. 41-46, 2012.
[8] F. Fani Saberi, A. Fazlyab, and A. Ajorkar, “Design and Implementation of a Sliding Mode Attitude Controller of a Satellite in Software in the Loop Test Bed,” International Journal of Computer Applications, vol. 98, no. 16, pp. 28-34, 2014,  https://doi.org/10.5120/17270-7653.
[9] Duong, MD., Pham, QT., Vu, TC. et al, “Adaptive fuzzy sliding mode control of an actuator powered by two opposing pneumatic artificial muscles,” Journal of Scientific Reports, vol. 13, no. 8242, 2023,  https://doi.org/10.1038/s41598-023-34491-3
[10] Hao Feng, Jinye Jiang, Xiaodan Chang, at al, “Adaptive sliding mode controller based on fuzzy rules for a typical excavator electro-hydraulic position control system”, Journal of Engineering Applications of Artificial Intelligence, vol.  126, Part C, 2023, https://doi.org/10.1016/j.engappai.2023.107008
[11] M. J. Sidi, Spacecraft Dynamics and Control: A Practical Engineering Approach. Cambridge, UK: Cambridge University Press, 1997.
[12] Jungju Bae, Jaeyoung Kang, “Design concepts and control algorithm to minimize the control effort for earth-orbit-raising solar sails,” Journal of Aerospace Science and Technology, vol. 146, 2024, https://doi.org/10.1016/j.ast.2024.108994.
[13] P. R. Belanger, Control Engineering - A Modern Approach. Orlando, FL, USA: Saunders College Publishing, 1995.
[14] Bessa, Wallace Moreira, “An adaptive fuzzy sliding mode controller for nonlinear systems with non-symmetric dead-zone and its application to an electro-hydraulic system,” 2022, arXiv preprint arXiv:2205.13669.
[15] T. Iida and H. Wakana, “Satellite Antenna,” Science Direct, 2019. [Online]. Available: https://www.sciencedirect.com/topics/engineering/satellite-antenna. [Accessed: Jul. 29, 2026].
[16] F. Aguado-Agelet, A. E. Villa, M. Arias-Acuña, and F. J. Díaz-Otero, “AOCS Requirements and Practical Limitations for High-Speed Communications on Small Satellites,” International Journal of Aerospace Engineering, vol. 2019, pp. 1-16, Feb. 2019, https://doi.org/10.1155/2019/5079738.
[17] N. Chahat, R. Hodges, J. Sauder, M. Thomson, E. Peral, and Y. Rahmat-Samii, “CubeSat Deployable Ka-band Mesh Reflector Antenna Development for Earth Science Missions,” IEEE Transactions on Antennas and Propagation, vol. 64, no. 6, pp. 2083-2093, 2016, https://doi.org/10.1109/TAP.2016.2546306.
[18] A. Mousavi, A. H. Davaie-Markazi, and A. Ferrara, “A Reinforcement Learning-Based Approach for Near-Optimal Sliding-Mode Control of Output-Constrained Uncertain Nonlinear Systems,” International Journal of Robust and Nonlinear Control, vol. 33, no. 12, pp. 6655-6674, 2023, https://doi.org/10.1002/rnc.6716.
[19] J. R. Wertz, Spacecraft Attitude Determination and Control. Dordrecht, The Netherlands: Kluwer Academic Publishers, 1978.
دوره 6، شماره 1
مهر 1405
صفحه 117-131

  • تاریخ دریافت 18 مرداد 1404
  • تاریخ بازنگری 15 دی 1404
  • تاریخ پذیرش 27 بهمن 1404