Abstract

This study presents an innovative approach to attitude control in microsatellites by utilizing a spherical magnetohydrodynamic attitude control device (MHD-SACD) for three-axis attitude adjustments. A novel method is developed to quantify the output torque generated by this device, analyzing the relationship between torque, voltage, and average fluid velocity. Utilizing the energy conservation principle, an equivalent coupling circuit for the MHD-SACD is derived to assess its power dynamics. This leads to the formulation of the electromagnetic torque equation. Additionally, simulations are conducted to calculate friction torque and resultant output torque. The findings provide a qualitative assessment of the device’s torque characteristics, serving as a reference for future design optimization and setting the stage for subsequent experimental investigations. This study introduces a groundbreaking perspective to the domain of microsatellite attitude control.

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Data Availability Statement

Some or all data, models, or code that support the findings of this study are available from the corresponding author upon reasonable request.

Acknowledgments

The authors disclose receipt of the following financial support for the research, authorship, and/or publication of this article: This work is supported by the National Natural Science Foundation of China (Grant No. 51875338).

References

Akbaritabar, S., R. Esmaelzadeh, and R. Zardashti. 2018. “Comparing fluid ring and CMG servomechanisms for active control of rigid satellites.” Aircr. Eng. Aerosp. Technol. 90 (6): 896–905. https://doi.org/10.1108/AEAT-01-2017-0039.
Ben-David, O., A. Levy, B. Mikhailovich, and A. Azulay. 2014. “Magnetohydrodynamic flow excited by rotating permanent magnets in an orthogonal container.” Phys. Fluids 26 (9): 097104. https://doi.org/10.1063/1.4895901.
Geng, Y., X. Shan, X. Chen, and S. Zhang. 2012. “Design of a combined attitude and thermal control system for small satellites based on mechanically-pumped fluid loop.” Acta Aeronautica et Astronautica Sinica 33 (1): 147–155.
Gu, Y. L., Q. Liang, S. Wang, A. Zhou, and C. Liu. 2022. “Shape optimization of the momentum ring cross section for satellite attitude control based on magnetohydrodynamics.” Appl. Comput. Electromagn. Soc. J. 37 (3): 348–353. https://doi.org/10.13052/2022.ACES.J.370312.
Gu, Y. L., Q. H. Liang, A. L. Zhou, C. Z. Liu, and S. G. Wang. 2021. “Design and analysis of MHD-based momentum ring for satellite attitude adjustment.” In Proc., 4th Int. Symp. on Power Electronics and Control Engineering. Bellingham, WA: SPIE.
Ji, Y., F. Liu, X. F. Li, and J. Y. Li. 2022. “Effect of surface roughness on laminar flow in closed channels.” Phys. Fluids 34 (1): 013602. https://doi.org/10.1063/5.0078368.
Ji, Y., M. Xu, X. Li, T. Wu, W. Tuo, J. Wu, and J. Dong. 2018. “Error analysis of magnetohydrodynamic angular rate sensor combing with Coriolis effect at low frequency.” Sensors 18 (6): 1921. https://doi.org/10.3390/s18061921.
Juha, P., J. Tapani, and H. Valeria. 2018. Design of rotating electrical machines. 2nd ed. Beijing: China Machine Press.
Kelly, A., C. McChesney, P. Smith, S. Walenta, and C. Zaruba. 2004. A performance test of a fluidic momentum controller in three axes. Austin, TX: Univ. of Texas.
Kumar, K. D. 2009. “Satellite attitude stabilization using fluid rings.” Acta Mech. 208 (1–2): 117–131. https://doi.org/10.1007/s00707-008-0132-5.
Mesurolle, M., Y. Lefèvre, and C. Casteras. 2016. “Electric vector potential formulation to model a magnetohydrodynamic inertial actuator.” IEEE Trans. Magn. 52 (3): 1. https://doi.org/10.1109/TMAG.2015.2489235.
Moffatt, H. K. 1991. “Electromagnetic stirring.” Phys. Fluids A 3 (5): 1336–1343. https://doi.org/10.1063/1.858062.
Noack, D., and K. Brieß. 2014. “Laboratory investigation of a fluid-dynamic actuator designed for CubeSats.” Acta Astronaut. 96 (65): 78–82. https://doi.org/10.1016/j.actaastro.2013.11.030.
Nobari, N. A., and A. K. Misra. 2010. “Satellite attitude stabilization using four fluid rings in a pyramidal configuration.” In Proc., AIAA/AAS Astrodynamics Specialist Conf., 2010–7652. Reston, VA: American Institute of Aeronautics and Astronautics.
Nobari, N. A., and A. K. Misra. 2012. “Attitude dynamics and control of satellites with fluid ring actuators.” J. Guid. Control Dyn. 35 (6): 1855–1864. https://doi.org/10.2514/1.54599.
Salvati, A., and F. Curti. 2015. “MHD reaction wheel for spacecraft attitude control: Configuration and lumped parameter model.” In Proc., 2nd Int. Academy of Astronautics Conf. on Dynamics and Control of Space Systems, 1427–1444. Rome: Univelt.
Shan, X. W., X. Q. Chen, Y. H. Geng, and S. Zhang. 2011. “Small satellite attitude control based on mechanically-pumped fluid loops.” In Proc., 6th IEEE Conf. on Industrial Electronics and Applications, 149–153. New York: IEEE.
Soleymani, A., and M. Nosratollahi. 2020. “Simulation of thermal distribution system of microsatellite equipped with FMC actuators.” Aircr. Eng. Aerosp. Technol. 92 (10): 1505–1512. https://doi.org/10.1108/AEAT-11-2019-0213.
Soleymani, A., M. Nosratollahi, and S. H. Sadati. 2019. “Decision-making system design for satellite temperature management in the presence of fluid momentum controller actuators fault.” Modares Mech. Eng. 19 (4): 947–957.
Tayebi, J., and A. Soleymani. 2015. “A comparative study of CMG and FMC actuators for Nano satellite attitude control system-pyramidal configuration.” In Proc., 7th Int. Conf. on Recent Advances in Space Technologies (RAST), 359–365. Piscataway, NJ: Institute of Electrical and Electronics Engineers.
Varatharajoo, R., R. Kahle, and S. Fasoulas. 2003. “Approach for combining spacecraft attitude and thermal control systems.” J. Spacecraft Rockets 40 (5): 657–664. https://doi.org/10.2514/2.6914.
White, F. M. 2016. Fluid mechanics. 8th ed. New York: McGraw-Hill Education.
Zhao, Y., O. Zikanov, and D. Krasnov. 2011. “Instability of magnetohydrodynamic flow in an annular channel at high Hartmann number.” Phys. Fluids 23 (8): 084103. https://doi.org/10.1063/1.3622775.
Zhou, A. L., Y. L. Gu, C. Z. Liu, Q. H. Liang, and S. G. Wang. 2022. “Numerical simulation of the influence of geometric parameters on a spherical magnetohydrodynamic attitude controller.” Magnetohydrodynamics 58 (3): 349–369. https://doi.org/10.22364/mhd.58.3.10.
Zhou, A. L., Y. L. Gu, C. Z. Liu, S. G. Wang, and Q. H. Liang. 2023. “Numerical simulation of the coupled magnetic and liquid flow fields in a spherical magnetohydrodynamic attitude control device.” J. Aerosp. Eng. 36 (3): 04023006. https://doi.org/10.1061/JAEEEZ.ASENG-4611.

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Go to Journal of Aerospace Engineering
Journal of Aerospace Engineering
Volume 37Issue 5September 2024

History

Received: Jun 23, 2023
Accepted: Feb 13, 2024
Published online: May 17, 2024
Published in print: Sep 1, 2024
Discussion open until: Oct 17, 2024

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Ph.D. Student, School of Mechanical Engineering, Shanghai Jiao Tong Univ., Shanghai 200240, China. ORCID: https://orcid.org/0000-0002-5913-2185. Email: [email protected]
Youlin Gu, Ph.D., D.WRE [email protected]
School of Mechanical Engineering, Shanghai Jiao Tong Univ., Shanghai 200240, China. Email: [email protected]
Chaozhen Liu, Dr.Eng. [email protected]
Senior Engineer, Shanghai Key Laboratory of Aerospace Intelligent Control Technology, Shanghai Aerospace Control Technology Institute, Shanghai 201109, China. Email: [email protected]
Shigang Wang [email protected]
Professor, School of Mechanical Engineering, Shanghai Jiao Tong Univ., Shanghai 200240, China. Email: [email protected]
Professor, School of Mechanical Engineering, Shanghai Jiao Tong Univ., Shanghai 200240, China (corresponding author). ORCID: https://orcid.org/0000-0001-5407-7167. Email: [email protected]

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