Acta Scientific Computer Sciences

Literature Review Volume 4 Issue 3

Design Considerations of a Power Conditioning Module for Microsatellites

Mohammed Bekhti*

Algerian Space Agency, Centre for Satellites Development, Research Department in Space Instrumentation, Algeria

*Corresponding Author:Mohammed Bekhti, Algerian Space Agency, Centre for Satellites Development, Research Department in Space Instrumentation, Algeria.

Received: November 16, 2021; Published: February 25, 2022

Abstract

One of the most critical subsystems of a small satellite is the Electrical Power System EPS. Power generated on board is necessary for the satellite to operate correctly during its lifetime.
The EPS consists mainly of solar cells, batteries, voltage converters and protection circuits. The EPS is responsible of providing stable power to the rest of the satellite subsystems and payloads.
This paper discusses the design and implementation of the power conditioning module PDM for the coming generation of small satellites for the Algerian Space Agency ASAL. The design must provide a reliable protection for the subsystems from the over-current associated with a device failure.


Keywords: Power System; Small Satellites; Power Conditioning Module; Subsystems; Reliable Protection

References

  1. JZ Slowikowski and MJ Blewett. “Power supplies, conditioning and distribution on UOSAT”. The Radio and Electronic Engineer819 (1982): 425-430.
  2. UoSAT Engineering Research Unit, UoSAT Spacecraft data Booklet, Guildford, U.K.: Dept. of Electronic and Electrical Engineering University of Surrey (1987).
  3. HS Wong and MJ Blewett. “The UoSAT-2 spacecraft power system”. Journal of IERE5 (1987): S.116-S.122.
  4. DO’Sullivan. “Satellite power system topologies”. ESA Journal2 (1989): 77-88.
  5. VM Van der Zel. “MSc thesis: autonomous power system for low earth orbit microsatellite”. Guildford, United Kingdom, University of Surrey (1990).
  6. Wiley J Larson and James R Wertz. “Space mission analysis and design”. second edition, space technology library (1992).
  7. Peter Fortescue and John Stark. “Spacecraft systems engineering”. Second edition, John Wiley and Sons (1995).
  8. C Brown. “Spacecraft Mission Design”. Second Edition, EDUCATION SERIES J. S. Przemieniecki Series Editor-in-Chief, Published by American Institute of Aeronautics and Astronautics (1998).
  9. Marco D'Errico., et al. “Design and development of a power conditioning unit for an earth observation microsatellite”. 3rd IAA Symposium on Small Satellites for Earth Observation (2001).
  10. Charles D Brown. “Elements of Spacecraft Design’, EDUCATION SERIES J. S. Przemieniecki Series Editor-in-Chief”. Published by American Institute of Aeronautics and Astronautics (2002).
  11. Ned Mohan., et al. “Power Electronics: Converters, Applications, and Design”. 3rd edition (2002).
  12. Unsal Orlu., et al. Bilsat-1: power system sizing and design, , Istanbul, Turkey (2003).
  13. Mukund R Patel. “Spacecraft Power Systems”. U.S. Merchant Marine Academy, Kings Point, New York (2005).
  14. Roger Birkeland., et al. “Design of a small student satellite”. Master’s thesis, NTNU (2006).
  15. Krishna Shenai. “Spacecraft Power Systems Design to Minimize Electro Magnetic Interference (EMI) Effects”. PIERS Proceedings (2007).
  16. Craig S Clark. “An advanced eelctrical power system for cubesats”. European Small Satellite Services Symposium (2010).
  17. M Bensaada., et al. “Sliding mode controller for buck DC/DC Converter, International Multi-Conference on Systems, Signals and Devices”. IEEE 9th International Multi-Conference on Systems, Signals and Devices (SSD) (2012).
  18. M Bensaada., et al. “Sliding mode controller for buck DC-DC Converter”. International Multi-Conference on Systems, Signals and Devices (2012).
  19. Mohammed Bekhti. “Design and Qualification Tests of the Alsat-1 High Efficiency Solar Panels”. International Journal of Renewable Energy Research1 (2013).
  20. Mohammed Bekhti. “Radiation Analysis of InGaP/GaAs/Ge and GaAs/Ge Solar Cell: A comparative Study”. International Journal of Renewable Energy Research4 (2013).
  21. Anusha R and Usha P. “Fully Regulated 28V Bus Using Bidirectional Battery Charge/Discharge Regulator for Satellite Applications”. International Journal of Advanced Research in Electrical, Electronics and Instrumentation Engineering8 (2014).
  22. Mohammed Bekhti. “In Orbit Irradiation Effects Evaluation of the Alsat-1 Solar Panels”. International Journal of Energy Science and Engineering1 (2015): 24-30.
  23. Mohammed Bekhti M Bensaada., et al. “Small satellite power distribution module adopting overcurrent protection”. International Conference on Industrial Application in Engineering Science IEEE IAS Intel IEEE ICIAES (2019): 5-9.
  24. S Della Krachai., et al. “Experimental investigation of artificial intelligence applied in MPPT techniques”. International Journal of Power Electronics and Drive Systems (IJPEDS)4 (2019).
  25. K Teffah and M Bekhti. “Characterization of Solar Cells Used in First Algerian Satellite AlSat-1”. 5th International Congress on Energy Efficiency and Energy Related Materials (ENEFM 2019), 22-28 October, Fethiye - Mugla, Turkey (2019).
  26. Mohammed Bekhti and Messaoud Bensaada. “Solar Arrays and Battery Power Sources Conceptual Design for Low Earth Orbit Microsatellites”. Engineering and Applied Sciences. Special Issue: Research on Emerging Technologies in Design and Manufacturing3 (2020): 66-70.
  27.  

Citation

Citation: Mohammed Bekhti. “Design Considerations of a Power Conditioning Module for Microsatellites”. Acta Scientific Computer Sciences 4.3 (2022): 48-53.

Copyright

Copyright: © 2022 Mohammed Bekhti. This is an open-access article distributed under the terms of the Creative Commons Attribution License, which permits unrestricted use, distribution, and reproduction in any medium, provided the original author and source are credited.




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Acceptance rate35%
Acceptance to publication20-30 days

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