Научная электронная библиотека ULRICH'S Periodicals Directory

Сибирский государственный университет
науки и технологий имени академика М.Ф. Решетнева

Сибирский аэрокосмический журнал
ISSN 2712-8970 (Print) ISSN 2782-5760 (on-line)

Сведения об образовательной организации

UDK 621.31 Doi: 10.31772/2587-6066-2020-21-1-96-105
PROSPECTS FOR THE DEVELOPMENT OF HIGH-VOLTAGE POWER SUPPLY SYSTEMS OF SPACECRAFT WITH A CHARGE-DISCHARGE REGULATOR
Filonova M. M.
Tomsk State University of Control System and Radio Electronics 40, Lenina Av., Tomsk, 634050, Russian Federation.E-mail : cmm91@inbox.ru
Changing the low-voltage level of the output load power bus (27–28 V) in the power supply system (PSS) of the spacecraft (SC) to a high-voltage (100 V) allowed us to significantly reduce the SC mass in connection with the reduction in the mass of cables and energy converting equipment (ECE). However, a number of problems have arisen related to the difficulty of matching the increased voltage levels of energy sources and loads, taking into account the necessary level of reliability of the PSS. Therefore, the issues of choosing the PSS structure and methods for developing ECE are relevant and priority task facing their developers. To date, in the field of development and creation of high-voltage high-power PSS of SC, a promising direction is their design based on integrated ECE modules, in particular, on the basis of modules of charge-discharge regulators (CDR) of accumulator batteries (AB). In the article, a calculation and comparative analysis of the SC PSS structures with the connection of the CDR module to the solar battery (SB) bus and with the connection of the CDR module to the output load power bus is performed. In the course of analysis of the results obtained, it was found that both options for the PSS implementation can be optimal depending on the given curve of the SC load and the requirements for the PSS for specific energy, weightdimension and other characteristics. The final choice of the SC PSS structure should be made subject to the specific power of the ECE and the subsequent calculation of the weight-dimension characteristics of the alternative PSS. Simulation of two options for the implementation of the AB CDR module was carried out: a push-pull converter with one inductor and a Weinberg converter with a magnetically coupled inductor and an additional power diode. It is established that both investigated options can be used in the development and creation of the CDR module of the highvoltage PSS of spacecraft. However, the design of CDR module based on the Weinberg converter can significantly reduce the values of the used inductors and output capacitors subject to the required levels of output voltage ripple.
Keywords: spacecraft, power supply system, maximum power point tracking mode, battery charge-discharge regulator, Weinberg converter.
References

1. Chernaya M. M. Method for calculating the energy characteristics and solar battery parameters of highvoltage power supply systems. Siberian Journal of Science and Technology. 2018, Vol. 19, No. 4, P. 651–657.
2. Soustin B. P., Ivanchura V. I., Chernyshev A. I., Islyaev Sh. N. Sistemy elektropitaniya kosmicheskikh apparatov [Power supply systems of space crafts]. Novosibirsk, Nauka Publ., 1994, 318 p.
3. Nesterishin M. V., Kozlov R. V., Zhuravlev A. V. [Comparative analysis of energy efficiency of energy
converting equipment with parallel and serial solar battery power controller]. Doklady TUSURa. 2018, Vol. 21.
No. 3. P. 98–102 (In Russ.).
4. Chebotaev V. E., Kosenko V. E. Osnovy proektirovaniya kosmicheskikh apparatov informatsionnogo obespecheniya [Basics of design of information space vehicles]. Krasnoyarsk, Sib. State Aerokos. Univ. Publ., 2011, 515 p.
5. Shinyakov Yu. A., Gurtov A. S., Gordeev K. G.
at al. [The choice of the structure of power supply systems for low-orbit spacecraft]. Vestnik Samarskogo gosudarstvennogo aerokosmicheskogo universiteta im.
akademika S. P. Koroleva. 2010, No. 1(21), P. 103–113
(In Russ.).
6. Akishin A. I. [Impact of electrical discharges on solar panels]. Nauchno-issledovatel'skii institut yadernoi
fiziki imeni D. V. Skobel'tsyna MGU. 2008, No. 4, P. 68–71 (In Russ.).
7. Lesnykh A. N., Sarychev V. A. [The research of high-voltage power supply systems for space crafts with
boost converter]. Vestnik SibGAU. 2006, No. 6 (13), P. 63–66 (In Russ.).
8. Chernaya M. M., Shinyakov Yu. A. [Research and development of energy-converting equipment for highvoltage power supply systems for low-Earth orbit space remote sensing devices]. Sbornik materialov VII Mezhdunarodnoi nauchnotekhnicheskoi konferentsii K. E. Tsiolkovskii – 160 let so dnya rozhdeniya. Kosmonavtika. Radioelektronika. Geoinformatika. [Proc. of the VII International Scientific and Technical Conference named K. E. Tsiolkovsky]. Ryazan', 2017, P. 134–136 (In Russ.).
9. Chernaya M. M. [Spacecraft Power Systems with Charger-Discharge Module]. Sbornik izbrannykh statey
nauchnoy sessii TUSUR. 2018, Vol.1, No. 2, P. 163–166 (In Russ.).
10. Yan Li, Trillion Q. Zheng, Qian Chen. Research on High Efficiency Non-Isolated Push-Pull Converters
with Continuous Current in Solar-Battery Systems. Journal of Power Electronics. 2014, Vol. 14, No. 3, P. 432–443.
11. Maset E., Ferreres A., Ejea J. B. et al. [High Efficiency Weinberg Converter for Battery Discharging in
Aerospace Applications]. IEEE PESC Conf. 2006, Р. 1510–1516.
12. Chen W., Rong P., Lu Z. Y. [Snubberless bidirectional DC-DC converter with new CLLC resonant tank
featuring minimized switching loss]. IEEE Trans. Ind. Electron. 2010, Vol. 57, No. 9, P. 3075–3086.
13. Borodin D. B., Tyunin S. S., Kabirov V. A., Semenov V. D. [Weinberg Bidirectional Converter for
spacecraft’s charge-discharge device]. XIII Mezhdunarodnaya nauchno-prakticheskaya konferentsiya,
posvyashchennaya 55-letiyu TUSURa. Tomsk, 2017, P. 204–207 (In Russ.).
14. Weinberg A. K., Rueda Boldo P. [A High Power, High Frequency, DC to DC Converter for Space Applications]. Power Electronics Specialists Conference. 1992, Vol. 2, Р. 1140–1147.
15. Maset E., Ferreres A., Ejea J. B. et al. [5kW Weinberg Converter for Battery Dischargingin HighPower Communications Satellites]. IEEE PESC Conf. 2005, Р. 69–75.  


Filonova Mariya Mikhailovna – Cand. Sc., senior Researcher; Tomsk State University of Control Systems
and Radioelectronics, Department of Radio Engineering Systems. Е-mail: cmm91@inbox.ru.  


  PROSPECTS FOR THE DEVELOPMENT OF HIGH-VOLTAGE POWER SUPPLY SYSTEMS OF SPACECRAFT WITH A CHARGE-DISCHARGE REGULATOR