Download fulltext HTML
Chernaya, M. M., & Shinyakov, Y. A. (2018). High-voltage Spacecraft Power System Based on Adjustable Voltage Inverters. KnE Engineering, 3(5), 210–220. https://doi.org/10.18502/keg.v3i4.2244

https://doi.org/10.18502/keg.v3i4.2244

statistics

  • 375 Abstract Views
  • 172 PDF Views
  • 0 HTML Views

authors

  • M M Chernaya
    No author data available.
  • Y A Shinyakov
    No author data available.

Published Date

  • May 7, 2018

High-voltage Spacecraft Power System Based on Adjustable Voltage Inverters

KnE Engineering / Russian Forum of Young Scientists (RFYS) / Pages 210–220

Abstract

The authors have proposed the solar battery mathematical model based on use of its photoelectric energy converters parameters of any unit area and its experimental current-voltage characteristics, provided by manufacturer of solar batteries. The mathematical model allows drawing current-voltage and voltage-watt characteristics depending on its operation conditions and used to calculate the solar batteries electrical characteristics regardless of the manufacturing technology and the substrate material: Si, GaAs, etc. High-voltage high-efficiency spacecraft power system based on adjustable voltage inverters has been developed. The system provides for simplification of voltage matching of solar battery, accumulator battery and load and allows adjusting solar battery voltage in a range sufficient to implement the maximum power point tracking (MPPT) mode. Calculation of the solar battery parameters ensuring the restoration of the accumulator battery capacity to the beginning of a new calculation cycle for an arbitrarily compiled load curve with allowance for the solar battery maximum open circuit voltage limitation (180 V) with a change of solar battery and load powers. The results of the development and experimental researches of the energy-converting device based on voltage inverter providing a high efficiency (not less than 96 %) are shown.

References
[1] Soustin B P, Ivanchura V I, Chernyshev A I, Islyaev Sh N 1994 Spacecraft power system(Novosibirsk: Nayka) p 318.


[2] Lesnykh A N and Sarychev V A 2006 The research of high-voltage power supply systems for space crafts with boost converter Bulletin of Siberian state aerospace university named after academician M.F. Reshetnev6 63–66.


[3] Osipov A V, Shurygin Yu A, Shinyakov Yu A, Otto A I and Chernaya M M 2013 The comparative analysis of the energy conversion efficiency of solar energy by DC converters Reports of Tomsk Sate University of control systems and radioelectronics 1 (27) 14-20.


[4] Privalov V D and Nikiforov V E 1981 Evaluating the effectiveness of the maximum power point traker in autonomous power supply systems (Kuybyshev: KPI).


[5] Chernaya M M 2014 Conf. Proc. of Int. Conf. on Energy: efficiency, reliability, safety (Tomsk) vol 1 (Tomsk: Tomsk politechnic university publishing house) pp 138–143.


[6] Rozanov Yu K 1987 Semiconducter converters with link of the increased frequency(Moscow: Energoatomizdat) p 184.


[7] Chernaya M M, Shinyakov Y A and Osipov A V 2016 Proc. of the 17th International conference of young specialists on micro/nanotechnologies and electron devices. EDM 2016 (Erlagol) vol 1 (Novosibirsk: IEEE Computer Society) pp 589–593.