Peculiarities of using additional low-power energy sources in the power supply system of small spacecraft

Abstract


We propose a method of selecting the orbit for spin-stabilized spacecraft in order to obtain maximum electric energy on board due to the spacecraft motion in the earth magnetic field. The article describes the peculiarities of using additional low-power energy sources for power supply systems of small space vehicles. A method is proposed for taking into account the complex dependence of the position of the resultant magnetic induction vector on the spatial attitude of the spacecraft for converting the energy of the earth magnetic field into electric power.


About the authors

D. L. Kargu

A.F. Mozhaisky Military Space Academy

Author for correspondence.
Email: dmitrii_kargu@mail.ru

Russian Federation

Candidate of Science (Engineering), Associate Professor,
Head of the Department of Airborne Electrical Equipment and Energy Systems of Flying Vehicles

A. M. Beznyakov

A.F. Mozhaisky Military Space Academy

Email: bez-al@mail.ru

Russian Federation

Candidate of Science (Engineering),
lecturer of the Department of Airborne Electrical Equipment and Energy Systems of Aircraft

A. V. Nemirov

A.F. Mozhaisky Military Space Academy

Email: nemirov-vka@yandex.ru

Russian Federation

lecturer of the Department of Airborne Electrical Equipment and Energy Systems of Flying Vehicles

N. V. Radionov

A.F. Mozhaisky Military Space Academy

Email: rnv_vka@mail.ru

Russian Federation

Doctor of Economics, Candidate of Science (Engineering), Associate Professor,
Professor of the Department of Airborne Electrical Equipment and Energy Systems of Flying Vehicles

Yu. A. Chudnovsky

A.F. Mozhaisky Military Space Academy

Email: chya_vka@mail.ru

Russian Federation

Candidate of Science (Engineering), Associate Professor,
Department of Airborne Electrical Equipment and Energy Systems of Flying Vehicles

References

  1. Kargu L., Steganov G.B., Petrenko V.I., Vlasov V.A., Ratushnyak A.I., Malenin E.N., Radionov N.V. Sistemy elektrosnabzheniya kosmicheskikh apparatov i raket-nositeley: uch. posobie [Systems of power supply for spacecraft and carrier rockets: study guide]. Saint-Petersburg: Mozhaisky Military Space Academy Publ., 2013. 116 p.
  2. Kargu D.L., Beznyakov A.M. Kombinirovannyy nakopitel' elektricheskoy energii [Hybrid energy storage unit for electrical energy: Application for invention]. Application for a discovery no. 2017100117 dated 09.01.2017.
  3. Beznyakov A.M., Kargu D.L., Kuznetsov V.A., Komarov P.A., Ovsyannikov A.E. Sistema elektrosnabzheniya kosmicheskogo apparata [Spacecraft power supply system]. Patent RF, no. 2598862, 2016. (Publ. 27.09.2016, bull. no. 27).
  4. Kargu D.L., Beznyakov A.M., Nemirov A.V. Spacecraft power supply system using additional low-power sources of energy. Vestnik of Samara University. Aerospace and Mechanical Engineering. 2016. V. 15, no. 3. P. 17-24. (In Russ.).
  5. doi: 10.18287/2541-7533-2016-15-3-17-24
  6. Chilin Yu.N. Modelirovanie i optimizatsiya v energeticheskikh sistemakh [Modelling and optimization in power systems]. Saint-Petersburg: Mozhaisky Military Space Academy Publ., 1995. 277 p.
  7. Magnetospheric Field Models. Available at:http://modelweb.gsfc.nasa.gov/magnetos/magnetos_index.html
  8. GOST 25645.126-85. Geomagnetic field. Magnetic field model of infernal originals. Moscow: Izdatel'stvo Standartov Publ., 1990. 23 p. (In Russ.)
  9. GOST 25645.127-85. Earth's magnetosphere. Magnetic field model of magnetospheric currents. Moscow: Izdatel'stvo Standartov Publ., 1990. 11 p. (In Russ.)
  10. Analogovyy mir Maxim. Novye mikroskhemy.Vyp. 2 [Analog world of Maxim. Novel microcircuits. Iss. 2]. Maxim Integrated Products, 2013. 64 p.

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