Skip to main content
SpringerLink
Log in

Development of a Model of Magnetic Disturbances from Structural Elements of a Small Spacecraft and Investigation of Their Influence on the Orientation and Stabilization System

  • Published:
Solar System Research Aims and scope Submit manuscript

Abstract

The results of theoretical work on addressing the effects of magnetic disturbances in the engineering development of an attitude control system of a microsatellite are presented. Magnetic disturbances were calculated using the finite element method. Their influence on the control system was evaluated by integrating numerically the differential equations of the orbital and controlled rotational motion of the spacecraft. The magnetic field of the Earth was modeled in accordance with the IGRF-12 analytical relations.

This is a preview of subscription content, log in via an institution to check access.

Access this article

Log in via an institution

Price excludes VAT (USA)
Tax calculation will be finalised during checkout.

Instant access to the full article PDF.

Institutional subscriptions

Fig. 1.
Fig. 2.
Fig. 3.
Fig. 4.
Fig. 5.
Fig. 6.
Fig. 7.
Fig. 8.
Fig. 9.
Fig. 10.
Fig. 11.
Fig. 12.
Fig. 13.
Fig. 14.
Fig. 15.
Fig. 16.

Similar content being viewed by others

REFERENCES

  1. Arkhangel’skii, R.N., Milov, A.E., Kudryashov, P.V., Malinin, A.S., et al., RF Patent 2651309, 2017.

  2. Belyaev, B.B., Dobritsa, B.T., and Rozin, P.E., Method for increasing the accuracy of the state vector estimation while controlling the angular motion of the spacecraft in the stabilization mode, Vestn. NPO im. S.A. Lavochkina, 2013, no. 5, pp. 11–15.

  3. Dmitriev, D.V., Iosipenko, S.V., Kudryashov, P.V., Malinin, A.S., et al., Specific design of a high-resolution camera for the Earth remote sensing Auriga microsatellite, Kosmonavtika Raketostr., 2018, no. 1 (100), pp. 79–88.

  4. Folkner, W.M., Williams, J.G., Boggs, D.H., Park, R.S., et al., The Planetary and Lunar Ephemerides DE430 and DE431, IPN Progress Report 42-196, Pasadena, CA: Jet Propulsion Lab., 2014.

  5. Kovalev, A.P., Magnitnye sistemy upravleniya kosmicheksimi letatel’nymi apparatami (Magnetic Control Systems for Spacecrafts), Moscow: Mashinostroenie, 1975.

  6. Lemoine, F.G. and Kenyon, S.C., The Development of the Joint NASA GSFC and NIMA Geopotential Model EGM96, Greenbelt, MD: NASA Goddard Space Flight Center, 1998.

    Google Scholar 

  7. Malinin, A.S., Great opportunities of Auriga small spacecraft, Ross. Kosmos, 2018, no. 6 (149), pp. 42–46.

  8. Montenbruck, O. and Gill, E., Satellite Orbits: Models, Methods, and Applications, Berlin: Springer-Verlag, 2001.

    MATH  Google Scholar 

  9. Pretsizionnye splavy: spravochnik (Precision Alloys: Handbook), Molotilov, B.V., Ed., Moscow: Metallurgiya, 1974.

    Google Scholar 

  10. Rozin, P.E., The system of orientation and stabilization of the Auriga small spacecraft for Earth remote sensing, Tr. Mosk. Aviats. Inst., 2016, no. 90. http://trudymai.ru/upload/iblock/6a9/rozin_rus.pdf. Accessed September 2, 2018.

  11. Rozin, P.E., Dynamic engineering of control and navigation system for small spacecrafts for Earth remote sensing with frame survey equipment, Cand. Sci. (Eng.) Dissertation, Moscow: Moscow Aviat. Inst., 2017.

  12. Sandomirskii, S.G., Raschet i analiz razmagnichivayushchego faktora ferromagnitnykh tel (Calculation and Analysis of the Demagnetizing Factor of Ferromagnetic Bodies), Minsk: Belaruskaya Navuka, 2015.

  13. Tekhnicheskaya kibernetika. Ustroistva i elementy avtomaticheskogo regulirovnaiya i upravleniya. Kniga 3. Ispolnitel’nye ustroistva i servomekhanizmy (Technical Cybernetics. Devices and Elements of Automatic Control and Regulation, Book 3: Executive Devices and Servo Units), Solodovnikov, V.V., Ed., Moscow: Mashinostroenie, 1976.

    Google Scholar 

  14. Thebault, E., Finlay, C.C., Beggan, C.D., et al., International geomagnetic reference field: the 12th generation, Earth, Planets Space, 2015. https://doi.org/10.1186/s40623-015-0228-9

  15. Tumarina, M.V., Ryazanskii, M.V., and Milov, A.E., RF Patent 2646418, 2017.

Download references

Author information

Authors and Affiliations

  1. Dauria Aerospace, 143025, Skolkovo, Moscow oblast, Russia

    A. E. Milov & P. E. Rozin

Authors
  1. A. E. Milov
    View author publications

    You can also search for this author in PubMed Google Scholar

  2. P. E. Rozin
    View author publications

    You can also search for this author in PubMed Google Scholar

Corresponding authors

Correspondence to A. E. Milov or P. E. Rozin.

Additional information

Translated by D. Safin

Rights and permissions

Reprints and permissions

About this article

Check for updates. Verify currency and authenticity via CrossMark

Cite this article

Milov, A.E., Rozin, P.E. Development of a Model of Magnetic Disturbances from Structural Elements of a Small Spacecraft and Investigation of Their Influence on the Orientation and Stabilization System. Sol Syst Res 53, 533–542 (2019). https://doi.org/10.1134/S0038094619070141

Download citation

  • Received:

  • Published:

  • Issue Date:

  • DOI: https://doi.org/10.1134/S0038094619070141

Keywords:

Search

Navigation