Mathematics in Computer Science

, Volume 11, Issue 3–4, pp 383–391 | Cite as

Three-Body Problem with Variable Masses that Change Anisotropically at Different Rates

  • M. Zh. Minglibayev
  • A. N. Prokopenya
  • G. M. Mayemerova
  • Zh. U. Imanova
Article
  • 84 Downloads

Abstract

In this paper we consider a general case of the three-body problem with variable masses that change anisotropically at different rates. Due to the change of masses reactive forces appear which significantly complicate the problem. Equations of motion of the system have been derived in Jacobi coordinates for the first time. Using these equations of motion and applying the methods of perturbation theory in modified Jacobi and Delaunay elements, we have obtained canonical equations of perturbed motion of the system in the presence of reactive forces. Canonical system of equations for secular perturbations in the three-body problem with variable masses changing anisotropically was derived in explicit form in terms of the analogues of the second system of Poincaré elements. An approximate analytical solution of the differential equations for secular perturbations was obtained by Picard’s method.

Keywords

Three-body problem Variable masses Reactive forces Secular perturbations Analogues of the Poincare second system 

Mathematics Subject Classification

Primary 70F07 Secondary 70P05 

Preview

Unable to display preview. Download preview PDF.

Unable to display preview. Download preview PDF.

References

  1. 1.
    Omarov, T.B. (ed.): Non-Stationary Dynamical Problems in Astronomy. Nova Science Publishers. Inc., New York (2002)Google Scholar
  2. 2.
    Bekov, A.A., Omarov, T.B.: The theory of orbits in non-stationary stellar systems. Astron. Astrophys. Trans. 22, 145–153 (2003)CrossRefGoogle Scholar
  3. 3.
    Eggleton, P.: Evolutionary Processes in Binary and Multiple Stars. Cambridge University Press, Cambridge (2006)CrossRefGoogle Scholar
  4. 4.
    Luk’yanov, L.G.: Dynamical evolution of stellar orbits in close binary systems with conservative mass transfer. Astron. Rep. 52, 680–692 (2008)CrossRefGoogle Scholar
  5. 5.
    Minglibayev, M.Zh.: Dinamika gravitiruyushchikh tel s peremennymi massami i razmerami. Postupatel’noye i postupatel’no-vrashchatel’noye dvizheniye. LAP LAMBERT Academic Publishing, Saarbrucken (2012)Google Scholar
  6. 6.
    Minglibayev, M.Zh., Mayemerova, G.M.: Investigation of the evolution equations of the three-body problem with variable masses. Appl. Math. Sci. 7, 4439–4454 (2013)Google Scholar
  7. 7.
    Prokopenya, A.N., Minglibayev, M.Zh., Mayemerova, G.M.: Symbolic calculations in studying the problem of three bodies with variable masses. Program. Comput. Softw. 40, 79–85 (2014)Google Scholar
  8. 8.
    Minglibayev, M.Zh., Mayemerova, G.M.: Evolution of the orbital-plane orientations in the two-protoplanet three-body problem with variable masses. Astron. Rep. 58, 762–772 (2014)Google Scholar
  9. 9.
    Meshchersky, I.V.: Rabotji po mehanike tel peremennoj massji. Gos. Izd. tehniko-teoret. lit, Moscow (1952)Google Scholar
  10. 10.
    Robe, H.A.: A new kind of three body problem. Celest. Mech. Dyn. Astron. 16, 343–351 (1977)CrossRefMATHGoogle Scholar
  11. 11.
    Prokopenya, A.N.: Solving Physical Problems with Mathematica. Brest State Technical University Publications, Brest (2005)MATHGoogle Scholar

Copyright information

© Springer International Publishing 2017

Authors and Affiliations

  • M. Zh. Minglibayev
    • 1
    • 2
  • A. N. Prokopenya
    • 3
  • G. M. Mayemerova
    • 1
  • Zh. U. Imanova
    • 1
  1. 1.Al-Farabi Kazakh National UniversityAlmatyKazakhstan
  2. 2.Fesenkov Astrophysical InstituteAlmatyKazakhstan
  3. 3.Warsaw University of Life SciencesWarsawPoland

Personalised recommendations