Skip to main content
Log in

A splitting of collinear libration points in circular restricted three-body problem by an artificial electrostatic field

  • Original paper
  • Published:
Nonlinear Dynamics Aims and scope Submit manuscript

Abstract

This paper focuses on the study of a new type of a planar, circular restricted three-body problem with an attractive artificial electrostatic field (E-field) at collinear libration points. For instance, this attractive field can be generated by an orbiting spacecraft located at the Mars-Phobos L1 libration point and an electrostatic capsule launched from Phobos. The feasibility of the proposed retrieval system is discussed from the aspect of local space weather Debye length. The attractive E-field splits the collinear libration point into two new collinear points, and the greater the E-field potential and the Debye length the greater the distance between the new libration points and the “old” original libration point. The new equilibrium positions caused by the action of the E-field have been found, and an instability of these new libration points has been proven. A new Jacobi integral in analytical form is obtained and equations of motion are derived for the restricted problem of three bodies taking into account the E-field. A numerical simulation shows the impact of the E-field potential on capsule capture in the small vicinity of the Mars-Phobos L1 libration point. This work expands the classic three-body problem filling with new content. The obtained results can be applied, for example, to study an opportunity of delivering the Phobos samples using Coulomb interaction of bodies in space.

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

Access this article

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

Instant access to the full article PDF.

Fig.1
Fig. 2
Fig. 3

Similar content being viewed by others

References

  1. Szebehely, V.: The Restricted Problem of Three Bodies. Academic Press Inc., New York (1967)

    MATH  Google Scholar 

  2. Connor Howell, K.: Three-dimensional, periodic, ‘halo’ orbits. Celestial Mech. 32, 53–71 (1984). https://doi.org/10.1007/BF01358403

    Article  MathSciNet  MATH  Google Scholar 

  3. Luo, T., Pucacco, G., Xu, M.: Lissajous and halo orbits in the restricted three-body problem by normalization method. Nonlinear Dyn. 101, 2629–2644 (2020). https://doi.org/10.1007/s11071-020-05875-1

    Article  Google Scholar 

  4. Zotos, E.E.: Classifying orbits in the restricted three-body problem. Nonlinear Dyn. 82, 1233–1250 (2015). https://doi.org/10.1007/s11071-015-2229-4

    Article  MathSciNet  MATH  Google Scholar 

  5. Ferrari, F., Lavagna, M.: Periodic motion around libration points in the elliptic restricted three-body problem. Nonlinear Dyn. 93, 453–462 (2018). https://doi.org/10.1007/s11071-018-4203-4

    Article  Google Scholar 

  6. Woo, P., Misra, A.K.: Equilibrium points in the full three-body problem. Acta Astronaut. 99, 158–165 (2014). https://doi.org/10.1016/j.actaastro.2014.02.019

    Article  Google Scholar 

  7. Biggs, J.D., Negri, A.: Orbit-attitude control in a circular restricted three-body problem using distributed reflectivity devices. J. Guid. Control Dyn. 42(12), 2712–2721 (2019). https://doi.org/10.2514/1.G004493

    Article  Google Scholar 

  8. Alessi, E.M., Sánchez, J.P.: Semi-analytical approach for distant encounters in the spatial circular restricted three-body problem. J. Guid. Control Dyn. 39(2), 351–359 (2016). https://doi.org/10.2514/1.G001237

    Article  Google Scholar 

  9. Shibata, T., Bennett, T., Schaub, H.: Prospects of a hybrid magnetic/electrostatic sample container retriever. J. Spacecraft Rockets 57(3), 434–445 (2020). https://doi.org/10.2514/1.A34509

    Article  Google Scholar 

  10. Dankanich, J., Klein, E.: Mars ascent vehicle development status, IEEE Aerospace Conference, Big Sky. USA (2012). https://doi.org/10.1190/AERO.2012.6187295

    Article  Google Scholar 

  11. Schaub, H., Junkins, J.: Analytical Mechanics of Space Systems, AIAA EducationSeries, 2nd edn. Reston, VA (2009)

    MATH  Google Scholar 

  12. Roy, A.E.: Orbital motion. IoP, Bristol and Philadelphia (2005)

    MATH  Google Scholar 

  13. Hartzell, C.M., Farrell, W., Marshall, J.: Shaking as means to detach adhered regolith for manned Phobos exploration. Adv. Space Res. 62(8), 2213–2219 (2018). https://doi.org/10.1016/j.asr.2017.09.010

    Article  Google Scholar 

  14. Martynov, M.B., et al.: Planetary protection principles used for Phobos-Grunt mission. Sol. Syst. Res. 45–7, 593–596 (2011). https://doi.org/10.1134/S0038094611070185

    Article  Google Scholar 

Download references

Acknowledgements

This study was supported by the Russian Science Foundation (Project No. 19-19-00085).

Author information

Authors and Affiliations

Authors

Corresponding author

Correspondence to Vladimir S. Aslanov.

Ethics declarations

Conflict of interest

The author declares that he has no conflict of interest.

Additional information

Publisher's Note

Springer Nature remains neutral with regard to jurisdictional claims in published maps and institutional affiliations.

Rights and permissions

Reprints and permissions

About this article

Check for updates. Verify currency and authenticity via CrossMark

Cite this article

Aslanov, V.S. A splitting of collinear libration points in circular restricted three-body problem by an artificial electrostatic field. Nonlinear Dyn 103, 2451–2460 (2021). https://doi.org/10.1007/s11071-021-06226-4

Download citation

  • Received:

  • Accepted:

  • Published:

  • Issue Date:

  • DOI: https://doi.org/10.1007/s11071-021-06226-4

Keywords

Navigation