Skip to main content
Log in

A new control law based on characteristic exponent assignment for libration point orbit maintenance

  • Research Paper
  • Published:
Acta Mechanica Sinica Aims and scope Submit manuscript

Abstract

A new method is developed for stabilizing motion on collinear libration point orbits using the formalism of the circular restricted three body problem. Linearization about the collinear libration point orbits yields an unstable linear parameter-varying system with periodic coefficients. Given the variational equations, an innovative control law based on characteristic exponent assignment is introduced for libration point orbit maintenance. A numerical simulation choosing the Richardson’s third order approximation for a halo orbit as a nominal orbit is conducted, and the results demonstrate the effectiveness of this control law.

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.

Similar content being viewed by others

References

  1. Farquhar, R.W.: The control and use of libration-point satellites. NASA Technical Report R-346, Goddard Space Flight Center, 1970

  2. Jones, B.L., Bishop, R.H.: H2 optimal halo guidance. AIAA/AAS Astrodynamics Conference, Hilton Head Island, SC, 10–12 August 1992

  3. Rahmani, A., Jalali, M.A., Pourtakdoust, S.H.: Optimal approach to halo orbit control. AIAA Guidance, Navigation, and Control Conference and Exhibit, Austin, TX, 11–14 August 2003

  4. Wong, H., Kapila, V.: Adaptive nonlinear control of spacecraft near Sun–Earth L2 lagrange point. American Control Conference, pp. 1116–1121. Denver, CO, 4–6 June 2003

  5. Gurfil, P., Meltzer, D.: Stationkeeping on libration point orbits in the elliptic restricted three-body problem. AIAA/AAS Astrodynamics Specialist Conference and Exhibit, Keystone, CO, 21–24 August 2006

  6. Koon W.S., Lo M.W., Marsden J.E., Ross S.D.: Dynamical Systems, the Three-Body Problem and Space Mission Design. Springer, Heidelberg (2006)

    Google Scholar 

  7. Szebehely V.: Theory of Orbits: the Restricted Problem of Three Bodies. Academic Press, New York (1976)

    Google Scholar 

  8. Cielaszyk D., Wie B.: New approach to halo orbit determination and control. J. Guidance Control Dyn. 19(2), 266–273 (1996)

    Article  MATH  Google Scholar 

  9. Lee Y.J., Balas M.J.: Controllers design of periodic time-varying systems via time-invariant methods. J. Guidance Control Dyn. 22(3), 486–488 (1999)

    Article  Google Scholar 

  10. Agrawal, S.K., Xu, X.: Approach via transformation to a canonical form. In: Proceedings of the American Control Conference, pp. 2819–2823, June 1998

  11. Loukianov, A.G., Utkin, V.I.: Time-varying linear system decomposed control. In: Proceedings of the American Control Conference, Philadelphia, 24–26 June 1998

  12. Wang P., Li T., Wu H.: Characteristric exponent assignment for linear periodic system. Acta Autom. Sin. 30(4), 530–538 (2004)

    MathSciNet  Google Scholar 

  13. Richardson D.L.: Analytic construction of periodic orbits about the collinear points. Celest. Mech. 22, 241–253 (1980)

    Article  MATH  Google Scholar 

Download references

Author information

Authors and Affiliations

Authors

Corresponding author

Correspondence to Jian Wei.

Additional information

The project was supported by the National Natural Science Foundation of China (10702003).

Rights and permissions

Reprints and permissions

About this article

Cite this article

Wei, J., Xu, SJ. A new control law based on characteristic exponent assignment for libration point orbit maintenance. Acta Mech Sin 26, 495–500 (2010). https://doi.org/10.1007/s10409-010-0344-5

Download citation

  • Received:

  • Revised:

  • Accepted:

  • Published:

  • Issue Date:

  • DOI: https://doi.org/10.1007/s10409-010-0344-5

Keywords

Navigation