Skip to main content
SpringerLink
Log in

Modification of the exact pole placement method and its application for the control of spacecraft motion

  • Control Systems of Moving Objects
  • Published:
Journal of Computer and Systems Sciences International Aims and scope

Abstract

For linear stationary models of the spacecraft motion, a modification of the exact pole placement method is developed that makes it possible to design a modal control for any class of linear stationary systems. In the case of circular orbits, the modified method is used to obtain an analytical solution of the problem of gravitational angular momentum unload problem for inertial actuators of a spacecraft in the gyroscopically coupled roll-yaw channels.

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

Similar content being viewed by others

References

  1. N. E. Zubov, E. A. Mikrin, M. Sh. Misriknanov, and V. N. Ryabchenko, “Synthesis of Decoupling Laws for Attitude Stabilization of a Spacecraft,” J. Comput. Syst. Sci. Int. 50, 80–96 (2011).

    Article  Google Scholar 

  2. F. R. Gantmakher, The Theory of Matrices (Fizmatlit, Moscow, 2004; Chelsea, New York, 1959).

    Google Scholar 

  3. C. R. Rao and S. K. Mitra, Generalized Inverse of Matrices and Its Applications (Wiley, New York, 1971).

    MATH  Google Scholar 

  4. A. Ben-Israel and T. N. E. Greville, Generalized Inverses: Theory and Applications (Springer, New York, 2003).

    MATH  Google Scholar 

  5. N. E. Zubov, E. A. Mikrin, M. Sh. Misrikhanov, et al., “Identification of the Position of an Equilibrium Attitude of the International Space Station as a Problem of Stable Matrix Completion,” J. Comput. Syst. Sci. Int. 51, 291–305 (2012).

    Article  MathSciNet  Google Scholar 

  6. B. V. Raushenbakh and E. N. Tokar’, Spacecraft Attitude Control (Nauka, Moscow, 1974) [in Russian].

    Google Scholar 

Download references

Author information

Authors and Affiliations

  1. S.P. Korolev Rocket and Space Corporation “Energia”, ul. Lenina 4a, Korolev, Moscow oblast, 141070, Russia

    N. E. Zubov, E. A. Mikrin, M. Sh. Misrikhanov & V. N. Ryabchenko

Authors
  1. N. E. Zubov
    View author publications

    You can also search for this author in PubMed Google Scholar

  2. E. A. Mikrin
    View author publications

    You can also search for this author in PubMed Google Scholar

  3. M. Sh. Misrikhanov
    View author publications

    You can also search for this author in PubMed Google Scholar

  4. V. N. Ryabchenko
    View author publications

    You can also search for this author in PubMed Google Scholar

Corresponding author

Correspondence to N. E. Zubov.

Additional information

Original Russian Text © N.E. Zubov, E.A. Mikrin, M.Sh. Misrikhanov, V.N. Ryabchenko, 2013, published in Izvestiya Akademii Nauk. Teoriya i Sistemy Upravleniya, 2013, No. 2, pp. 118–132.

Rights and permissions

Reprints and permissions

About this article

Cite this article

Zubov, N.E., Mikrin, E.A., Misrikhanov, M.S. et al. Modification of the exact pole placement method and its application for the control of spacecraft motion. J. Comput. Syst. Sci. Int. 52, 279–292 (2013). https://doi.org/10.1134/S1064230713020135

Download citation

  • Received:

  • Accepted:

  • Published:

  • Issue Date:

  • DOI: https://doi.org/10.1134/S1064230713020135

Keywords

Search

Navigation