Skip to main content
SpringerLink
Log in

Synthesis of decoupling laws for controlling the angular motion of landing module with solid-fuel landing engine minimizing the transient time

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

Abstract

Application of the exact pole placement method and modal control to the problem of angular motion control of a landing module with a solid-fuel landing engine in the landing phase in the presence of deterministic external disturbances is considered. A technique for finding the poles that ensure the minimal transient time under the condition that the magnitude of the angular velocity of the landing module does not exceed a specified threshold is proposed. Examples of numerical simulation are discussed.

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. S. N. Evdokimov, S. I. Klimanov, L. I. Komarova, and E. A. Mikrin, “Control of angular motion of a landing module of “Soyuz” type upon satellite returning from the orbit,” J. Comput. Syst. Sci. Int. 50, 826–836 (2011).

    Article  MathSciNet  Google Scholar 

  2. Handbook of Automatic Control Theory, Ed. by A. A. Krasovskii (Nauka, Moscow, 1987) [in Russian].

    Google Scholar 

  3. 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. 51, 80–96 (2012).

    Article  MathSciNet  Google Scholar 

  4. Theoretical Foundations of Designing Information Control Systems for Space Vehicles, Ed. by E. A. Mikrin (Nauka, Moscow, 2006) [in Russian].

    Google Scholar 

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

    Google Scholar 

  6. Yu. M. Lipnitskii, A. V. Krasil’nikov, A. N. Pokrovskii, et al., Nonstationary Aerodynamics of Ballistic Flight (Fizmatlit, Moscow, 2003) [in Russian].

    Google Scholar 

  7. V. G. Mikeladze and V. M. Titov, Basic Geometric and Aerodynamic Characteristics of Aircraft and Rockets: Handbook (Mashinostroenie, Moscow, 1982) [in Russian].

    Google Scholar 

  8. GOST R25645.166-2004: Upper Earth Atmosphere. Density Model for Ballistic Calculations of Satellite Flights (Izd-vo standartov, Moscow, 2004) [in Russian].

  9. G. A. Korn and T. M. Korn, Mathematical Handbook for Scientists and Engineers (McGraw-Hill, New York, 1968; Nauka, Moscow, 1984).

    Google Scholar 

  10. N. N. Martynov, Introduction to Matlab 6 (Kudits-obraz, Moscow, 2002) [in Russian].

    Google Scholar 

  11. M. Sh. Misrikhanov and V. N. Ryabchenko, “Algebraic and matrix methods in the theory of linear MIMO systems,” Vestn. IGEU, No. 5, 196–240 (2005).

    Google Scholar 

  12. S. I. Bobrovskii, Delphi 7: Textbook (Piter, St. Petersburg, 2004) [in Russian].

    Google Scholar 

  13. A. A. Amosov, Yu. A. Dubinskii, and N. V. Kopchenova, Computational Methods for Engineers: Textbook (Vysshaya shkola, Moscow, 1994) [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, A. V. Lapin & E. A. Mikrin

  2. Moscow Institute of Physics and Technology, Institutskii per. 9, Dolgoprudnyi, Moscow oblast, 141700, Russia

    N. E. Zubov, A. V. Lapin & E. A. Mikrin

  3. Bauman State Technical University, Vtoraya Baumanskaya ul. 5, Moscow, 107005, Russia

    N. E. Zubov, A. V. Lapin & E. A. Mikrin

Authors
  1. N. E. Zubov
    View author publications

    You can also search for this author in PubMed Google Scholar

  2. A. V. Lapin
    View author publications

    You can also search for this author in PubMed Google Scholar

  3. E. A. Mikrin
    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, A.V. Lapin, E.A. Mikrin, 2013, published in Izvestiya Akademii Nauk. Teoriya i Sistemy Upravleniya, 2013, No. 3, pp. 155–166.

Rights and permissions

Reprints and permissions

About this article

Cite this article

Zubov, N.E., Lapin, A.V. & Mikrin, E.A. Synthesis of decoupling laws for controlling the angular motion of landing module with solid-fuel landing engine minimizing the transient time. J. Comput. Syst. Sci. Int. 52, 480–490 (2013). https://doi.org/10.1134/S1064230713030179

Download citation

  • Received:

  • Accepted:

  • Published:

  • Issue Date:

  • DOI: https://doi.org/10.1134/S1064230713030179

Keywords

Search

Navigation