Synthesis of stabilizing spacecraft control based on generalized Ackermann’s formula

  • N. E. Zubov
  • E. A. Vorob’eva
  • E. A. Mikrin
  • M. Sh. Misrikhanov
  • V. N. Ryabchenko
  • S. N. Timakov
Control Systems of Moving Objects

DOI: 10.1134/S1064230711010199

Cite this article as:
Zubov, N.E., Vorob’eva, E.A., Mikrin, E.A. et al. J. Comput. Syst. Sci. Int. (2011) 50: 93. doi:10.1134/S1064230711010199

Abstract

Problem of modal synthesis of controllers and observers using the generalized Ackermann’s formula is solved for a spacecraft as a complex dynamic system with high interconnections. All possible controller matrices (the whole set of controllers) are obtained for solution of the problem of stabilization of orbital orientation of the spacecraft in inseparable channels of bank and yaw angles.

Copyright information

© Pleiades Publishing, Ltd. 2011

Authors and Affiliations

  • N. E. Zubov
    • 1
  • E. A. Vorob’eva
    • 1
  • E. A. Mikrin
    • 1
  • M. Sh. Misrikhanov
    • 1
  • V. N. Ryabchenko
    • 1
  • S. N. Timakov
    • 1
  1. 1.S.P. Korolev Rocket and Space Corporation “Energia”Moscow reg.Russia