The use of the exact pole placement algorithm for the control of spacecraft motion

  • Authors:
  • N. E. Zubov;E. A. Mikrin;M. Sh. Misrikhanov;V. N. Ryabchenko;S. N. Timakov

  • Affiliations:
  • S.P. Korolev Rocket and Space Corporation "Energia", Korolev, Moscow oblast, Russia 141070;S.P. Korolev Rocket and Space Corporation "Energia", Korolev, Moscow oblast, Russia 141070;S.P. Korolev Rocket and Space Corporation "Energia", Korolev, Moscow oblast, Russia 141070;S.P. Korolev Rocket and Space Corporation "Energia", Korolev, Moscow oblast, Russia 141070;S.P. Korolev Rocket and Space Corporation "Energia", Korolev, Moscow oblast, Russia 141070

  • Venue:
  • Journal of Computer and Systems Sciences International
  • Year:
  • 2013

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Abstract

For a linear steady model of spacecraft motion, a method for the simultaneous observation and identification in the process of motion control is proposed. The method is based on the exact pole placement algorithm and the mathematical model of the Luenberger observer. Examples illustrating the advantages of this method for practical observation and identification problems in controlling a spacecraft motion are discussed.