Control Systems of Moving Objects

Journal of Computer and Systems Sciences International

, Volume 50, Issue 1, pp 93-103

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

  • N. E. ZubovAffiliated withS.P. Korolev Rocket and Space Corporation “Energia”
  • , E. A. Vorob’evaAffiliated withS.P. Korolev Rocket and Space Corporation “Energia”
  • , E. A. MikrinAffiliated withS.P. Korolev Rocket and Space Corporation “Energia”
  • , M. Sh. MisrikhanovAffiliated withS.P. Korolev Rocket and Space Corporation “Energia”
  • , V. N. RyabchenkoAffiliated withS.P. Korolev Rocket and Space Corporation “Energia”
  • , S. N. TimakovAffiliated withS.P. Korolev Rocket and Space Corporation “Energia”

Rent the article at a discount

Rent now

* Final gross prices may vary according to local VAT.

Get Access

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.