Date: 07 Mar 2011

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

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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.

Original Russian Text © N.E. Zubov, E.A. Vorob’eva, E.A. Mikrin, M.Sh. Misrikhanov, V.N. Ryabchenko, S.N. Timakov, 2011, published in Izvestiya Akademii Nauk. Teoriya i Sistemy Upravleniya, 2011, No. 1, pp. 96–106.