Synthesis of controls for a spacecraft that optimize the pole placement of the closed-loop control system
For a linear time-independent model of spacecraft motion, a method for the optimal pole placement of the spacecraft model transition matrix closed by a feedback is proposed. The method is based on the relationship between the modal and optimization approaches to the synthesis of the feedback ensurin...
|Published in:||Journal of computer and systems sciences international, Vol. 51, No. 3 (2012), p. 431-444|
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|Item Description:||Original Russian Text © N.E. Zubov, E.A. Mikrin, M.Sh. Misrikhanov, V.N. Ryabchenko, 2012, published in Izvestiya Akademii Nauk. Teoriya i Sistemy Upravleniya, 2012, No. 3, pp. 98–111.|
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