Synthesis of control law for spacecraft optimal pole placement
Автор: Zubov N.E., Mikrin E.A., Negodyayev S.S., Ryabchenko V.N., Lapin A.B.
Журнал: Труды Московского физико-технического института @trudy-mipt
Рубрика: Аэрокосмические исследования, прикладная механика
Статья в выпуске: 2 (14) т.4, 2012 года.
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We consider the problem of spacecraft orbital stability. The method provides the solution of the optimal pole placement of a closed system. Using this method, the synthesis of control law with feedback for the orbital stabilization of the spacecraft is realized.
Orbital stabilization of spacecraft, feedback, optimal pole placement, decomposition, orthogonal zero devisor
Короткий адрес: https://sciup.org/142185821
IDR: 142185821
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