Synthesis of single-channel system unloading kinetic moment of inertia in the executive bodies of a spacecraft
Автор: Zubov N.E., Mikrin E.A., Negodyayev S.S., Ryabchenko V.N.
Журнал: Труды Московского физико-технического института @trudy-mipt
Рубрика: Геокосмическая механика и энергетика
Статья в выпуске: 3 (15) т.4, 2012 года.
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We consider the gravitational unloading kinetic moment of inertia problem in the executive bodies of the spacecraft pitch channel for pie and elliptic orbits using band criteria controllability. Control of gravitational unloading received laws and the stabilization of specified provisions of space is uniquely defined by the object parameters and the coefficients specified characteristic equation.
Inertial executive bodies, unloading kinetic moment, state feedback, closed system, orthogonal divisor of ze, band criteria of controllability
Короткий адрес: https://sciup.org/142185848
IDR: 142185848
