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Nonlinear Dynamics of the Spacecraft Gyromoment Control System with Plasma Thrusters at Initial Modes

Yevgeny Somov, Gennady Titov, Valentine Rayevsky, Yevgeny Yakimov
Recently, space science and engineering advanced new problem before theoretical mechanics and motion control theory: a spacecraft directed respinup by the weak restricted control internal forces. The paper presents some results on this problem, which is very actual for energy supply of the small communication satellites with plasma thrusters at initial mission modes.
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