发明名称 Attitude control actuator, particularly for spacecraft.
摘要 <p>Two flywheels (F1, F2) are driven by respective motors (M1, M2) with opposite and equal spins, which are supported by gimbals (G1, G2). The gimbals are journaled in a frame (S), rigidly connected with the spacecraft, about respective parallel axes at right angles to the axes of the flywheels. Motor means (MG, TG, TF, T1, T2) are mounted on the frame for rotating the gimbals through desired angular displacements about their journal axes.</p>
申请公布号 EP0392130(A1) 申请公布日期 1990.10.17
申请号 EP19890830162 申请日期 1989.04.11
申请人 CONTRAVES ITALIANA S.P.A. 发明人 STELLA, DOMENICO;GRECO, EMILIO
分类号 G05D1/08;B64G1/28 主分类号 G05D1/08
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