RATE-OPTIMAL PARAMETERS OF A SATELLITE EQUIPPED WITH TWO STABILIZERS.

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作者：

Sarychev, V.A.

Yakovlev, N.I.

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来源：

Cosmic Research (English translation of Kosmicheskie Issledovaniya) | 1977年 / 15卷 / 03期

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摘要：

Equations of motion are derived for a satellite-stabilizer system. It is assumed that each stabilizer is coupled with the satellite through a one-degree-of-freedom viscoelastic suspension of the rotational or translational type. All equilibrium positions of the satellite-stabilizer system are determined. The two-stabilizer satellite is analyzed in detail. The conditions for stability near the equilibrium position are formulated for this case, and the rate-optimal parameters are determined.

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页码：302 / 311