Satellite spin axis stabilization using a single degree of freedom transverse momentum storage device

Methods and systems for stabilizing satellite spin about an intermediate inertia axis (Z) are disclosed. A set of gyros (22) sense the X component and the Y component of the angular velocity of the satellite body. A single degree of freedom momentum wheel (26) has a fixed transverse orientation with...

Ausführliche Beschreibung

Bibliographische Detailangaben

Hauptverfasser:	YOCUM, JOHN F, FOWELL, RICHARD A
Format:	Patent
Sprache:	eng ; fre ; ger
Schlagworte:	AIRCRAFT AVIATION CONTROLLING COSMONAUTICS PERFORMING OPERATIONS PHYSICS REGULATING SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES TRANSPORTING VEHICLES OR EQUIPMENT THEREFOR
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