FIELD: gyroscopy; inertial control systems of gimballess objects.
SUBSTANCE: proposed angular-rate sensor on base of modulation gyroscope has rotor made in form of parallelepiped on elastic equal-rigid suspension placed in sealed evacuate chamber rotating together with rotor, gas-dynamic spherical supports, engine, torque sensor brought of evacuated space, information reading and rotor control unit made in rotating coordinate system in form of capacitance-frequency transducer and sine-cosine converter, as well as moving-coil torque sensor consisting of coils and two permanent magnets at radial texture of magnetizing which are diametrically opposite in gyroscope rotor; magnets and magnetic circuits are located on rotor and torque sensor windings are located behind wall of hermetic ampoule and are threaded by radial field of permanent magnets.
EFFECT: enhanced accuracy of measurement of angular rate due to linearity of moving-coil torque sensor.
5 dwg
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Authors
Dates
2006-05-20—Published
2004-05-25—Filed