发明名称 Gyroscope closed-loop speed controller
摘要 A closed-loop controller for controlling the frequency of the power applied to a gyroscope synchronous motor to rotate the seismic mass (wheel) of the gyro so as to compensate for movement of the gyro case about the spin axis of the gyro is disclosed. The controller includes a sensor for sensing fluctuations in the current drawn by the gyro, said fluctuations being directly related to the fluctuations in the load angle of the gyro caused by movement of the gyro case about the spin axis. The current fluctuations create an analog voltage, which is amplified by several orders of magnitude. The result is used to modulate the frequency of the applied power so as to compensate for the load angle fluctuations caused by case movement about the spin axis. In essence, the controller reduces the frequency of the hunting mode of the gyro to a level below which movement of the gyro case about its spin axis has substantially no undesirable effect. In addition, the controller phase shifts the feedback modulation signal so as to damp hunting excursions at the lower hunting mode frequency. Finally, noise signals, particularly noise signals at the motor excitation frequency, are filtered out to prevent such signals from saturating the feedback electronics.
申请公布号 US4269073(A) 申请公布日期 1981.05.26
申请号 US19780927453 申请日期 1978.07.24
申请人 THE BOEING COMPANY 发明人 MCINTYRE, MELVILLE D.
分类号 G01C19/08;G01C19/06;(IPC1-7):G01C19/08;H02P7/00 主分类号 G01C19/08
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