发明名称 GYROSCOPE CONTROL SYSTEMS
摘要 A gyroscope system includes a gyroscope (1), angle pick-offs (5) and a control circuit (6,7). The angle pick-offs (5) sense the tilt of the gyroscope's rotor and generate a signal which is received by the control circuit (6,7). The control circuit generates a control signal which causes a torque to be applied to the rotor. The control circuit includes both a primary integrator (6) which integrates the signal from the angle pick-offs (5) and a secondary integrator (7) which integrates the signal output by the primary integrator (6). In one example an independent angular accelerometer provides a further input to the secondary integrator (7).
申请公布号 EP0359484(A3) 申请公布日期 1991.09.04
申请号 EP19890309130 申请日期 1989.09.08
申请人 BRITISH AEROSPACE PUBLIC LIMITED COMPANY 发明人 RENNIE, NIGEL FORBES C/O BRITISH AEROSPACE PLC
分类号 G01C19/30;(IPC1-7):G01C19/30 主分类号 G01C19/30
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