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 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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