发明名称 |
GYROSCOPE SYSTEM |
摘要 |
A gyroscope system comprises a dual-axis rate gyroscope (1) including angle pick-offs and rotor torque applying means (5), and a control circuit (3) arranged to supply a control signal to the rotor torque applying means (5) in accordance with the output angle sensed by the angle pick-offs. The system further comprises an angular acceleration sensor (2) which is independent of the dual-axis rate gyroscope and is arranged to output a signal to the control circuit (3). The signal modifies in accordance with the sensed angular acceleration the control signal supplied to the torque applying means (5). Preferably the angular acceleration sensor (2) forms part of a guidance system independent of the dual-axis rate gyroscope (1). |
申请公布号 |
EP0329344(B1) |
申请公布日期 |
1992.01.15 |
申请号 |
EP19890301289 |
申请日期 |
1989.02.10 |
申请人 |
BRITISH AEROSPACE PUBLIC LIMITED COMPANY |
发明人 |
DOWNTON, GEOFFREY CHARLES |
分类号 |
G01C19/30;G01C19/42;G01C21/16 |
主分类号 |
G01C19/30 |
代理机构 |
|
代理人 |
|
主权项 |
|
地址 |
|