发明名称 |
Gyroscopic platform for inertial guidance system - has gimbal mounted platform with motor-driven gyroscopic stabilisation system |
摘要 |
<p>The gyroscopic stabilised platform is used for inertial navigational equipment in aircraft and missiles. The platform is mounted on gimbals on a vertical axis and is driven by an electric motor supported on the frame of the craft. A synchro is used to measure the relative angular position between platform and craft. For measurement of angular velocity and for platform stabilisation, a gyroscope is used. Mounted on the platform may be a range finder and weapons system. Additionally the platform can contain an accelerometer. Sensor signals are transmitted to an onboard computer to output position, speed, and acceleration parameters.</p> |
申请公布号 |
DE3019743(A1) |
申请公布日期 |
1981.12.03 |
申请号 |
DE19803019743 |
申请日期 |
1980.05.23 |
申请人 |
DEUTSCHE FORSCHUNGS- UND VERSUCHSANSTALT FUER LUFT- UND RAUMFAHRT E.V. |
发明人 |
STIELER,BERNHARD,DR.-ING. |
分类号 |
G01C21/18;G01C21/20;(IPC1-7):05D3/12;41G5/16;01C21/18 |
主分类号 |
G01C21/18 |
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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