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
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