发明名称 INERTIALLY STABILIZED GIMBAL PLATFORM
摘要 An inertially stabilized gimbal platform is disclosed wherein the gyros used in such system operate about their mechanical null positions and control the gimbal drive means through an electronic control section. The electronic control section includes a control signal which is combined with the gyro output to provide a drive signal for the gimbal drive means. The control signal is proportional to the offset between the electrical null position and the mechanical null position of the gyro. The control signal may be modified in accordance with platform command signals to orient the platform in a desired attitude.
申请公布号 US3875488(A) 申请公布日期 1975.04.01
申请号 US19730332856 申请日期 1973.02.15
申请人 RAYTHEON COMPANY 发明人 CROCKER, THOMAS H.;LEVITT, BARRY N.
分类号 G01C21/18;(IPC1-7):B64C17/02 主分类号 G01C21/18
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