发明名称 HIGH RATE ROTATION SENSING
摘要 One embodiment is directed towards an inertial measurement unit (IMU) for measuring an input rate of rotation about an input axis. The IMU includes a first three dimensional gyroscope disposed such that a first axis of its three axes is oriented at a skew angle in degrees away from a reference plane, wherein the reference plane is normal to the input axis. The IMU also includes one or more processing devices coupled to the first gyroscope. The IMU also includes one or more data storage devices coupled to the one or more processing devices, the one or more data storage devices including instructions which, when executed by the one or more processing devices, cause the one or more processing devices to calculate the input rate of rotation based on dividing a sensed rate of rotation about the first axis by the sine of the skew angle.
申请公布号 US2016097640(A1) 申请公布日期 2016.04.07
申请号 US201514608957 申请日期 2015.01.29
申请人 Honeywell International Inc. 发明人 Hanson Timothy J.;Troske Terrance;Willits David S.
分类号 G01C19/34;G01C19/44 主分类号 G01C19/34
代理机构 代理人
主权项 1. An inertial measurement unit (IMU) for measuring an input rate of rotation about an input axis, the IMU comprising: a first three dimensional gyroscope, the first gyroscope configured to sense rotation about a first set of three mutually orthogonal axes, wherein the first gyroscope is disposed such that a first axis of the first set of three axes is oriented at a skew angle in degrees away from a reference plane, the reference plane normal to the input axis; one or more processing devices coupled to the first gyroscope; and one or more data storage devices coupled to the one or more processing devices, the one or more data storage devices including instructions which, when executed by the one or more processing devices, cause the one or more processing devices to calculate the input rate of rotation based on dividing a sensed rate of rotation about the first axis by the sine of the skew angle.
地址 Morristown NJ US