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Motion measurement is of potential value to controlling, monitoring or analyzing just about anything that moves.  Two type of inertial sensing are used to described motion: accelerometers to measure the rate of change of linear velocity components, and angular-rate sensors to measure the rate of change of orientation, i.e. rotational velocities.  Inertial sensors can measure the rates of change of motion across a range of frequencies from low frequency motions of ships to high frequency vibration behavior of machinery.

The Aventech Inertial Measurement Unit (IMU) is a robust, integrated, fully calibrated / compensated set of three accelerometers and three angular rate sensors.  As part of the AIMMS-20, the IMU tracks acceleration and orientation of an aircraft, which is a necessary part of resolving winds.  The IMU can operate alone communicating motion data to a host data system via one of two means: a) an RS-232 data port; or, b) a serial network bus, specifically, a Controller Area Network (CAN) interface.

By adding a dual-antenna GPS module to the IMU, one can obtain absolute orientation angles with precision levels exceeding 0.1 degree.  A proprietary algorithm was developed to fuse GPS differential phase data with angular rates from the IMU to obtain attitude measurement that is more robust and stable when undergoing significant dynamics than what would be possible with GPS-only multi-antenna methods alone.

For more information about the AIMMS-20, click here.