This 9 Degrees of Freedom (DOF) Inertial Measurement Unit (IMU) is used for tracking and sensing motion of any mechanical platform and is an ideal sensor system for motion control of aerial autonomous systems like multi-rotors, model airplanes, helicopters etc, and other systems that require to control the pitch, roll and yaw. An internal processor acquires data from a gyro, an accelerometer and a magnetometer to calculate the pitch, roll and absolute heading (yaw). This is known as AHRS (Attitude Heading Reference System) that is used for aircraft control.
This IMU, with and AHRS system outputs the pitch roll and absolute heading (yaw) of the system on a TTL/CMOS compatible serial UART line.
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