IMU 600 - Fiber Optic Gyro Inertial Measurement Unit

The IMU 600 is a small, high-performance inertial sensor incorporating  three FOG 600s and three accelerometers. The IMU 600 (0.01°/hr typical in-run drift stability) is designed for applications requiring higher accuracy than the IMU 200, including navigation, precision pointing and satellite stabilization.

A version of this IMU 600 is deployed aboard the F/A-18 fighter aircraft as part of the Advanced Targeted Forward Looking Infra-Red (ATFLIR) program.

IMU 600 Features and Benefits

IMU 600 Applications

The IMU 600's high performance makes it suitable for a number of demanding applications including:

The gyro channels have wide bandwidth enabling the IMU to be  used for applications such as gimbal stabilization and motion compensation. Inertial data is precisely time tagged — often required for tight integration  with GPS.

Interface

The IMU 600 has a high speed RS-485 digital interface and  provides three axes of delta velocity and three axes of delta angle at a 2 kHz  rate. The IMU 600 requires ±15 V, ±5V.

Size

The IMU 600 shown is a custom  configuration in production for the ATFLIR application. The IMU 600 can be  repackaged for other applications.

Weight

The IMU 600 weighs 3.5 lb (1.6 kg). 

Environment

The IMU 600 was designed and qualified for flight in a military  fighter aircraft environment.

Performance

Northrop Grumman developed the IMU 600 for military applications demanding high accuracy over a wide temperature range.  Any IMU’s performance is affected by the operating environment. In a benign environment, gyro bias stability (short term drift) for this IMU is approximately 0.01°/hr.