Based on the broad portfolio of inertial sensors, LITEF can flexibly create customized, 6-axis inertial measurement units. The most difficult requirements in terms of accuracy, form factor and interfaces can be met.

The LCR-110 is a low cost, small size, low weight hybrid GNSS/inertial reference system based on MEMS accelerometers and fiber optic gyroscopes.

Enhanced variant of the successful LCR-100 AHRS to be used as backup inertial navigation source during GPS outages.

Based on decades of experience with fiber optic gyroscopes and the development of accelerometers based on MEMS technology, LITEF successfully established its LCR-100 Attitude Heading Reference System (AHRS) with a broad number of airborne platforms.

Based on MEMS-technology gyroscopes and accelerometers, the LCR-350B AHRS delivers ultimate reliability under the most challenging and most demanding operational conditions.

The µIMU is based on MEMS sensors that we developed in-house and is the perfect measuring unit for stabilization and navigation.

The EF2000 IMU is an inertial Attitude and Heading Reference System relevant to flight safety that was developed for the flight control in the Eurofighter Typhoon.

The MC (Main Computer) controls the avionics and weapons systems of the Tornado fighter aircraft and ensures its operation under extreme conditions.

The LITEF Seat Sequencer (LISS) is a system for controlling the escape sequence of an ejection seat.