Tactical Inertial Navigation Solutions
We develop Inertial Measurement Units that deliver high-output rate, low-noise accelerometer, gyroscope and magnetometer data, and are fully calibrated across the full temperature range of -40 °C to +85 °C. All our units incorporate an onboard Attitude, Heading and Reference System (AHRS) algorithm for real-time, continuous 360° attitude (yaw, pitch and roll) output, providing optimal heading estimates even in challenging magnetic environments.
Our GNSS-aided INS, featuring industry-leading inertial navigation algorithms, deliver higher-accuracy estimates and better dynamic performance than standalone GNSS or INS.
Outputting accelerometer, gyroscope and magnetometer data, as well as attitude, position, velocity and timing, our GNSS/INS go beyond what products of their size and weight typically deliver.