LandMark™60 IMU
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Automated Testing Comprehensive ERP Environmental Test Lab: - Shock - Vibration - Temperature Calibration - G-Sensivity -Axis Alignment - Centrifuge - GPS Simulation Products: Gyros Accelerometers IMU VG AHRS VG/GPS G PS/AH RS INS/GPS NON-ITAR MEMS IMU Ultra Low Gyro Noise 0.0016°/sec/lHz Low Accel Noise 0.05 mg/lHz Wide Sensor Bandwidth >250 Hz Gyro Bias In-Run 3°/hour 1o Bias Over Temperature <90°/hour 1o Compensated Misalignment < 0.5 mrad and g-Sensitivity < 0.001 °/sec/g 1o Full Temperature Calibration (Bias & SF) 16/24/32-bit Data Format (selectable) RS-422/485 Message Rate < 5 kHz (selectable) External Sync up to 6 kHz CAN BUS 2.0B 1 MHz Vibration 8grms Shock 600g Light Weight < 115 grams Low Power < 500 mW typical Gladiator Technologies Division LKD Aerospace 8020 Bracken Place SE Applications Airborne Platform Stabilization Antenna Stabilization Antenna Pointing EO/IR Stabilization LIDAR Stabilization Navigation Flight Testing o®$o sales@gladiatortechnologies.com www.gladiatortechnologies.com

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Axes (Top View) Right Hand Rule Specification Mating Connector: M83513/03-BN Pin No. Note: Any unused inputs (Pins 4, 6, 9) must be connected to signal ground (Pin 8). Specification subject to change without notice

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