NON-ITAR Commercial MEMS Analog Output IMU ±5 or ±2.5 Volt Signal Output Swing Low Gyro Noise < 0.0016°/sec/VHz (250°/sec) Low Accel Noise < 0.04mg/VHz (6g) In Run Gyro Bias 3°/hour 1a Fully Temperature Compensated Bias and Scale Factor -40°C to +85°C Compensated Misalignment 1/2 mrad and g-Sensitivity < 0.001°/sec/g typical Input Power +7 V to +36 V (single sided) Light Weight < 170 grams Wide Sensor Bandwidth 250 Hz Bandwidth Filtering Capability External Sync (6 kHz) Precision Alignment Vibration 8 gRMS Shock Resistant 600g's 6 Internal Temperature Sensors Self Test High MTBF 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 Gladiator Technologies Division LKD Aerospace 8020 Bracken Place SE Applications Automotive Testing Railway Motion Monitoring Antenna Stabilization Antenna Pointing Platform Stabilization EO/IR Stabilization Flight Testing Track Telemetry Laboratory Use [email protected] www.gladiatortechnologies.com

Axes (Top View) Right Hand Rule Preliminary Specification Mating Connector: M83513/03B03N Pin No. For -250 the analog signals are ± 5 volts full scale measured with respect to signal ground Pin 8. For-490 the analog signals are ±2.5 volts full scale measured with respect to 2.5 V reference Pin 8. Load > 5 kQ and <100 pf on each signal. Specification subject to change without notice