IMU

· 6-axis / 9-axis MEMS sensor fusion · High-g accelerometer + gyroscope · Low bias instability · For humanoid balance control / AGV navigation / autonomous driving / UAV attitude sensing

Product Information

• Supplier Qualification: ISO 9001:2015 audited · In-house MEMS wafer packaging & calibration · 100% bias & noise test per unit
• Technical Specification: Gyro bias instability 0.5–5 °/hr · Accelerometer noise density 10–50 μg/√Hz · Output rate 200–1000 Hz · Operating −40 to +85 ℃
• Available Documents: CE / RoHS / FCC Part 15B SDoC test report / IEC 61000-4 (EMC) test report / Bias-Stability Calibration Report / EN 10204 3.1 (+UL / EAC / KC per destination)