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HOME > PRODUCT > MEMS INERTIAL > MEMS INS > INS100C-C0 Inertial Navigation System

INS100C-C0 Inertial Navigation System

QUARTZ ACCELEROMETER

INS100C-C0 Inertial Navigation System

roll & pitch attitude accuracy (GNSS valid)：0.05°

azimuth accuracy (2m antenna baseline)：0.1°

gyroscope bias stability (10 s)：0.5°/h

acceleration bias stability (10 s)：≤100µg

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