Aviation Navigation TDF41A Airborne Optical Gyro Inertial Navigation System with ≤500μg Bias Repeatability, ≤0.03°/√hr Random Walk, and ≤0.2° Pitch & Roll Accuracy
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Aviation Navigation TDF41A Airborne Optical Gyro-Inertial Navigation 1 Introduction The airborne optical gyro inertial navigation system (INS) utilizes optical gyros and quartz accelerometers as its core sensors, employing either a strapdown or dithered (......
QINGDAO NAVI OPTICS TECHNOLOGY CO.,LTD
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