Attitude Determination-EMES Inertial Navigation System

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Attitude Determination-EMES Inertial Navigation System

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Attitude Determination-EMES Inertial Navigation System

Performance Specifications Parameter Unit Type 004 Heading Accuracy(RMS) Heading ° 0.1(2m base line) Pitch / Roll ° 0.2 Position Accuracy Horizontal m 1.5m(Single Point)(RTK:0.8cm+1ppm) (RMS) Vertical ...

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