INS-U | GPS-Aided INS with Air Data Computer - Single Antenna (original) (raw)
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Inertial Navigation Sensors: MEMS IMU, Accelerometers, Gyroscopes, AHRS, GPS-INS & Point Cloud Generation
INS-U inertial-labs Product GPS-Aided INS with Air Data Computer - Single Antenna
INS-U
The INS-U is a GNSS-aided inertial navigation system that also provides AHRS and ADC (air data computer) functionalities. Ideal for UAV (unmanned aerial vehicle) applications, it provides high-accuracy position, velocity, heading, pitch and roll data for both static and dynamic applications.
The IP67-rated sensor combines a single-antenna multi-constellation GNSS receiver, three-axis MEMS accelerometers and gyroscopes, a miniature gyro-compensated fluxgate compass, and two Honeywell TruStability pressure sensors. All sensing elements are fully calibrated over the entire operational temperature range for superior performance.
Specifications:
Dimensions | 82 x 40 x 26 mm |
---|---|
Weight | <200g |
Power | 5-32 VDC, <1W |
Update Rate | 1 – 200 Hz |
Horizontal Position Accuracy | SP: 1.5m CEP RTK: 0.01m + 1 ppm CEP |
Vertical Position Accuracy | RTK: 0.01m + 1 ppm CEP |
Velocity Accuracy | 0.05 m/s |
Heading Accuracy | Static: 0.6 deg RMS Dynamic w/GNSS: 0.3 deg RMS |
Pitch & Roll Accuracy | Static: 0.08 deg Dynamic: 0.05 deg RMS |
ADC Outputs | Static Pressure (calibrated), Dynamic Pressure (calibrated), Baro-Corrected Pressure Altitude, Pressure Altitude, Calibrated Airspeed, True Airspeed, Mach-Number, Static Pressure Over Total Pressure, True Angle of Attack, Rate of Climb |