| Customization: | Available |
|---|---|
| Output Signal Type: | Digital Output |
| Measuring Shaft Quantities: | Three |
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The INS600 integrated navigation system is a compact dual-axis rotating MEMS integrated navigation system. Through the realization of multi-sensor fusion and navigation calculation algorithm, it meets the requirements of precise measurement of attitude, heading, position and other information in the application fields of medium and high-precision mobile measurement systems, large unmanned aerial vehicles
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Project
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Test conditions
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Indicators
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Positioning accuracy
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GNSS Valid, Single Point
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Better than satellite positioning accuracy
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GNSS Valid, RTK
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Better than satellite positioning accuracy
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Pure inertial horizontal positioning holding
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4nm/60min(CEP)
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1nm/30min(CEP)
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200m/6min(CEP)
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Heading accuracy
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Dual antenna
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0.2 °/L (RMS)
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Heading holding
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0.05°/30min(RMS),0.1°/h(RMS)
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Self-north seeking accuracy
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0.3 ° SecL, alignment 15 min
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Attitude accuracy
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GNSS is valid
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0.05°(RMS)
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Attitude hold (GNSS failure)
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0.05°/30min(RMS),0.1°/h(RMS)
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Gyroscope
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Measuring range
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±400°/s
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Zero bias stability
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≤0.3°/h
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Accelerometer
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Measuring range
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±16g
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Zero bias stability
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≤100µg
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Physical dimensions and electrical characteristics
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Voltage
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10-36V DC
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Power consumption
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≤9W
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Interface
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2-route RS232, 1-route RS422, 1-route PPS (LVTTL/422 level)
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Size
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110mm × 94mm × 94mm (L, W, H)
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Weight
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≤1kg
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Environmental characteristics
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Operating temperature
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-40ºC+65ºC
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Storage temperature
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-45ºC+70ºC
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Vibration
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20~2000Hz,6.06g
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Impact
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30g,11ms
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Life span
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> 15 years
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Continuous working time
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>24h
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Note:
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* The alignment is valid;
* 10 s average; * With shock absorption |
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