High Precision FOG GNSS/INS Integrated Inertial Navigation System for Unmanned Ship Navigation
Product Description
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 and so on.
Technical parameters
Project | Test conditions | Indicators |
Positioning accuracy | GNSS Valid, Single Point | Better than satellite positioning accuracy |
GNSS Valid, RTK | Better than satellite positioning accuracy |
Pure inertial horizontal positioning holding | 4nm/60min(CEP) |
1nm/30min(CEP) |
200m/6min(CEP) |
Heading accuracy | Dual antenna | 0.2 °/L (RMS) |
Heading holding | 0.05°/30min(RMS),0.1°/h(RMS) |
Self-north seeking accuracy | 0.3 ° SecL, alignment 15 min |
Attitude accuracy | GNSS is valid | 0.05°(RMS) |
Attitude hold (GNSS failure) | 0.05°/30min(RMS),0.1°/h(RMS) |
Gyroscope | Measuring range | ±400°/s |
Zero bias stability | ≤0.3°/h |
Accelerometer | Measuring range | ±16g |
Zero bias stability | ≤100µg |
Physical dimensions and electrical characteristics | Voltage | 10-36V DC |
Power consumption | ≤9W |
Interface | 2-route RS232, 1-route RS422, 1-route PPS (LVTTL/422 level) |
Size | 110mm × 94mm × 94mm (L, W, H) |
Weight | ≤1kg |
Environmental characteristics | Operating temperature | -40ºC+65ºC |
Storage temperature | -45ºC+70ºC |
Vibration | 20~2000Hz,6.06g |
Impact | 30g,11ms |
Life span | > 15 years |
Continuous working time | >24h |
Note: |
* The alignment is valid; * 10 s average; * With shock absorption |
Detailed photo


Dimension

Factory Photo

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