| Customization: | Available |
|---|---|
| Type: | Inertial Navigation |
| Output Signal Type: | Digital Output |
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The INS600A-B0 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.
| 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: | ||
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