| Price | negotiable |
| MOQ | 1 |
| Delivery Time | 1 week for sample |
| Brand | Firepower |
| Place of Origin | CHINA |
| Certification | CE |
| Model Number | INS600 |
| Packaging Details | Sponge/Box |
| Payment Terms | L/C,T/T |
| Supply Ability | 500/Month |
| Heading Accuracy | 0.2 °/L (RMS) | Place of Origin | CHINA |
| Accelerometer Bias Stability | ≤100ug | Gyro Bias Stability | ≤0.3°/h |
| Packaging Details | Sponge/Box | Model Number | INS600 |
| Supply Ability | 500/Month | Accelerometer Range | ±16g |
| Certification | CE | Weight | ≤1kg |
| Brand Name | Firepower | Payment Terms | L/C,T/T |
| Gyro Range | ±400°/s | Price | negotiable |
| Delivery Time | 1 week for sample | Minimum Order Quantity | 1 |
| Attitude Accuracy | 0.05°(RMS) | Interface | 1 Channel 422/232/CAN/PPS |
| Attribute | Value |
|---|---|
| Gyro Range | ±400°/s |
| Gyro Bias Stability | ≤0.3°/h |
| Accelerometer Range | ±16g |
| Accelerometer Bias Stability | ≤100µg |
| Heading Accuracy | 0.2 °/L (RMS) |
| Attitude Accuracy | 0.05°(RMS) |
| Interface | 1 Channel 422/232/CAN/PPS |
| Weight | ≤1kg |
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.
| 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 |
