FOG integrated inertial navigation system low cost INS
| Azimuth accuracy | Parameter | 150A | 150B | 150C | 150D | |
| (2m Baseline) | 0.1 deg | 0.1 deg | 0.1 deg | 0.1 deg | ||
| Satellite signal loss | 0.01deg /5min | 0.015deg /5min | 0.02 deg /5min | 0.025deg /5min | ||
| 0.06 deg /1h | 0.09 deg /1h | 0.12 deg /1h | 0.15 deg /1h | |||
| attitude | Roll | ≤0.1 deg | ≤0.2 deg | ≤0.5deg | ≤0.8 deg | |
| Pitch | ≤0.1 deg | ≤0.2 deg | ≤0.5 deg | ≤0.8 deg | ||
|
Combined external GPS |
Speed accuracy | 0.1m/s | ||||
| Single point positioning accuracy | DGPS accuracy 0.5m /RTK accuracy 2cm | |||||
| Directional accuracy | 0.1deg,(2m Baseline) | |||||
| measure measuring range | Azimuth | ±180 deg | ||||
| Roll angle | ±90 deg | |||||
| Pitch angle | ±90 deg | |||||
| angle speed | ±300 deg/s | |||||
| Acceleration | ±4 g | |||||
| interface characteristic | power supply | 9~36 VDC, ≤3 W @ 24VDC | ||||
| Output interface | RS422 | |||||
| Data update rate | 100 Hz @ 115,200 baud rate | |||||
| Use environment | Operating temperature | -40°C ~ +60°C | ||||
| storage temperature | -55°C ~ +85°C | |||||
| physicalcharacteristic | size | 153 ×142 × 115 mm(Designable) | ||||
| weight | ≤1000 g | |||||
| Connector | Y11P-1210ZK10 | |||||
