Output Signal Type: | Digital Output |
---|---|
Measuring Shaft Quantities: | Three |
Accuracy Grade: | 0.1deg |
GI300D inertial navigation system is based on high-precision closed-loop fiber optic gyroscope and accelerometer, and is realized through multi-
sensor fusion and navigation calculation algorithm. It provides high-precision attitude, speed, position and other information to meet the
requirements of high-precision measurement and control.
Project | Test conditions | Indicators |
Attitude accuracy | Self-seeking north | 0.1 ° × sec (Lati), 15 min alignment of stationary base; |
Attitude | 0.01°(RMS), | |
Fiber optical Gyroscope | Measuring range | ±400°/s |
Zero bias stability | ≤0.02°/h | |
Quartz flexibility Accelerometer | Measuring range | ±20g |
Zero bias stability | ≤ 50 µg (10 s average) | |
Communication interface | RS422 | 3 route(configurable to 232) |
RS232 | 2 Route | |
CAN | 2 route CAN | |
Network port | One network interface | |
Electrical characteristics | Voltage | 12~36VDC |
Power consumption | ≤24W | |
Structural characteristics | Inertial navigation host size | 188.8mm × 176.8mm × 117 mm (L × W × H) |
Weight of the main engine | ≤5kg |