NAV-INS
Built-in high-performance MEMS Inertial Measurement Unit (IMU) and a full-system, full-frequency, high-precision positioning and orientation module, outputting information such as the carrier’s attitude, heading, position, and speed. When GNSS is not available, it can continuously output inertially calculated position, velocity, and attitude information, keeping navigation accuracy.
Heading Accuracy
Dual GNSS: 0.1°, 2m baseline (RMS)
Single GNSS: 0.1°
Magnetic Combined Accuracy: 2° (GNSS Invalid)
Attitude Accuracy
GNSS Effective: 0.1°
Inertial/Odometer Combined: 0.1°
V-G Mode: < 2°
Accelerometer
Measurement Range: ± 16g
Zero Bias Stability: 30μg
General
Voltage: 5~36 VDC
Power: ≤ 3W
Dimensions: 80*53*23 mm
Weight: ≤ 150g
Environment
IP Protection Rating: IP65
Operating Temperature: -40 ~ 70°C
Vibration: 20~2000 Hz，6.06 g
Shock: 30 g，11 ms
MTBF: 30000 h
Gyroscope
Measurement Range: ± 450°/s
Zero Bias Stability: 2 °/h
Satellite Board
Cold start: 35 s
Warm start: 5 s
Receiver type: GPS+GLO+BDS
Mechanical: ≤ 4 g
Velocity: ≤ 500 m/s
Altitude: ≤ 80000 m
- Built-in high-performance MEMS gyroscope and accelerometer.
- Inertial navigation capability when GNSS is invalid.
- Accuracy guaranteed within the -40~70°C range.
- Features sway and dynamic base alignment functions.
- Outputs raw data of IMU and satellite navigation board.