CSSC Star&Inertia Technology co.,ltd.
CSSC Star&Inertia Technology co.,ltd.
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IMU (Dubhe-IMU1)
The Optical Inertial Measurement Unit (IMU) employs gyroscopes and accelerometers in a strapdown configuration, performing real-time data output according to specific protocols after compensating for installation errors and temperature effects. Applications include missile systems, pod-mounted equipment, and platforms requiring precise angular/linear rate measurements.
Key features:
1) High accuracy and stability with flexible design;
2) All-solid-state construction without moving parts;
3) Fast startup with digital output for easy integration;
4) Low noise, power consumption and cost;
5) High reliability and long service life.
| Model | Dubhe-IMU1 | ||
| Item | indicator | Description | Parameter |
| Gyro | Zero bias | Bias stability (10s) | 0.01°/h |
| Zero bias stability at variable temperature (100s) | 0.05°/h | ||
| Scaling Factor | Scale factor nonlinearity | ≤20ppm | |
| Other indicators | Random walk coefficient | 0.001°/½h | |
| Input range | 400°/s | ||
| Accelerometer | Deviation | Zero bias repeatability | 20μg |
| Zero bias | Bias temperature sensitivity | 20μg/℃ | |
| Scaling Factor | Scale factor repeatability | 20ppm | |
| Scale factor temperature sensitivity | 20ppm/℃ | ||
| Range indicators | Input range | ±20g | |
| Features | Environmental performance | Operating temperature | -40℃～60℃ |
| Storage temperature | -45℃～70℃ | ||
| General Requirements | Power supply | 18～36V(DC) | |
| Stable power consumption | ≤20W | ||
| Mounting hole diameter | 4-Φ6.5mm | ||
| Dimensions(mm) | 185*136*110 | ||
| Weight | ≤3200g | ||