CSSC Star&Inertia Technology co.,ltd.
CSSC Star&Inertia Technology co.,ltd.
Add to Cart
IMU (Merak-IMU1)
This military-grade optical IMU integrates precision gyros and accelerometers in a rugged strapdown architecture. After advanced error compensation processing, it delivers real-time motion data for: • Missile guidance systems • Targeting pods • Stabilization platforms.
Performance advantages:
1) Exceptional accuracy and design adaptability;
2) Solid-state reliability;
3) Instant operation readiness;
4) Optimized SWaP-C characteristics;
5) Extended mission lifespan.
| Model | Merak-IMU1 | ||
| Item | indicator | Description | Parameter |
| Gyro | Zero bias | Bias stability (10s) | 0.005°/h |
| Zero bias stability at variable temperature (100s) | 0.02°/h | ||
| Scaling Factor | Scale factor nonlinearity | ≤20ppm | |
| Other indicators | Random walk coefficient | 0.0005°/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 | ≤16W | ||
| Mounting hole diameter | 4-Φ5.5mm | ||
| Dimensions(mm) | 130*130*110 | ||
| Weight | ≤2200g | ||