Shenzhen Fire Power Control Technology Co., LTD
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1. Product application areas
Aerospace: for attitude control, navigation and stabilization systems of aircraft.
Unmanned systems: navigation and attitude control for unmanned aircraft, unmanned vehicles and unmanned ships.
Navigation and submarine: inertial navigation system for ships and submarines.
Land Vehicles: Inertial Measurement Units (IMUs) for self-driving cars, AGVs (Automated Guided Vehicles).
Robotics: Attitude control and motion detection for industrial and service robots.
Precision instruments: for high-precision measurement equipment, such as LIDAR, optical stabilization platforms, etc.
2. Overall dimensions
3. Parameters
| Serial number | Test item | Unit | Technical requirements |
| 1 | Start-up time | min | Power-on bias stability index |
| 2 | Zero bias stability | (°)/h | ≤ 0.05 (10s smoothing) ≤ 0.015 (100s smoothing) |
| 3 | Zero bias stability at full temperature (1 ℃/min variable temperature, 100 s average) | (°)/h | ≤0.08 |
| 4 | Zero-bias repeatability | (°)/h | ≤0.015 |
| 5 | Random walk coefficient | (º)/h1/2 | ≤0.003 |
| 6 | Scale factor nonlinearity | ppm | ≤20 |
| 7 | Scale factor asymmetry | ppm | ≤5 |
| 8 | Scale factor repeatability | ppm | ≤10 |
| 9 | Scale factor repeatability (full temperature) | ppm | ≤50 |
| 10 | Operating temperature | ℃ | -40~+60 |
| 11 | Storage temperature | ℃ | -50~+70 |
| 12 | Dynamic range | (°)/s | ±500 |
| 13 | Supply voltage | V | +5V |
| 14 | Steady state power consumption (full temperature) | W | ＜4 |
4. Production environments