ER-FIMU-40 High Accuracy FOG IMU
ER-FIMU-40 FOG inertial measurement unit is specially developed for tactical system applications. The product consists of all solid-state three-axis fiber optic gyroscope, three-axis quartz flexible accelerometer, body structure, data interface board and other components.
Features
- It does not rely on external signals such as GPS/BDS and base stations. It can work independently in underground, underwaterand GPS-denied environments, providing continuous angular velocity and linear velocity data.
- No wearing parts, long service life and high reliability
- Fast dynamic response, suitable for complex motion scenarios
- Wide temperature range operation: -50℃ to +80℃. Suitable for extreme temperature and humidity scenarios such as polar regions, upper air, and deserts, without performance degradation
- Small in size, light in weight, and easy to integrate
Applications
- Communication satellite antenna pointing
- Underwater robots (ROV/AUV), underwater cleaning equipment
- The primary/backup inertial navigation systems for helicopters (rescue, mapping, transportation types), suitable for low-altitude flights and mountain rescue scenarios
- Coal seam mining, underground mining equipment for non-ferrous metal mines
- Geographic information mapping, such as urban topographic mapping and farmland water conservancy mapping
- Subway tunnel boring machine (TBM)
- Medium and large-sized civilian unmanned aircraft
Specifications
Gyroscope:
| No. | Item | Unit | Parameter |
| 1 | Measuring range | º/s | -500~+500 |
| 2 | Bias stability (1σ 10s) | º/h | ≤0.1 |
| 3 | Bias stability(1σ 100s) | º/h | ≤0.035 |
| 4 | Bias repeatability | º/h | ≤0.1 |
| 5 | Random walk coefficient | º/√h | ≤ 0.01 |
| 6 | Scale factor non-linearity | ppm | ≤50 |
| 7 | Scale factor repeatability | ppm | ≤ 50 |
| 8 | Scale factor asymmetry | ppm | ≤ 50 |
| 9 | Bandwidth | Hz | ≥500 |
Accelerometer:
| No. | Item | Unit | Parameter |
| 1 | Range | g | ±50 |
| 2 | Threshold/Resolution | μg | 5 |
| 3 | Bias | mg | ≤ (±5) |
| 4 | 0g 4 Hours short time stability | μg | ≤30 |
| 5 | 1g 4Hours short time stability | μg | ≤30 |
| 6 | Bias repeatability | μg | ≤40 |
| 7 | Scale factor | mA/g | 1.3±0.2 |
| 8 | Class II non-linearity | μg /g2 | ≤ (±30) |
| 9 | Scale factor repeatability | ppm | ≤50 |
| 10 | Class II non-linearity repeatability | μg /g2 | ≤ (±30) |
| 11 | Noise (840ΩSampling resistor) | mv | ≤8.4 |
| 12 | Bandwidth | Hz | 800~2500Hz |
IMU:
| No. | Item | Unit | Parameter |
| 1 | Dimensions | mm | 100×100×75 |
| 2 | Operating temperature | ℃ | -50~+80 |
| 3 | Data output rate | Hz | 200 |
| 4 | Data update rate | Hz | 1~1000 (Adjustable) |
| 5 | Weight | Kg | 1.0±0.06 |
| 6 | Power supply | V | 28 |
| 7 | Communication interface | / | RS-422 (Customizable) |
Data update frequency: Adjustable from 1 to 1000Hz
| Byte | Data Content | Supplementary explanation |
| 1~4 | Head | 0X EB8055AA |
| 5~8 | X Gyro data | Low first, then high, dimensionless numerical quantity |
| 9~12 | Y Gyro data | Low first, then high, dimensionless numerical quantity |
| 13~16 | Z Gyro data | Low first, then high, dimensionless numerical quantity |
| 17~20 | X Accl data | Low first, then high, dimensionless numerical quantity |
| 21~24 | Y Accl data | Low first, then high, dimensionless numerical quantity |
| 25~28 | Z Accl data | Low first, then high, dimensionless numerical quantity |
| 29~30 | Temperature | Low first, then high |
| 31~33 | End | 0X 00FF34 |
The connector wiring definitions are shown in the table below:
| No | J30 | Define | Note |
| 1 | 1、3 | 12~28V | Power |
| 2 | 2、4 | GND | |
| 8 | 8 | T+ | 422 |
| 9 | 9 | T- | |
| 10 | 11 | R- | |
| 11 | 10 | R+ |
Application Techniques
1.Internal Structure Analysis of IMU
2.What are the Application Scenarios of the IMU?
3.Application of IMU in UAV Flight Control System
4.IMU in Drones (MEMS triaxial accelerometer, triaxial gyroscope, triaxial magnetometer)
6.IMU inertial measurement unit (provides odometer, position, attitude)








