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High Accuracy Compact Size Low Power Consumption Inertial Measurement Unit (IMU) for Aerospace and Robotics
Key Attributes
Brand Name:
The Inertial Measurement Unit (IMU)
Model Number:
F41IMU
Place of Origin:
China
Certification:
CCS
Minimum Order Quantity:
one set
Supply Ability:
30 set per month
Delivery Time:
15 Days
Payment Terms:
T/T
Standard Packaging:
carton box
Product Summary
High-precision IMU with 0.02°/√h random walk, 400°/s range, -40°C to +85°C operation. Compact, low power (≤8W), ideal for aerospace, robotics, drones. Factory calibrated with digital output.
Product Custom Attributes
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Ground Tracking Inaccuracy:
Ship's Speed (less Than 1 Kn)： ±0.01 M/s, Whichever Is Greater Ship's Speed (more Than 1 Kn)： ±1.0 % Or ±0.1 Kn, Whichever Is Greater
Water Tracking Inaccuracy:
±1.0 % Or ±0.1 Kn, Whichever Is Greater
Depth Range:
1-200 M
Transducer Diameter:
Ø112
Gate Valve Diameter:
Ø125
Gate Valve Weight:
120 Kg
Input Range:
400°/s
Interface:
I2C, SPI, UART
Dimensions:
Varies By Model, Typically In Mm Scale
Applications:
Aerospace, Robotics, Smartphones, Drones, Automotive
Operating Temperature Range:
-40°C To +85°C
Components:
Accelerometer, Gyroscope, Magnetometer
Random Walk Coefficient:
0.02°/√h
Type:
Sensor
Degrees Of Freedom:
6-DOF Or 9-DOF
Calibration:
Factory Calibrated Or User Calibratable
Zero Bias Repeatability:
0.005°/h
Output:
Digital Or Analog Signals
Output Data Format:
Quaternion, Euler Angles, Raw Sensor Data
Measurement:
Acceleration, Angular Velocity, Magnetic Field
Weight:
Typically Less Than 50 Grams
Product Description
Inertial Measurement Unit (IMU)
The Inertial Measurement Unit (IMU) features a compact size, light weight, low power consumption, and high precision. It enables the design of pure strapdown, single-axis, and dual-axis modulated inertial navigation systems, meeting the demand for small-size, high-precision inertial navigation equipment in new unmanned platforms, underwater/torpedo weaponry, and land-based/airborne weapon platforms. The unit provides dynamic measurement of carrier angular and linear motion information.
Technical Specifications
| Component | Parameter | Description | Value | Notes |
|---|---|---|---|---|
| Gyro | Zero Bias | Bias Stability (10s) | 0.3°/h | |
| Zero Bias | Bias Stability at Variable Temperature (100s) | 0.5°/h | ||
| Scaling Factor | Scale Factor Nonlinearity | ≤20ppm | ||
| Other Indicators | Random Walk Coefficient | 0.02°/½h | ||
| Range | Input Range | 400°/s | ||
| Accelerometer | Deviation | Zero Bias Repeatability | 0.3mg | |
| Zero Bias | Bias Temperature Sensitivity | 50μg/℃ | ||
| Scaling Factor | Scale Factor Repeatability | 300ppm | ||
| Scaling Factor | Scale Factor Temperature Sensitivity | 20ppm/℃ | ||
| Accelerometer | Range Indicators | Input Range | ±20g | |
| Characteristics | Environmental Performance | Operating Temperature | -40℃～60℃ | |
| Environmental Performance | Storage Temperature | -45℃～70℃ | ||
| General Requirements | Power | Power Supply | 18～36V(DC) | |
| Power | Stable Power Consumption | ≤8W | Startup Power Consumption ≤15W | |
| Mechanical | Mounting Hole Diameter | 4-Φ4.5mm | ||
| Dimensions | Size | 70.3*70.3*53 mm | ||
| Weight | Mass | ≤500g |
Structural Diagram
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