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| Categories | IMU Accelerometer Gyro | 
|---|---|
| Brand Name: | Firepower | 
| Model Number: | IMU6-1 | 
| Place of Origin: | China | 
| MOQ: | 1 | 
| Payment Terms: | T/T | 
| Supply Ability: | 1000pcs | 
| Delivery Time: | 1 week | 
| Packaging Details: | wooden carton | 
| Product Name: | IMU Gyro for UAV | 
| Gyro Measure Range: | 450deg/s | 
| Bias Stability: | 0.3°/h | 
| Scale Factor Nonlinearity: | 150ppm | 
| Scale Factor Repeatability (1σ ): | 20ppm | 
| Acc Measuring range (customizable): | ±10g | 
| Bias stability @10s: | 0.05mg | 
| 3 dB Bandwidth: | 100Hz | 
| Company Info. | 
| Shenzhen Fire Power Control Technology Co., LTD | 
| Verified Supplier | 
| View Contact Details | 
| Product List | 
| Parameter | Unit | IMU6-1 | IMU6-1A | IMU6-1B | IMU6-1C | 
| Measuring range (customizable) | °/s | ±400 | ±400 | ±400 | ±2000 | 
| In-Run Bias Stability(@ Allan variance) 
 | °/h | 0.3 | 0.1 | 0. 05 | 1 | 
| Bias stability @10s (10s smooth, 1σ, room temperature) | °/h | 3 | 1 | 0.5 | 6 | 
| Bias stability in full temperature | °/h | 10 | 3 | 2 | 18 | 
| Angular Random Walk | °/√h | 0.15 | 0.1 | 0.02 | 0.3 | 
| Bias repeatability (1σ ) | 1 | 0.5 | 0.3 | 2 | |
| Bias acceleration sensitivity | °/h/g | 1 | 1 | 1 | 2 | 
| Scale Factor Non-Linearity(1σ ) | ppm | 150 | 150 | 150 | 300 | 
| Scale Factor Repeatability (1σ ) | ppm | 20 | 20 | 20 | 100 | 
| Misalignment | ° | ±0.05 | ±0.05 | ±0.05 | ±0.05 | 
| 3 dB Bandwidth | Hz | 250 | 200 | 150 | 250 | 
| Parameter | Unit | IMU6-1y-1 | IMU6-1y-2 | IMU6-1y-3 | IMU6-1y-4 | |||
| Measuring range (customizable) | g | ±10 | ±30 | ±50 | ±80 | |||
| In-Run Bias Stability (Allan Variance @ 25 ℃) | mg | 0.02 | 0.05 | 0.1 | 0.2 | |||
| Bias stability @10s | mg | 0.05 | 0.2 | 0.5 | 1 | |||
| Bias stability in full temperature | mg | 1 | 3 | 5 | 15 | |||
| Angular Random Walk | m/s/√h | 0.001 | 0.002 | 0.005 | 0.01 | |||
| Bias repeatability(1σ ) | mg | 0.1 | 0.5 | 1 | 2 | |||
| Scale Factor Repeatability (1σ ) | ppm | 200 | 200 | 200 | 200 | |||
| Scale Factor Non-Linearity(1σ ) | ppm | 50 | 100 | 200 | 300 | |||
| Misalignment | ° | ±0.05 | ±0.05 | ±0.05 | ±0.05 | |||
| 3 dB Bandwidth | Hz | 100 | 100 | 100 | 100 | |||
| Parameter | Unit | IMU6-1y-x | 
| Measuring range (customizable) | g | ±1.7 | 
| Bias stability (1s smoothing) | mg | 0.5 | 
| Random walk | m/s/√h | 0.08 | 
| Scale factor non-linearity | ppm | 100 | 
| Parameter | Unit | IMU6-1y-x | 
| Voltage | V | 5 | 
| Power consumption | W | 2 | 
| Ripple | mV | 100 | 
| Parameter | Unit | IMU6-1y-x | 
| Operating temperature | ℃ | -45~85 | 
| Storage temperature | ℃ | -55~105 | 
| Vibration | -- | 10~2000Hz,6.06g | 
| Impact | -- | 1000g,0.1ms | 
| Parameter | Unit | IMU6-1y-x | 
| Weight | g | 55±5 | 
MEMS Inertial Measurement Unit (IMU) integrates a three-axis gyroscope, three-axis accelerometer, three-axis inclinometer, temperature sensor, and signal processing board into a compact, robust system. It measures angular rate, acceleration, and inclination of a carrier with high accuracy and outputs compensated data (temperature, misalignment, nonlinear errors) via RS-422. Ideal for navigation, attitude control, and stabilization, this MEMS IMU offers a cost-effective and high-performance replacement for STIM300 in UAVs, vehicles, and industrial platforms.
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