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IMU588 Inertial Measurement Unit is a high performance tactical grade MEMS Inertial Measurement Unit, which MEMS gyroscope enjoys 1°/h (Allan) bias instability and MEMS accelerometer enjoys 30µg (Allan, ±16g range) bias instability, it adds another ± 50g (±100g optional) in Z axis, which increase the Z axis measurement range up to ± 50g (±100g), and it can output precise 3 axis outputs of angular rate and 3 axis acceleration data.
IMU588 Inertial Measurement Unit adopts latest MEMS technology and advanced MEMS components, and IMU588 has been produced in bulk, which reduces the cost deeply. IMU588 enjoys excellent measurement performance, small size, light weight, and high reliability and robustness, it can output precise measurement data in harsh environment, and it has been widely applied in rain-seeding rocket, target drone, unmanned aircraft, unmanned surface vessel, platform stabilization, etc.
Parameter | Test Condition | Min. | Typical | Max. | Unit |
Gyroscopes | |||||
Range① | ±450 | °/s | |||
Bias Instability | Allan variance | 0.6 | °/h | ||
10s average(-40~+85°C, fixed temp.) | 2 | °/h | |||
Bias Repeatability | 1.8 | °/h | |||
Random Walk | 0.08 | °/√h | |||
Bais | Bias change at full temp. range② | ±0.03 | °/s | ||
Bias change in vibration conditions③ | 6 | °/h | |||
Non-linearity | 100 | ppm | |||
Bandwidth | 200 | Hz | |||
Accelerometers(X/Y) | |||||
Range① | ±16 | g | |||
Bias Instability | Allan variance | 30 | 45 | ug | |
10s average(-40~+85°C, fixed temp.) | 60 | ug | |||
Bias Repeatability | 60 | ug | |||
Random Walk | 0.01 | m/s/√h | |||
Non-linearity | 100 | ppm | |||
Bandwidth | 200 | Hz | |||
Accelerometers(Z) | |||||
Range④ | ±50/±100 | g | |||
Bias Instability | Allan variance | 0.15 | mg | ||
10s average(-40~+85°C, fixed temp.) | 3 | mg | |||
Bias Repeatability | 5 | mg | |||
Random Walk | 0.1 | 0.2 | m/s/√h | ||
Non-linearity | 200 | ppm | |||
Bandwidth | 200 | Hz | |||
Magnetometer | |||||
Dynamic Range | ±2 | Gauss | |||
Resolution | 120 | uGauss | |||
Noise RMS | 10Hz | 50 | uGauss | ||
Bandwidth | 200 | Hz | |||
Barometer | |||||
Pressure Range | 450 | 1100 | mbar | ||
Resolution | 0.1 | mbar | |||
Absolute Accuracy | 1.5 | mbar | |||
Interface | |||||
UART⑤ | |||||
Baud Rate | 230400 | bps | |||
Output Rate | 200 | Hz | |||
SPI | |||||
Serial clock frequency | 25 | MHz | |||
Output Rate | 2000 | Hz | |||
Reliability | |||||
MTBF | 20000 h | ||||
Continuous Working Time | 120 h | ||||
Electrical Features | |||||
Supply Voltage | 3.3 V | ||||
Power Consumption | 0.15 W | ||||
Ripple Wave | 100mV (P-P) | ||||
Environment Conditions | |||||
Operating Temperature | -40°C ~ 85°C | ||||
Storage Temperature | -55°C ~ 105°C | ||||
Vibration Resistance | 20-2000Hz, 6.06g | ||||
Shock Resistance | 1000g, 0.5ms | ||||
Physical Parameter | |||||
Size | 47 × 44 × 14 mm | ||||
Weight | 50grams | ||||
Connector | 2 × 12 pins | ||||
NoA1:F60te: ①:The range of Gyroscopes and Accelerometers can be configured in our factory. ②:The bias value is calculated based on the whole temperature change period, the temperature changing rate<=2°C/minute, temperature range:-40~+85°C; ③:(before vibration average value +after vibration average value) /2-during vibration average value, the vibration conditions are 6.06g, 20~2000Hz ④: The Z-axis can be equipped with an accelerometer with a range of ±50g or ±100g in our factory. ⑤: The baud rate and output rate can be configured in our factory. |
IMU588 Inertial Measurement Unit is a high performance 6DoF MEMS-based inertial sensors, which has been widely used in the following fields:
– Rain-Seeding Rocket
– Target Drones
– Unmanned Surface Vessel
– Unmanned Aircraft
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