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IMU5000 Robust Precision 10DoF 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) bias instability, and it can output precise 3 axis outputs of angular rate, 3 axis acceleration data, 3 axis magnetometer data, and barometer data, etc.
IMU5000 IMU sensor is with a rugged housing featuring excellent protection against environmental influences. It is designed for easy integration and seamless interfacing with other equipment. And it enjoys excellent measurement performance, small size, light weight, and high reliability and robustness, and it has been widely applied in tactical applications such as unmanned aerial vehicles, unmanned surface vessel, gimbal stabilization, platform stabilization, etc.
Parameter | Test Condition | Min. | Typical | Max. | Unit |
Gyroscopes | |||||
Range① | ±4000 | °/s | |||
Bias Instability | Allan variance | 1 | °/h | ||
10s average(-40~+85°C, fixed temp.) | 6 | 10 | 15 | °/h | |
Bias Repeatability | 10 | °/h | |||
Random Walk | 0.1 | °/√h | |||
Bais | Bias change at full temp. range② | ±0.2 | °/s | ||
Bias change in vibration conditions③ | 20 | °/h | |||
Non-linearity | 500 | ppm | |||
Bandwidth | 200 | Hz | |||
Accelerometers(X/Y) | |||||
Range① | ±30 | g | |||
Bias Instability | Allan variance | 50 | ug | ||
10s average(-40~+85°C, fixed temp.) | 100 | ug | |||
Bias Repeatability | 100 | ug | |||
Random Walk | 0.01 | m/s/√h | |||
Non-linearity | 100 | ppm | |||
Bandwidth | 200 | Hz | |||
Accelerometers(Z) | |||||
Range① | ±150 | g | |||
Bias Instability | Allan variance | 120 | 150 | ug | |
10s average(-40~+85°C, fixed temp.) | 500 | ug | |||
Bias Repetition | 500 | ug | |||
Random Walk | 0.05 | m/s/√h | |||
Non-linearity | 1000 | 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 | |||
Interface④(RS422) | |||||
Baud Rate | 460800 | bps | |||
Output Rate | 500 | Hz | |||
Reliability | |||||
MTBF | 20000 h | ||||
Continuous Working Time | 120 h | ||||
Electrical Features | |||||
Supply Voltage | 6 ~ 30 V | ||||
Power Consumption | < 0.5W | ||||
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 | 46×46×24 mm | ||||
Weight | 100grams | ||||
Interface Model | 15pins J30J | ||||
Note: 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 baud rate and output rate can be configured in our factory. |
– Unmanned Aerial Vehicles
– Unmanned Surface Vessel
– Gimbal Stabilization
– Platform Stabilization
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