Light Weight Imu with Large Dynamic Measurement Range
Product Details
| Customization: | Available |
|---|---|
| Type: | Inertial Measurement Unit |
| Output Signal Type: | Digital Output |
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Address
Floor 18th, Ruihua Builiding, No. 315, Zhongshan South Road, Qinhuai District, Nanjing, ...
International Commercial Terms(Incoterms)
FOB, EXW, CFR, CIF, CIP
Terms of Payment
LC, T/T, Western Union, Money Gram
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Basic Info.
- Model NO.
- IMU5000
- Measuring Shaft Quantities
- 10
- Accuracy Grade
- 1degree/H
- IP Rating
- IP67
- Certification
- ISO
- Customized
- Non-Customized
- Range
- Gyro: +-4000deg/S, Acc: +-30g (X,Y),+-150g (Z)
- Bias Instability
- Gyro: 1deg/H, Acc: 30ug (X,Y), 120ug (Z) (Allan)
- Working Temperature
- -40~+85degc
- Interface
- Uart
- Transport Package
- Carton
- Specification
- 46*46*24mm
- Trademark
- SkyMEMS
- Origin
- China
- HS Code
- 9014100000
- Production Capacity
- 2000/Month
Product Description
IMU5000
Main Features
- Robust Precision 10DoF Inertial Measurement Unit
- Range (Typical): Gyro ±4000°/s,
Acc ±30g (X,Y), ±150g (Z)
- Bias Instability: Gyro: 1°/h,
Acc 30μg (X,Y: ±30g), 120μg (Z: ±150g) (Allan)
- Full Temperature Range Accuracy Assured
- High Bandwidth (Typical): 200Hz
- Working Temperature: -40~+85°C
Brief Introduction
IMU5000 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.
Technical Specifications
Typical Applications
- Unmanned Aerial Vehicles
- Unmanned Surface Vessel
- Gimbal Stabilization
- Platform Stabilization
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Robust Precision 10DoF Inertial Measurement Unit
Main Features
- Robust Precision 10DoF Inertial Measurement Unit
- Range (Typical): Gyro ±4000°/s,
Acc ±30g (X,Y), ±150g (Z)
- Bias Instability: Gyro: 1°/h,
Acc 30μg (X,Y: ±30g), 120μg (Z: ±150g) (Allan)
- Full Temperature Range Accuracy Assured
- High Bandwidth (Typical): 200Hz
- Working Temperature: -40~+85°C
Brief Introduction
IMU5000 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.
Technical Specifications
| 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 | |||
| Radom Walk | 0.1 | º/√h | |||
| Bais | Bias change at full temp. range2 | ±0.2 | °/s | ||
| Bias change in vibration conditions3 | 20 | °/h | |||
| Scale Factor Nonlinearity | 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 Repeatability | 500 | ug | |||
| Random Walk | 0.05 | m/s/√h | |||
| Non-linearity | 1000 | ppm | |||
| Bandwidth | 200 | Hz | |||
| Magnetometer | |||||
| 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 | 20000h | ||||
| Continuous Working Time | 120h | ||||
| Electronic Features | |||||
| Supply Voltage | 6 ~ 30 V | ||||
| Power Consumption | <0.5 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 Characteristics | |||||
| Size | 46 × 46 × 24 mm | ||||
| Weight | 100grams | ||||
| Interface Model | 15pins J30J | ||||
| 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. |
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Typical Applications
- Unmanned Aerial Vehicles
- Unmanned Surface Vessel
- Gimbal Stabilization
- Platform Stabilization
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