High Performance Tactical Grade Mems Inertial Measurement Unit
Product Details
| Customization: | Available |
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| Type: | Inertial Measurement Unit |
| Output Signal Type: | Digital Output |
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Floor 18th, Ruihua Builiding, No. 315, Zhongshan South Road, Qinhuai District, Nanjing, ...
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Basic Info.
- Model NO.
- IMU288
- Measuring Shaft Quantities
- 6
- Accuracy Grade
- Bias Instability: Gyro 1°/H, Acc 0.03mg (Allen)
- IP Rating
- IP67
- Certification
- ISO
- Customized
- Non-Customized
- Vibration Resistance
- 20-2000Hz, 6.06g
- Working Temperature
- -40°C ~ 85°C
- Shock Resistance
- Half Sine, 0.5ms, 1000g
- Weight
- 15grams
- Interface
- Uart
- Transport Package
- Carton
- Specification
- 25*25*10.5mm
- Trademark
- SkyMEMS
- Origin
- China
- HS Code
- 9014100000
- Production Capacity
- 2000/Month
Packaging & Delivery
- Package Size
- 15.00cm * 15.00cm * 5.00cm
- Package Gross Weight
- 0.090kg
Product Description
IMU288 Miniature 6DoF MEMS IMU
Main Features
-Dynamic Range: Gyro ±450°/s, Acc ±16g
-Bias Instability: Gyro 1°/h, Acc 30µg
-Full Temperature Range Accuracy Assured: Built-in High Performance Temperature Calibration and Compensation Algorithm
-UART Interface, Output rate up to 2000Hz
-Compact and Light weight: 25 × 25 × 10.5mm, 15 grams
-Working Temperature: -40~+85°C
Brief Introduction
IMU288 Inertial Measurement Unit is a high performance tactical grade MEMS Inertial Measurement Unit, it is composed of 1°/h (Allan) bias stability MEMS gyroscope and 30µg (Allan) bias stability MEMS accelerometer, which can output precise 3-axis angular rates, 3 axis acceleration data and temperature data.
IMU288 Inertial Measurement Unit adopts latest MEMS technology and advanced MEMS components, which reduces the cost deeply. The system enjoys small size and light weight, and it has been widely applied in unmanned aircraft, autonomous vehicles, platform stabilization, unmanned robotics, etc.
Technical Specifications
| Parameter | Test Condition | Min. Typical Max. | Unit |
| Gyroscopes | |||
| Range1 | ±450 | °/s | |
| Bias Instability | Allan variance | 1 | °/h |
| 10s average(-40~+85°C, fixed temp.) | 2 3 4 | °/h | |
| Bias Repeatability | 2 | °/h | |
| Random Walk | 0.1 | °/√h | |
| Bais | Bias change at full temp. range2 | ±0.04 | °/s |
| Bias change in vibration conditions3 | 6 | °/h | |
| Non-linearity | 100 | ppm | |
| Bandwidth | 200 | Hz | |
| Accelerometers | |||
| Range1 | ±16 | g | |
| Bias Instability | Allan variance | 0.03 0.045 | mg |
| 10s average(-40~+85°C, fixed temp.) | 0.06 | mg | |
| Bias Repeatability | 0.06 | mg | |
| Random Walk | 0.01 | m/s/√h | |
| Non-linearity | 100 | ppm | |
| Bandwidth | 200 | Hz | |
| Interface4 (UART) | |||
| Baud Rate | 921600 | bps | |
| Output Rate | 2000 | Hz | |
| Reliability | |||
| MTBF | 20000 h | ||
| Continuous Working Time | 120h | ||
| Electrical Features | |||
| Supply Voltage | 3.3 V | ||
| Power Consumption | 1.5 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 | half sine, 0.5ms, 1000g | ||
| Physical Parameter | |||
| Size | 25 × 25 × 10.5 mm³ | ||
| Weight | 15grams | ||
| Connector | molex connector, model: 5015680607 | ||
| 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. | |||
Typical Application
- Robotics
- Unmanned Aircraft
- Platform Stabilization
- Autonomous Vehicle
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