Customization: | Available |
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Type: | Inertial Measurement Unit |
Output Signal Type: | Digital Output |
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IMU388 is a high performance tactical grade MEMS Inertial Measurement Unit, which enjoys high accuracy: MEMS gyroscope is 0.6°/h bias instability (Allan) and MEMS accelerometer is 30µg bias instability (Allan), and its MEMS gyroscope range can be optional in ±250°/s~ ±4000°/s, the accelerometer range is ±40g, and it can output precise 3-axis outputs of angular rate and 3-axis acceleration data.
IMU388 adopts latest MEMS technology and advanced MEMS components, and it has been produced in bulk, which reduces the cost deeply. IMU388 can output precise measurement data in harsh environment, and it has been widely applied in unmanned aircraft, unmanned surface vessel, platform stabilization, industrial robotics, etc., and IMU388 is easily integrated into the variety of architectures that these applications present. The extremely small size, light weight, and low power make the IMU388 ideal for most applications.
Technical SpecificationsParameter | Test Condition | Min | Typical | Max | Unit |
Gyroscopes | |||||
Range1 | ±500 | °/s | |||
Bias Instability | Allan variance | 0.6 | °/h | ||
10s average (-40~+85°C, fixed temp.) | 2 | °/h | |||
Bias Repeatability | 1.8 | °/h | |||
Radom Walk | 0.1 | º/√h | |||
Bais | Bias change at full temp. range2 | ±0.04 | °/s | ||
Bias change in vibration conditions3 | 6 | °/h | |||
Scale Factor Nonlinearity | 100 | ppm | |||
Bandwidth | 200 | Hz | |||
Accelerometers | |||||
Range1 | ±40 | 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 | |||
Interface4(RS422) | |||||
Baud Rate | 115200 | 230400 | 921600 | bps | |
Output Rate | 250 | 500 | 2000 | Hz | |
Reliability | |||||
MTBF | 20000h | ||||
Continuous Working Time | 120h | ||||
Electronic Features | |||||
Supply Voltage | 3.6 ~ 36 V | ||||
Power Consumption | < 0.2 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 | 33.5 × 25.5 × 15 mm | ||||
Weight | 30grams | ||||
Interface Model | 9pins J63A | ||||
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. |
Why Selecting IMU388M Inertial Measurement Unit
IMU388M Inertial Measurement Unit is designed and produced by SkyMEMS, it enjoys high performance and accuracy, extra large range, and high reliability with competitive price. It is a tactical inertial measurement unit sensor, which has the main following advantages:
We are continuously focusing on MEMS measurement & control technologies. IMU388 has been widely used in tactical UAS Navigation & Control, Seeker, Platform Stabilization, etc. and now more than 200 customers are using our tactical IMU around the world.
5. World-class Production Line, Fast DeliveryServing customers with heart is the principle of SkyMEMS, Customer demand is the fundamental driving force of our development.
We treat our customers with heart, customers' satisfaction is the direction and target of SkyMEMS. Through continuously technology innovation and service upgrading, we will realize win-win cooperation with customers.