Shenzhen Fire Power Control Technology Co., LTD
                                                                                                           
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Adis16488 Replacement Sensors lmu Accelerometer Gyro

Price Negotiable
Price: negotiable
MOQ: 1
Delivery Time: 1 week for sample
Brand: Firepower
Product Description
ADIS16488 Replacement Sensors - IMU Accelerometer Gyro
The ADIS16488C multi-degree-of-freedom inertial measurement unit is a complete inertial system featuring a built-in three-axis gyroscope, three-axis accelerometer, three-axis magnetometer, and pressure sensor. This advanced system measures critical carrier parameters including three-axis angle rate, acceleration, three-axis magnetic field, and air pressure. All output data is provided after comprehensive error compensation (including temperature compensation, installation misalignment angle compensation, and nonlinear compensation) through the SPI communication protocol.
Technical Specifications
Gyroscope Parameters
Parameter Test Conditions Minimum Typical Maximum Unit
Dynamic Measuring Range 500 2000 °/s
Zero Bias Stability Allan variance, Z-axis 0.8 °/h
Zero Bias Stability Allan variance, X and Y axis 1.6 °/h
Zero Bias Stability 10 s average (-40℃ ~ +70℃, constant temperature), Z-axis 3 °/h
Zero Bias Stability 10 s average (-40℃ ~ +70℃, constant temperature), X-axis and Y-axis 6 °/h
Zero Bias Zero-bias range, Z-axis ±0.07 °/s
Zero Bias Zero-bias range, X-axis and Y-axis ±0.2 °/s
Zero Bias Change Full temperature range, Z-axis ±0.02 °/s
Zero Bias Change Over temperature, X and Y axis ±0.06 °/s
Successive Start Repeatability Z-axis 0.002
Successive Start Repeatability X-axis and Y-axis 0.006
Day-by-day Start Repeatability Z-axis 0.003 °/s
Day-by-day Start Repeatability X-axis and Y-axis 0.009 °/s
Effect of Linear Acceleration on Bias 0.002 °/s/g
Influence of Vibration on Zero Bias Change before and after vibration 0.002 °/s/g
Influence of Vibration on Zero Bias Change before and during vibration 0.002 °/s/g
Scale Factor Accuracy Z-axis 0.3 %
Scale Factor Accuracy X and Y axis 0.6 %
Scale Factor Nonlinearity Z-axis 0.01 %FS
Scale Factor Nonlinearity X and Y axis 0.02 %FS
Angular Random Walk 0.15 °/√hr
Noise Density 0.001 °/s/√Hz
Resolution 3.052×10⁻⁷ °/s/LSB
Bandwidth 200 Hz
Accelerometer Parameters
Parameter Test Conditions Minimum Typical Maximum Unit
Dynamic Measuring Range 16 200 g
Zero Bias Stability Allan variance 0.06 mg
Zero Bias Stability 10 s average (-40℃ ~ +70℃, constant temperature) 0.4 mg
Zero Bias Range 2 mg
Zero Bias Change Full temperature range, peak-to-peak value 4 mg
Successive Start Repeatability 0.5 mg
Day-by-day Start Repeatability 0.8 mg
Zero-bias Temperature Coefficient 0.05 0.1 mg/℃
Dimensions
ADIS16488 IMU Accelerometer Gyro dimensional diagram and specifications
Packaging & Shipping
ADIS16488 IMU packaging overview and shipping materials ADIS16488 IMU secure packaging details ADIS16488 IMU shipping container and protection

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Company Shenzhen Fire Power Control Technology Co., LTD
Location 429, Building A10, Fuhai Information Port, Xinhe Community, Fuhai Street, Shenzhen, Guangdong, China
Contact Person Caine

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