Specifications
Random Walk :
0.15°/√h
Zero-bias instability :
0.3º/h
Zero Bias Repatability :
≤5°/h
Bandwidth :
250Hz
Scale Factor Nonlinear :
≤100ppm
Scale factor repeatability :
≤100ppm
Brand Name :
Firepower
Model Number :
16488HA
Certification :
Military standard
Place of Origin :
China
MOQ :
1
Price :
negotiable
Payment Terms :
T/T
Supply Ability :
50/month
Delivery Time :
20 days for sample
Packaging Details :
sponge+ box
Description
9-Axis MEMS IMU 0.3°/h Gyro Bias for Drone Flight Control & GNSS-Denied Navigation
The ADIS16488HA is a compact, lightweight MEMS IMU featuring a three-axis gyroscope and accelerometer, with measurement ranges of ±450°/s angular rate and ±20 g acceleration. With exceptional zero-bias instability of 0.3°/h for the gyro and 0.25 mg for the accelerometer, this unit delivers minimal random walk and 100-500 ppm scale factor linearity. Advanced temperature, misalignment, and nonlinear error compensation ensure reliable performance across an operating range of -45°C to 85°C. Featuring SPI communication at 8-15 MHz, 1.5 W power consumption, 250 Hz bandwidth, and 0.1% cross-coupling, this IMU is ideal for UAVs, robotics, industrial automation, mobile mapping, and precision navigation systems.
Technical Specifications
Parameter Test Conditions Min Value Typical Value Max Value Unit
Gyroscope
Dynamic measuring range


±450 º/s
Zero-bias instability Allan variance, better than
0.3
º/h
Zero bias stability 10s smooth, RMS, better than
3
º/h
Zero bias in full temperature range -40℃ ~ 85℃, 10 s smooth, rms
20
º/h
Random walk
0.15
º/√h
Zero-bias repeatability
5
º/h
Scale factor repeatability
100
ppm
Scale factor nonlinearity
100
ppm
Bandwidth (-3dB)

250
Hz
Cross coupling

0.1
%
Resolution

2
º/h
Acceleration sensitivity

2
°/h/g
Accelerometer
Dynamic measuring range


±20 g
Zero bias stability Allan variance
0.07
mg
Zero bias in full temperature range -40℃ ~ 85℃, 10 s smooth, rms
3
mg
Zero bias stability 10s smooth, RMS, better than
0.25
mg
Random walk
0.029
m/s/√h
Zero-bias repeatability
0.5
mg
Scale factor repeatability
500
ppm
Scale factor nonlinearity FS=20g
500
ppm
Bandwidth (-3dB)

250
Hz
Cross coupling

0.1
%
Communication Interface
1-way SPI Enter the clock frequency
8 15 MHz
Electrical Characteristics
Voltage Direct current
3.3
V
Power consumption

1.5 1.5 W
Ripple P-P
48±2 100 mV
Use Environment
Operating temperature
-45
85
Storage temperature
-55
85
Product Diagrams
Outline Drawing
9-Axis MEMS IMU 0.3°/h Gyro Bias for Drone Flight Control & GNSS-Denied Navigation
Connector Diagram
9-Axis MEMS IMU 0.3°/h Gyro Bias for Drone Flight Control & GNSS-Denied Navigation
Axial Direction Diagram
9-Axis MEMS IMU 0.3°/h Gyro Bias for Drone Flight Control & GNSS-Denied Navigation
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9-Axis MEMS IMU 0.3°/h Gyro Bias for Drone Flight Control & GNSS-Denied Navigation

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Random Walk :
0.15°/√h
Zero-bias instability :
0.3º/h
Zero Bias Repatability :
≤5°/h
Bandwidth :
250Hz
Scale Factor Nonlinear :
≤100ppm
Scale factor repeatability :
≤100ppm
Contact Supplier
9-Axis MEMS IMU 0.3°/h Gyro Bias for Drone Flight Control & GNSS-Denied Navigation
9-Axis MEMS IMU 0.3°/h Gyro Bias for Drone Flight Control & GNSS-Denied Navigation
9-Axis MEMS IMU 0.3°/h Gyro Bias for Drone Flight Control & GNSS-Denied Navigation
9-Axis MEMS IMU 0.3°/h Gyro Bias for Drone Flight Control & GNSS-Denied Navigation
9-Axis MEMS IMU 0.3°/h Gyro Bias for Drone Flight Control & GNSS-Denied Navigation
9-Axis MEMS IMU 0.3°/h Gyro Bias for Drone Flight Control & GNSS-Denied Navigation

Shenzhen Fire Power Control Technology Co., LTD

Verified Supplier
5 Years
guangdong, shenzhen
Since 2001
Business Type :
Manufacturer, Exporter, Trading Company, Seller
Total Annual :
10000000-15000000
Employee Number :
60~100
Certification Level :
Verified Supplier
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