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Adis16488 Inertial Sensor IMU for UAV and Drone Stabilization System with Magnetometer

Adis16488 Inertial Sensor IMU for UAV and Drone Stabilization System with Magnetometer

Brand Name: FIREPOWER
Model Number: 16488c
MOQ: 1
Payment Terms: L/C,T/T
Supply Ability: 500/month
Detail Information
Place of Origin:
China
Scale Factor Nonlinear:
≤200ppm
Zero-bias Instability:
5º/h
Zero Bias Repeatability:
20°/h
Output:
RS422
Bandwidth (-3dB:
330 Hz
Weight:
48±2g
Packaging Details:
sponge +carton
Supply Ability:
500/month
Highlight:

Adis16488 IMU with magnetometer

,

UAV stabilization IMU sensor

,

drone gyro accelerometer system

Product Description
ADIS16488 Inertial Sensor IMU for UAV and Drone Stabilization System with Magnetometer

The ADIS16488C multi-degree-of-freedom inertial measurement unit is a complete inertial system featuring a three-axis gyroscope, three-axis accelerometer, three-axis magnetometer, and pressure sensor. This advanced IMU measures three-axis angular rate, acceleration, three-axis magnetic field, air pressure, and other critical parameters. The unit outputs error-compensated data (including temperature compensation, installation misalignment angle compensation, and nonlinear compensation) through SPI or UART communication protocols.

Technical Specifications
Parameter Test Conditions Minimum Value Typical Value Maximum Value Unit
Gyroscope
Dynamic Measuring Range Configurable

±450 º/s
Zero-bias Instability Allan variance, better than
5
º/h
Zero Bias Stability 10s smooth, RMS, better than
10
º/h
Zero Bias in Full Temperature Range -40℃ ~ 85℃, 10s smooth, RMS
60
º/h
Random Walk
0.26
º/√h
Zero-bias Repeatability
20
º/h
Zero-bias Acceleration Sensitive

20
º/h/g
Scale Factor Repeatability
200
ppm
Scale Factor Nonlinearity FS=450º/s
200
ppm
Bandwidth (-3dB)

330
Hz
Cross Coupling

0.2
%
Accelerometer
Dynamic Measuring Range Configurable

±20 g
Zero Bias Stability Allan variance
0.07
mg
Zero Bias in Full Temperature Range -40℃ ~ 85℃, 10s smooth, RMS
3
mg
Random Walk
0.029
m/s/√h
Zero-bias Repeatability
0.5
mg
Zero Bias Stability 10s smooth, RMS, better than
0.25
mg
Scale Factor Repeatability
500
ppm
Scale Factor Nonlinearity FS=10g
500
ppm
Bandwidth (-3dB)

250
Hz
Cross Coupling

0.2
%
Magnetometer
Dynamic Measuring Range


±2.5 gauss
Sensitivity

0.1
mgauss/LSB
Barometer
Pressure Range
300
1100 mbar
Sensitivity

6.1 × 10⁻⁷
mbar/LSB
Electrical Characteristics
Voltage Direct current
3.3±0.15
V
Power Consumption

0.5
W
Ripple P-P
100
mV
Weight

48±2
g
Environmental Specifications
Operating Temperature Scalable -45
85
Storage Temperature
-55
85
Outline Drawing
Adis16488 Inertial Sensor IMU for UAV and Drone Stabilization System with Magnetometer 0