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10-Axis Inertial Measurement Unit for UAV Attitude and Altitude Control Adis16488

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10-Axis Inertial Measurement Unit for UAV Attitude and Altitude Control Adis16488

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Brand Name :Firepower
Model Number :16488C
Place of Origin :CHINA
MOQ :1
Payment Terms :T/T,L/C
Supply Ability :1000pcs
Delivery Time :1 week
Packaging Details :wooden box
Acc Range :±20g
Gyro range :±450º/s
Zero-bias instability :5º/h
Zero-bias acceleration sensitiv :20º/h/g
Bandwidth :330 Hz
Voltage :3.3±0.15V
Weight :48g
Magnetometer Sensitivity :0.1mgauss/LSB
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Product Description


16488C Multi-Degree-of-Freedom Inertial Measurement Unit (IMU) is a high-performance, fully integrated inertial system equivalent to the ADIS16488. It combines a three-axis gyroscope, three-axis accelerometer, three-axis magnetometer, and barometric pressure sensor in a compact module.

This IMU provides accurate measurements of angular rate, linear acceleration, magnetic field, and air pressure for dynamic platforms such as autonomous vehicles, UAVs, robotics, and navigation systems.

Featuring built-in error compensation (including temperature drift, misalignment, and nonlinear correction), the 16488C ensures exceptional stability and precision in harsh environments. Data is output via SPI or UART interface under standard communication protocols, enabling easy system integration and real-time motion sensing.


Technical Parameters

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 ℃, 10 s smooth,

rms

60

º/h

Random walk

1σ

0.26

º/√h

Zero-bias repeatability

1σ

20

º/h

Zero-bias acceleration sensitive

20

º/h/g

Scale factor repeatability

1σ

200

Ppm

Scale factor nonlinearity

FS=450 º/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 ℃, 10 s 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

1σ

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

Characteristic

Voltage

Direct current

3.3±0.15

V

Power consumption

0.5

W

Ripple

P-P

100

mV

Weight

48±2

g

Use

Environment

Operating temperature

Scalable

-45

85

Storage temperature

-55

85

outline drawing


10-Axis Inertial Measurement Unit for UAV Attitude and Altitude Control Adis16488

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