9-Axis MEMS IMU 0.3°/h Gyro Bias for Drone Flight Control & GNSS-Denied Navigation

Brand Name:Firepower
Certification:Military standard
Model Number:16488HA
Minimum Order Quantity:1
Delivery Time:20 days for sample
Payment Terms:T/T
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Location: Shenzhen Guangdong China
Address: 429, Building A10, Fuhai Information Port, Xinhe Community, Fuhai Street, Shenzhen, Guangdong, China
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Product Details

ADIS16488HA is a compact, lightweight MEMS IMU with three-axis gyroscope and accelerometer, measuring ±450°/s angular rate and ±20 g acceleration. Zero-bias instability is 0.3°/h for the gyro and 0.25 mg for the accelerometer, with minimal random walk and 100–500 ppm scale factor linearity. Temperature, misalignment, and nonlinear error compensation ensure reliable performance from -45~85 °C. SPI communication at 8–15 MHz, 1.5 W power consumption, 250 Hz bandwidth, and 0.1 % cross-coupling make it ideal for UAVs, robotics, industrial automation, mobile mapping, and precision navigaion systems.



Technical Parameters

Parameter

Test conditions

Minimum value

Typical value

Maximum 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

outline drawing

9-Axis MEMS IMU 0.3°/h Gyro Bias for Drone Flight Control & GNSS-Denied Navigation

Connector

9-Axis MEMS IMU 0.3°/h Gyro Bias for Drone Flight Control & GNSS-Denied Navigation


axial direction

9-Axis MEMS IMU 0.3°/h Gyro Bias for Drone Flight Control & GNSS-Denied Navigation

China 9-Axis MEMS IMU 0.3°/h Gyro Bias for Drone Flight Control & GNSS-Denied Navigation supplier

9-Axis MEMS IMU 0.3°/h Gyro Bias for Drone Flight Control & GNSS-Denied Navigation

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