Shenzhen Fire Power Control Technology Co., LTD

Manufacturer from China
Verified Supplier
4 Years
Home / Products / IMU Accelerometer Gyro /

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

Contact Now
Shenzhen Fire Power Control Technology Co., LTD
Visit Website
City:shenzhen
Province/State:guangdong
Country/Region:china
Contact Person:Caine
Contact Now

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

Ask Latest Price
Video Channel
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
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
more
Contact Now

Add to Cart

Find Similar Videos
View Product Description

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

Inquiry Cart 0