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

Name: 9-Axis MEMS IMU 0.3°/h Gyro Bias for Drone Flight Control & GNSS-Denied Navigation
Brand: Shenzhen Fire Power Control Technology Co., LTD
SKU: 16488HA
Price: 3,003.00 USD
Availability: InStock

Brand Name:	Firepower
Model Number:	16488HA
MOQ:	1
Price:	negotiable
Payment Terms:	T/T
Supply Ability:	50/month

Detail Information

Product Description

Detail Information

Place of Origin:

China

Certification:

Military standard

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

Packaging Details:

sponge+ box

Supply Ability:

50/month

Highlight:

high precision fiber optic gyro

100ppm fiber optic gyro

Product 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	1σ		0.15		º/√h
Zero-bias repeatability	1σ		5		º/h
Scale factor repeatability	1σ		100		ppm
Scale factor nonlinearity	1σ		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	1σ		0.029		m/s/√h
Zero-bias repeatability	1σ		0.5		mg
Scale factor repeatability	1σ		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

Connector Diagram

Axial Direction Diagram

Tags:

Accelerometer Gyro Sensor

IMU Accelerometer Gyro

Quartz Flexure Accelerometer

Fiber Optic Gyro

Inertial Navigation System

Gyro North Finder

Magnetometer Sensor

Accelerometer Gyro Sensor

IMU Accelerometer Gyro

Quartz Flexure Accelerometer

Fiber Optic Gyro

Inertial Navigation System

Gyro North Finder

Magnetometer Sensor

products details

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

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