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IMU Accelerometer Gyro

6 Axis IMU Accelerometer Gyro Inertial Measure Unit Low Cost

Name: 6 Axis IMU Accelerometer Gyro Inertial Measure Unit Low Cost
Brand: Shenzhen Fire Power Control Technology Co., LTD
SKU: 16488
Price: 3,003.00 USD
Availability: InStock

Brand Name:	Firepower
Model Number:	16488
MOQ:	1
Payment Terms:	T/T
Supply Ability:	500/month

Detail Information

Product Description

Detail Information

Place of Origin:

CHINA

Certification:

CE ROHS

Product Name:

Inertial Gyro Accelerometer

Gyro Range:

±500º/s

Gyro Bias Instability:

<2º/h

Bias In Full Temperature Range:

<5º/h

Scale Factor Is Nonlinear:

<500ppm

Accelerometer Bias:

1mg

Bias Repeatability:

0.5mg

Random Walk:

0.029 M/s/√h

Packaging Details:

sponge/box

Supply Ability:

500/month

Highlight:

6 Axis IMU Accelerometer Gyro

IMU Accelerometer Gyro Inertial Measure Unit

6 axis IMU High Performance

Product Description

6 Axis IMU Accelerometer Gyro Inertial Measure Unit

Key Features

High-precision MEMS IMU designed to replace ADIS16488
Superior performance to ADIS16488 with identical form factor
Configurable gyro range up to ±500º/s
Low bias instability: <2º/h (gyro), 0.5mg (accelerometer)
Multiple communication interfaces: SPI, UART, CAN
Professional customization services available

Technical Specifications

Attribute	Value
Gyro range	±500º/s
Gyro bias instability	<2º/h
Bias in full temperature range	<5º/h
Scale factor nonlinearity	<500ppm
Accelerometer bias	1mg
Bias repeatability	0.5mg
Random walk	0.029 m/s/√h

Product Description

The 16488-C is a domestic MEMS IMU designed as a high-performance replacement for ADIS16488. This unit offers improved precision while maintaining identical dimensions, appearance, and communication protocols for seamless integration. Multiple versions are available to suit specific application requirements.

Detailed Performance Comparison

Parameter	Conditions	16488-C	ADIS16488	Unit
Gyro Specifications
Dynamic measuring range	Configurable	±450	±480	º/s
Bias instability	Allan	3.5	5.1	º/h
Bias stability	1s,rms	30	/	º/h
Bias in full temperature range	-40℃~85℃,10s,rms	0.02	/	º/s
Random walk	1б	0.25	0.26	º/√h
Bias repeatability	1б	35	/	º/h
Output noise	No filtering,rms	0.09	0.135	º/s
Scale factor repeatability	1б	0.02	1.0	%
Scale factor Temperature coefficient	-40℃~85℃, 1б	5	±35	ppm/°C
The scale factor is nonlinear	FS=450º/s	0.008	0.01	%FS
Bandwidth(-3dB)		330	330	Hz
Accelerometer Specifications
Dynamic measuring range	Configurable (Max ±40)	±20	±18	g
Bias stability	Allan error	0.005	/	mg
Bias in full temperature range	-40℃~85℃,10s,rms	0.5	16	mg
Random walk	1б	0.01	0.029	m/s/√h
Bias instability	1б	0.16	/	mg
Output noise	No filterin,rms	1	/	mg
Scale factor repeatability	1б	0.01	0.5	%
Scale factor is nonlinear	FS=10g	0.002	0.1	%FS
Bandwidth(-3dB)		330	330	Hz
Cross coupling		0.18	/	%

Tags:

Accelerometer Gyro Sensor

IMU Accelerometer Gyro

Quartz Flexure Accelerometer

Fiber Optic Gyro

Inertial Navigation System

3 Axis Turntable

Gyro North Finder

Accelerometer Test Equipment

Magnetometer Sensor

1 Axis Turntable

2 Axis Turntable

Accelerometer Gyro Sensor

IMU Accelerometer Gyro

Quartz Flexure Accelerometer

Fiber Optic Gyro

Inertial Navigation System

3 Axis Turntable

Gyro North Finder

Accelerometer Test Equipment

Magnetometer Sensor

1 Axis Turntable

2 Axis Turntable

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6 Axis IMU Accelerometer Gyro Inertial Measure Unit Low Cost

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