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High-Stability IMU for Advanced Driver Assistance Systems ADAS

Name: High-Stability IMU for Advanced Driver Assistance Systems ADAS
Brand: Shenzhen Fire Power Control Technology Co., LTD
SKU: IMU115
Price: 3,003.00 USD
Availability: InStock

Brand Name:	Firepower
Model Number:	IMU115
MOQ:	1
Price:	Negotiable
Payment Terms:	T/T
Supply Ability:	200/MONTH

Detail Information

Product Description

Detail Information

Place of Origin:

CHINA

Range:

≥250 °/s

Bias Stability:

≤3°/h

Acc Bias Stability:

0.12 Mg

Acc Range:

4/16 G

Overall Dimension:

22.4mm X 22.4mm X 9.5mm

Random Vibration:

3g，20~2000Hz

Packaging Details:

Sponge+ box

Supply Ability:

200/MONTH

Highlight:

UAV integrated optic gyroscope

sagnac effect integrated optic gyroscope

Product Description

High-Stability IMU for Advanced Driver Assistance Systems (ADAS)

The IMU115 MEMS inertial unit integrates 3-axis gyro and accelerometer, providing precise angular velocity and linear acceleration measurements. Features include ±250°/s gyro, ±4g accelerometer, and built-in compensation for temperature and installation errors. Compact and reliable, ideal for UAV navigation, autonomous driving, mapping, and stabilization.

Product Features

Three-axis digital gyroscope:
- ±250º/s dynamic measuring range (500°/s optional)
- Zero bias stability: 10°/h (GJB, 10s, typical value), 6.0°/h (ALLAN, typical value)
Triaxial digital accelerometer:
- ±4g dynamic measurement range (configurable 16g)
- Zero-bias stability: 0.12 mg (GJB, 10s), 0.065 mg (ALLAN)
High reliability: MTBF > 20,000 hours
Guaranteed accuracy within full temperature range (-40℃ to 80℃) with built-in high-performance temperature calibration and compensation algorithm
Suitable for working under strong vibration conditions
Interface: 1-way UART

Field of Application

Intelligent driving
Communication in motion
Mapping
Stabilize the platform

Product Indicators

Parameter	Test conditions	Typical value	Maximum value	Unit
Gyroscope	Dynamic measuring range	250	500	º/s
	Zero bias stability (Allan variance)	3.0		º/h
	Zero bias stability (10s average, -40℃ to +80℃, constant temperature)	6.0		º/h
	Zero bias range	±0.2		º/s
	Zero bias variation over full temperature range	±0.3		º/s
	Scale factor accuracy	0.2		%
Accelerometer	Dynamic measuring range		4 \| 16	g
	Zero bias stability (Allan variance)	0.065		mg
	Zero bias stability (10s average, -40℃ to +80℃, constant temperature)	0.12		mg
	Zero bias range	±3		mg
	Zero bias change in full temperature range, peak-to-peak value	±6		mg
	Scale factor accuracy	0.3		%
Note: Calculate the zero bias of the whole temperature change process, the temperature change rate is ≤1℃/min, and the temperature range is -40℃ to +80℃

Structure Outline

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

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High-Stability IMU for Advanced Driver Assistance Systems ADAS

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