INT-M-IMU01 Customized Strapdown Gyroscope IMU | High-Precision Inertial Measurement System Units Zero bias stability at variable temperature (100s) ：0.5°/h

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INT-M-IMU01 Customized Strapdown Gyroscope IMU | High-Precision Inertial Measurement System Units Zero bias stability at variable temperature (100s) ：0.5°/hINT-M-IMU01 Customized Strapdown Gyroscope IMU | High-Precision Inertial Measurement System Units INT-M-IMU01 Customized Strapdown Gyroscope IMUsINT-M-IMU01 Strapdown Gyroscope IMU | High-Precision Inertial Measurement System Units Zero bias stability at variable temperature (100s) ：0.5°/h

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INT-M-IMU01 Customized Strapdown Gyroscope IMU | High-Precision Inertial Measurement System Units Zero bias stability at variable temperature (100s) ：0.5°/h.

Detail Information

Place of Origin

China

Brand Name INT

Model Number

INT-M-IMU01

Gyro\Bias Stability (10s):

0.3°/h

Gyro\Zero Bias Stability At Variable Temperature (100s):

0.5°/h

Gyro\Scale Factor Nonlinearity:

≤20ppm

Gyro\Random Walk Coefficient:

0.02°/½h

Gyro\Input Range:

400°/s

Accelerometer\Zero Bias Repeatability:

0.3mg

Accelerometer\Bias Temperature Sensitivity:

50μg/℃

Accelerometer\Scale Factor Repeatability:

300ppm

Accelerometer\Scale Factor Temperature Sensitivity:

20ppm/℃

Accelerometer\Input:

±20g

Features\Operating Temperature:

-40℃～60℃

Features\Storage Temperature:

-45℃～70℃

Features\Power Supply:

18～36V（DC）

Features\Stable Power Consumption:

≤8W

Features\Mounting Hole Diameter:

4-Φ4.5mm

Features\Dimensions(mm):

70.3*70.3*53

Features\Weight:

≤500g

Product Description

The INT-M-IMU01 Inertial Measurement Unit (IMU) features a strapdown architecture using optical gyroscopes and accelerometers. After applying calibration compensations, it delivers formatted real-time data streams, ensuring precise angular and linear rate measurements for a variety of platforms.

Deployment Scenarios:

Guided munitions and missile systems
Stabilized platforms for military and aerospace applications
Precision navigation and motion control systems

Design Highlights:

Adjustable accuracy and stability balance for diverse applications
Failure-resistant, ruggedized construction
Rapid initialization for immediate operational readiness
Clean digital signal path for high-fidelity data output
Extended mean time between failures for long-term reliability

Keywords: INT-M-IMU01, customized strapdown IMU, gyroscope inertial measurement unit, high-precision optical gyro IMU, missile guidance IMU, stabilized platform IMU, real-time motion data, strapdown inertial system, aerospace and military IMU

Model			INT-M-IMU01
Item	indicator	Description	Parameter
Gyro	Zero bias	Bias stability (10s)	0.3°/h
	Zero bias	Zero bias stability at variable temperature (100s)	0.5°/h
	Scaling Factor	Scale factor nonlinearity	≤20ppm
	Other indicators	Random walk coefficient	0.02°/½h
	Other indicators	Input range	400°/s
Accelerometer	Deviation	Zero bias repeatability	0.3mg
	Zero bias	Bias temperature sensitivity	50μg/℃
	Scaling Factor	Scale factor repeatability	300ppm
	Scaling Factor	Scale factor temperature sensitivity	20ppm/℃
	Range indicators	Input range	±20g
Features	Environmental performance	Operating temperature	-40℃～60℃
	Environmental performance	Storage temperature	-45℃～70℃
	General Requirements	Power supply	18～36V(DC)
		Stable power consumption	≤8W
		Mounting hole diameter	4-Φ4.5mm
		Dimensions(mm)	70.370.353
		Weight	≤500g

INT

INT-M-IMU01 Customized Strapdown Gyroscope IMU | High-Precision Inertial Measurement System Units Zero bias stability at variable temperature (100s) ：0.5°/h

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