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Dubhe-IMU1 MEMS Inertial Measurement Unit | Missile Gyroscope OEM IMU

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Dubhe-IMU1 MEMS Inertial Measurement Unit | Missile Gyroscope OEM IMU

MOQ:	1 set
Price:	$1000-$100000
Delivery Period:	30 work days
Payment Method:	T/T
Supply Capacity:	500 sets per year

Detail Information

Product Description

Detail Information

Place of Origin

China

Brand Name

Wuhan Deep Pilot Technology Co.,Ltd.

Model Number

Dubhe-IMU1

Gyro\Bias Stability (10s):

0.01°/h

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

0.05°/h

Gyro\Scale Factor Nonlinearity:

≤20ppm

Gyro\Random Walk Coefficient:

0.001°/½h

Gyro\Input Range:

400°/s

Accelerometer\Zero Bias Repeatability:

Accelerometer\Bias Temperature Sensitivity:

20μg/℃

Accelerometer\Scale Factor Repeatability:

20ppm

Accelerometer\Scale Factor Temperature Sensitivity:

20ppm/℃

Accelerometer\Input:

Features\Operating Temperature:

-40℃～60℃

Features\Storage Temperature:

-45℃～70℃

Features\Power Supply:

18～36V（DC）

Features\Stable Power Consumption:

Features\Mounting Hole Diameter:

4-Φ6.5mm

Features\Dimensions(mm):

185*136*110

Features\Weight:

≤3200g

Product Description

The Dubhe-IMU1 Optical Inertial Measurement Unit (IMU) is a high-precision strapdown navigation sensor combining gyroscopes and accelerometers. It provides real-time data output after compensating for installation errors and temperature effects, ensuring accurate angular and linear rate measurements for a variety of platforms.

Applications:

Missile systems
Pod-mounted equipment
Platforms requiring precise angular and linear rate measurements

Key Features and Capabilities:

High accuracy and stability with flexible design options
All-solid-state construction with no moving parts
Fast startup and digital output for easy system integration
Low noise, low power consumption, and cost-effective design
High reliability with long service life

Keywords: Dubhe-IMU1, MEMS inertial measurement unit, missile gyroscope IMU, strapdown IMU, high-precision navigation sensor, OEM IMU, gyroscope accelerometer IMU, real-time IMU data output

Model			Dubhe-IMU1
Item	indicator	Description	Parameter
Gyro	Zero bias	Bias stability (10s)	0.01°/h
	Zero bias	Zero bias stability at variable temperature (100s)	0.05°/h
	Scaling Factor	Scale factor nonlinearity	≤20ppm
	Other indicators	Random walk coefficient	0.001°/½h
	Other indicators	Input range	400°/s
Accelerometer	Deviation	Zero bias repeatability	20μg
	Zero bias	Bias temperature sensitivity	20μg/℃
	Scaling Factor	Scale factor repeatability	20ppm
	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	≤20W
		Mounting hole diameter	4-Φ6.5mm
		Dimensions(mm)	185136110
		Weight	≤3200g

Products

MOQ:	1 set
Price:	$1000-$100000
Delivery Period:	30 work days
Payment Method:	T/T
Supply Capacity:	500 sets per year

Detail Information

Product Description

Detail Information

Place of Origin

China

Brand Name

Wuhan Deep Pilot Technology Co.,Ltd.

Model Number

Dubhe-IMU1

Gyro\Bias Stability (10s):

0.01°/h

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

0.05°/h

Gyro\Scale Factor Nonlinearity:

≤20ppm

Gyro\Random Walk Coefficient:

0.001°/½h

Gyro\Input Range:

400°/s

Accelerometer\Zero Bias Repeatability:

Accelerometer\Bias Temperature Sensitivity:

20μg/℃

Accelerometer\Scale Factor Repeatability:

20ppm

Accelerometer\Scale Factor Temperature Sensitivity:

20ppm/℃

Accelerometer\Input:

Features\Operating Temperature:

-40℃～60℃

Features\Storage Temperature:

-45℃～70℃

Features\Power Supply:

18～36V（DC）

Features\Stable Power Consumption:

Features\Mounting Hole Diameter:

4-Φ6.5mm

Features\Dimensions(mm):

185*136*110

Features\Weight:

≤3200g

Minimum Order Quantity:

1 set

Price:

$1000-$100000

Delivery Time:

30 work days

Payment Terms:

Supply Ability:

500 sets per year

Product Description

Applications:

Missile systems
Pod-mounted equipment
Platforms requiring precise angular and linear rate measurements

Key Features and Capabilities:

High accuracy and stability with flexible design options
All-solid-state construction with no moving parts
Fast startup and digital output for easy system integration
Low noise, low power consumption, and cost-effective design
High reliability with long service life

Keywords: Dubhe-IMU1, MEMS inertial measurement unit, missile gyroscope IMU, strapdown IMU, high-precision navigation sensor, OEM IMU, gyroscope accelerometer IMU, real-time IMU data output

Model			Dubhe-IMU1
Item	indicator	Description	Parameter
Gyro	Zero bias	Bias stability (10s)	0.01°/h
	Zero bias	Zero bias stability at variable temperature (100s)	0.05°/h
	Scaling Factor	Scale factor nonlinearity	≤20ppm
	Other indicators	Random walk coefficient	0.001°/½h
	Other indicators	Input range	400°/s
Accelerometer	Deviation	Zero bias repeatability	20μg
	Zero bias	Bias temperature sensitivity	20μg/℃
	Scaling Factor	Scale factor repeatability	20ppm
	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	≤20W
		Mounting hole diameter	4-Φ6.5mm
		Dimensions(mm)	185136110
		Weight	≤3200g

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