PRODUCTS DETAILS

Home > Products >

Dubhe-IMU1 Missile Gyroscopes Mems Inertial Measurement Unit IMU OEM

Products

Laser Inertial Navigation System

Fiber Optic Inertial Navigation System

Aircraft Inertial Navigation System

Marine Inertial Navigation System

Automotive Inertial Navigation System

Ring Laser Gyroscope

Mr. Sales

18071128027@163.com

+86-18071128027

Contact Now

Dubhe-IMU1 Missile Gyroscopes Mems Inertial Measurement Unit IMU OEM

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

Details Information

Product Description

Detail Information

Place of Origin

China

Brand Name

Star & Inertia Technology

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

Highlight:

Missile mems inertial measurement unit

OEM mems inertial measurement unit

Missile imu inertial measuring unit

Product Description

IMU (Dubhe-IMU1)

The Optical Inertial Measurement Unit (IMU) employs gyroscopes and accelerometers in a strapdown configuration, performing real-time data output according to specific protocols after compensating for installation errors and temperature effects. Applications include missile systems, pod-mounted equipment, and platforms requiring precise angular/linear rate measurements.

Key features:

1) High accuracy and stability with flexible design;

2) All-solid-state construction without moving parts;

3) Fast startup with digital output for easy integration;

4) Low noise, power consumption and cost;

5) High reliability and long service life.

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

Tags:

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

Star & Inertia Technology

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:

20μg

Accelerometer\Bias Temperature Sensitivity:

20μg/℃

Accelerometer\Scale Factor Repeatability:

20ppm

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:

≤16W

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:

T/T

Supply Ability:

500 sets per year

Highlight

Missile mems inertial measurement unit

OEM mems inertial measurement unit

Missile imu inertial measuring unit

Product Description

IMU (Dubhe-IMU1)

Key features:

1) High accuracy and stability with flexible design;

2) All-solid-state construction without moving parts;

3) Fast startup with digital output for easy integration;

4) Low noise, power consumption and cost;

5) High reliability and long service life.

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

Tags:

Laser Inertial Navigation System

Fiber Optic Inertial Navigation System

Aircraft Inertial Navigation System

Marine Inertial Navigation System

Automotive Inertial Navigation System

AHRS System

IMU Inertial Measurement Unit

Fiber Optic Gyroscope

Ring Laser Gyroscope

Dubhe-IMU1 Missile Gyroscopes Mems Inertial Measurement Unit IMU OEM

Missile mems inertial measurement unit

OEM mems inertial measurement unit

Missile imu inertial measuring unit

inertial measurement system,

imu inertial sensor,

mems inertial measurement unit

Merak-IMU01 Customized Strapdown Gyroscope Inertial Measurement System Units

Merak-IMU03 50ppm Realtime IMU Inertial Measurement Unit With Gyro Accelerometer Core

Merak-IMU05 ODM Aerospace Inertial Measurement Units Imus Sensor Motion Sensitive

Merak-IMU1 Military Optical IMU Inertial Measurement Unit Gyroscope For Missile Guidance