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Dubhe-IMU1 Missile Gyroscopes Mems Inertial Measurement Unit IMU OEM

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Dubhe-IMU1 Missile Gyroscopes Mems Inertial Measurement Unit IMU OEM

Brand Name : Star & Inertia Technology

Model Number : Dubhe-IMU1

Place of Origin : China

MOQ : 1 set

Supply Ability : 500 sets per year

Delivery Time : 30 work days

Price : $1000-$100000

Payment Terms : T/T

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

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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 stability at variable temperature (100s) 0.05°/h
Scaling Factor Scale factor nonlinearity ≤20ppm
Other indicators Random walk coefficient 0.001°/½h
Input range 400°/s
Accelerometer Deviation Zero bias repeatability 20μg
Zero bias Bias temperature sensitivity 20μg/℃
Scaling Factor Scale factor repeatability 20ppm
Scale factor temperature sensitivity 20ppm/℃
Range indicators Input range ±20g
Features Environmental performance Operating temperature -40℃~60℃
Storage temperature -45℃~70℃
General Requirements Power supply 18~36V(DC)
Stable power consumption ≤20W
Mounting hole diameter 4-Φ6.5mm
Dimensions(mm) 185*136*110
Weight ≤3200g



Product Tags:

Missile mems inertial measurement unit

      

OEM mems inertial measurement unit

      

Missile imu inertial measuring unit

      
China Dubhe-IMU1 Missile Gyroscopes Mems Inertial Measurement Unit IMU OEM factory

Dubhe-IMU1 Missile Gyroscopes Mems Inertial Measurement Unit IMU OEM Images

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