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


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Dubhe-IMU1 Missile Gyroscopes Mems Inertial Measurement Unit IMU OEM

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Product Detail
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
Contact Supplier
Dubhe-IMU1 Missile Gyroscopes Mems Inertial Measurement Unit IMU OEM

CSSC Star&Inertia Technology co.,ltd.

Verified Supplier
1 Years
hubei, wuhan
Since 2013
Business Type :
Manufacturer
Main Products :
Laser Inertial Navigation System, Fiber Optic Inertial Navigation System, Aircraft Inertial Navigation System
Total Annual :
5000000-10000000
Employee Number :
300~500
Certification Level :
Verified Supplier
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