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Merak-IMU61 Optical Gyroscope Strapdown Inertial Measurement Unit | High-Precision IMU System
  • name
  • name
  • name
  • name
  • name
  • name
  • name
  • name
  • name
  • name

Merak-IMU61 Optical Gyroscope Strapdown Inertial Measurement Unit | High-Precision IMU System

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
Merak-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 Merak-IMU61 Inertial Measurement Unit (IMU) features a strapdown architecture using optical gyroscopes and accelerometers. After applying calibration compensations, it delivers formatted, real-time data streams suitable for applications requiring precise angular and linear rate measurements, such as guided munitions and stabilized platforms.

Deployment Scenarios:

  • Guided munitions and missile systems

  • Stabilized platforms for military and aerospace applications

  • Precision navigation and control systems

Design Highlights:

  1. Adjustable accuracy and stability for versatile applications

  2. Failure-resistant, ruggedized construction

  3. Rapid initialization for quick operational readiness

  4. Clean digital signal path for high-fidelity data output

  5. Extended mean time between failures for reliable long-term operation

Keywords: Merak-IMU61, optical gyroscope IMU, strapdown inertial measurement unit, high-precision IMU, guided munitions navigation, stabilized platform IMU, optical gyro inertial system, real-time IMU data, aerospace and military IMU

Model
Merak-IMU61
Item indicator Description Parameter
Gyro Zero bias Bias stability (10s) 0.03°/h
Zero bias stability at variable temperature (100s) 0.5°/h
Scaling Factor Scale factor nonlinearity ≤20ppm
Other indicators Random walk coefficient 0.02°/½h
Input range 400°/s
Accelerometer Deviation Zero bias repeatability 0.3mg
Zero bias Bias temperature sensitivity 50μg/℃
Scaling Factor Scale factor repeatability 300ppm
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 ≤8W
Mounting hole diameter 4-Φ4.5mm
Dimensions(mm) 70.3*70.3*53
Weight ≤500g



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products
PRODUCTS DETAILS
Products

Ring Laser Gyroscope

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

Portable UUV

Laser
Merak-IMU61 Optical Gyroscope Strapdown Inertial Measurement Unit | High-Precision IMU System
  • name
  • name
  • name
  • name
  • name
  • name
  • name
  • name
  • name
  • name
Merak-IMU61 Optical Gyroscope Strapdown Inertial Measurement Unit | High-Precision IMU System
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
Merak-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
Minimum Order Quantity:
1 set
Price:
$1000-$100000
Delivery Time:
30 work days
Payment Terms:
T/T
Supply Ability:
500 sets per year
Product Description

The Merak-IMU61 Inertial Measurement Unit (IMU) features a strapdown architecture using optical gyroscopes and accelerometers. After applying calibration compensations, it delivers formatted, real-time data streams suitable for applications requiring precise angular and linear rate measurements, such as guided munitions and stabilized platforms.

Deployment Scenarios:

  • Guided munitions and missile systems

  • Stabilized platforms for military and aerospace applications

  • Precision navigation and control systems

Design Highlights:

  1. Adjustable accuracy and stability for versatile applications

  2. Failure-resistant, ruggedized construction

  3. Rapid initialization for quick operational readiness

  4. Clean digital signal path for high-fidelity data output

  5. Extended mean time between failures for reliable long-term operation

Keywords: Merak-IMU61, optical gyroscope IMU, strapdown inertial measurement unit, high-precision IMU, guided munitions navigation, stabilized platform IMU, optical gyro inertial system, real-time IMU data, aerospace and military IMU

Model
Merak-IMU61
Item indicator Description Parameter
Gyro Zero bias Bias stability (10s) 0.03°/h
Zero bias stability at variable temperature (100s) 0.5°/h
Scaling Factor Scale factor nonlinearity ≤20ppm
Other indicators Random walk coefficient 0.02°/½h
Input range 400°/s
Accelerometer Deviation Zero bias repeatability 0.3mg
Zero bias Bias temperature sensitivity 50μg/℃
Scaling Factor Scale factor repeatability 300ppm
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 ≤8W
Mounting hole diameter 4-Φ4.5mm
Dimensions(mm) 70.3*70.3*53
Weight ≤500g



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15827090628
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