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Robust Magnetometer Component Inertial Measurement Unit Attitude Determination Solutions Designed for Motion Sensing
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Robust Magnetometer Component Inertial Measurement Unit Attitude Determination Solutions Designed for Motion Sensing
  • name
  • name
  • name
  • name

Robust Magnetometer Component Inertial Measurement Unit Attitude Determination Solutions Designed for Motion Sensing

MOQ: 1
Standard Packaging: 30cm*30cm*28cm
Delivery Period: 30days
Payment Method: T/T
Supply Capacity: 50/1day
Details Information
Product Description
Detail Information
Place of Origin
WUHAN
Brand Name
CSSC
Certification
YJG253025689
Model Number
MEMS002
Highlight:

Magnetometer Inertial Measurement Unit

,

Energy MEMS Inertial Measurement Unit

,

MEMS Inertial Measurement Unit for UAV

Product Description
Performance Specifications






Parameter(Typical Values) Unit Type 002
Gyroscope Measurement Range °/s ±400
Bias Offset °/h 10
Bias Instability (Allan Variance) °/h 0.1
Bias Stability (10 s smoothing, 1σ, room temp) °/h 2
Bias over Full Temperature Range °/h 10
Bias Repeatability °/h 1
Angle Random Walk Robust Magnetometer Component Inertial Measurement Unit Attitude Determination Solutions Designed for Motion Sensing 0°/ 0.05
Scale Factor Nonlinearity ppm 100
Scale Factor Repeatability ppm 100
Bandwidth Hz 250
Cross Coupling % 0.1
Accelerometer Measurement Range g ±40
Bias Stability (10 s smoothing, 1σ, room temp) mg 0.2
Bias Variation over Temperature mg 1
Bias Repeatability mg 2
Scale Factor Repeatability ppm 500
Bandwidth Hz 100
Cross Coupling % 0.1
Start-up Stabilization Time s 1
Data Update Rate Hz 1000
Operating Voltage V 5±0.5
Steady-state Power Consumption W 1.5
Operating Temperature ℃ -45~80
Dimensions mm 44.8×38.6×20
Weight g 52±5
Start-up Stabilization Time
RS-422


Tags: 

mems based inertial navigation system,  

mems inertial measurement unit,  

mems imu inertial navigation system

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Products
PRODUCTS DETAILS
Products

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

Doppler Velocity Log

MEMS Inertial Navigation System
Robust Magnetometer Component Inertial Measurement Unit Attitude Determination Solutions Designed for Motion Sensing
  • name
  • name
  • name
  • name
Robust Magnetometer Component Inertial Measurement Unit Attitude Determination Solutions Designed for Motion Sensing
MOQ: 1
Standard Packaging: 30cm*30cm*28cm
Delivery Period: 30days
Payment Method: T/T
Supply Capacity: 50/1day
Detail Information
Product Description
Detail Information
Place of Origin
WUHAN
Brand Name
CSSC
Certification
YJG253025689
Model Number
MEMS002
Minimum Order Quantity:
1
Packaging Details:
30cm*30cm*28cm
Delivery Time:
30days
Payment Terms:
T/T
Supply Ability:
50/1day
Highlight

Magnetometer Inertial Measurement Unit

,

Energy MEMS Inertial Measurement Unit

,

MEMS Inertial Measurement Unit for UAV

Product Description
Performance Specifications






Parameter(Typical Values) Unit Type 002
Gyroscope Measurement Range °/s ±400
Bias Offset °/h 10
Bias Instability (Allan Variance) °/h 0.1
Bias Stability (10 s smoothing, 1σ, room temp) °/h 2
Bias over Full Temperature Range °/h 10
Bias Repeatability °/h 1
Angle Random Walk Robust Magnetometer Component Inertial Measurement Unit Attitude Determination Solutions Designed for Motion Sensing 0°/ 0.05
Scale Factor Nonlinearity ppm 100
Scale Factor Repeatability ppm 100
Bandwidth Hz 250
Cross Coupling % 0.1
Accelerometer Measurement Range g ±40
Bias Stability (10 s smoothing, 1σ, room temp) mg 0.2
Bias Variation over Temperature mg 1
Bias Repeatability mg 2
Scale Factor Repeatability ppm 500
Bandwidth Hz 100
Cross Coupling % 0.1
Start-up Stabilization Time s 1
Data Update Rate Hz 1000
Operating Voltage V 5±0.5
Steady-state Power Consumption W 1.5
Operating Temperature ℃ -45~80
Dimensions mm 44.8×38.6×20
Weight g 52±5
Start-up Stabilization Time
RS-422


Tags: 

mems based inertial navigation system,

mems inertial measurement unit,

mems imu inertial navigation system

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