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Highly Integrated Micro Inertial Navigation Module-Real-Time Dynamic Attitude Measurement System
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Highly Integrated Micro Inertial Navigation Module-Real-Time Dynamic Attitude Measurement System
  • name
  • name
  • name
  • name

Highly Integrated Micro Inertial Navigation Module-Real-Time Dynamic Attitude Measurement System

MOQ: 1
Price: 30000-55000RMB
Standard Packaging: 30cm*30cm*28cm
Delivery Period: 14days
Supply Capacity: 50/1day
Details Information
Product Description
Detail Information
Place of Origin
WUHAN
Brand Name
CSSC
Certification
TDD630285159
Model Number
DP-MS3AA
Function:
Inertial Navigation And Positioning
Powerconsumption:
Less Than 100 MW
Operating Temperature:
-40℃～﹢55℃
Heading:
≤0.15° (1σ)
Supply Voltage:
24V DC Rated(12～32V DC)
Technology:
Micro-Electro-Mechanical Systems (MEMS)
Pitch And Roll:
≤0.05° (1σ)
Operatingtemperaturerange:
-40°C To +85°C
Supplyvoltage:
3.3V To 5V
Initializationtime:
Less Than 10 Seconds
Updaterate:
100 Hz
Size:
Compact And Lightweight
Applicationfields:
Aerospace, Robotics, Automotive, Consumer Electronics
Bias Stability:
≤10°/h
Measurementaxes:
3-axis Accelerometer And 3-axis Gyroscope
Product Description

Performance Specifications

Parameter(Typical Values) Unit DP-MS3AA
Gyroscope Measurement Range °/s ±450
Bias Offset °/h 3
Bias Instability (Allan Variance) °/h 0.05
Bias Stability (10 s smoothing, 1σ, room temp) °/h 0.4
Bias over Full Temperature Range °/h 2
Bias Repeatability °/h 0.3
Angle Random Walk Highly Integrated Micro Inertial Navigation Module-Real-Time Dynamic Attitude Measurement System 0°/ 0.05
Scale Factor Nonlinearity ppm 100
Scale Factor Repeatability ppm 100
Bandwidth Hz 150
Cross Coupling % 0.1
Accelerometer Measurement Range g ±10
Bias Stability (10 s smoothing, 1σ, room temp) mg 0.05
Bias Variation over Temperature mg 0.2
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 ℃ -40~80
Dimensions mm 44.8×38.6×20
Weight g 52±5
Start-up Stabilization Time
RS-422

Highly Integrated Micro Inertial Navigation Module-Real-Time Dynamic Attitude Measurement System 1

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
Highly Integrated Micro Inertial Navigation Module-Real-Time Dynamic Attitude Measurement System
  • name
  • name
  • name
  • name
Highly Integrated Micro Inertial Navigation Module-Real-Time Dynamic Attitude Measurement System
MOQ: 1
Price: 30000-55000RMB
Standard Packaging: 30cm*30cm*28cm
Delivery Period: 14days
Supply Capacity: 50/1day
Detail Information
Product Description
Detail Information
Place of Origin
WUHAN
Brand Name
CSSC
Certification
TDD630285159
Model Number
DP-MS3AA
Function:
Inertial Navigation And Positioning
Powerconsumption:
Less Than 100 MW
Operating Temperature:
-40℃～﹢55℃
Heading:
≤0.15° (1σ)
Supply Voltage:
24V DC Rated(12～32V DC)
Technology:
Micro-Electro-Mechanical Systems (MEMS)
Pitch And Roll:
≤0.05° (1σ)
Operatingtemperaturerange:
-40°C To +85°C
Supplyvoltage:
3.3V To 5V
Initializationtime:
Less Than 10 Seconds
Updaterate:
100 Hz
Size:
Compact And Lightweight
Applicationfields:
Aerospace, Robotics, Automotive, Consumer Electronics
Bias Stability:
≤10°/h
Measurementaxes:
3-axis Accelerometer And 3-axis Gyroscope
Minimum Order Quantity:
1
Price:
30000-55000RMB
Packaging Details:
30cm*30cm*28cm
Delivery Time:
14days
Supply Ability:
50/1day
Product Description

Performance Specifications

Parameter(Typical Values) Unit DP-MS3AA
Gyroscope Measurement Range °/s ±450
Bias Offset °/h 3
Bias Instability (Allan Variance) °/h 0.05
Bias Stability (10 s smoothing, 1σ, room temp) °/h 0.4
Bias over Full Temperature Range °/h 2
Bias Repeatability °/h 0.3
Angle Random Walk Highly Integrated Micro Inertial Navigation Module-Real-Time Dynamic Attitude Measurement System 0°/ 0.05
Scale Factor Nonlinearity ppm 100
Scale Factor Repeatability ppm 100
Bandwidth Hz 150
Cross Coupling % 0.1
Accelerometer Measurement Range g ±10
Bias Stability (10 s smoothing, 1σ, room temp) mg 0.05
Bias Variation over Temperature mg 0.2
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 ℃ -40~80
Dimensions mm 44.8×38.6×20
Weight g 52±5
Start-up Stabilization Time
RS-422

Highly Integrated Micro Inertial Navigation Module-Real-Time Dynamic Attitude Measurement System 1

Tags: 

mems based inertial navigation system,

mems inertial measurement unit,

mems imu inertial navigation system

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