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High-Reliability Integrated Navigation System-Low-Power Consumption MEMS Measurement Unit
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High-Reliability Integrated Navigation System-Low-Power Consumption MEMS Measurement Unit
  • name
  • name
  • name
  • name

High-Reliability Integrated Navigation System-Low-Power Consumption MEMS Measurement Unit

MOQ: 1
Standard Packaging: 30cm*30cm*28cm
Delivery Period: 14days
Payment Method: T/T
Supply Capacity: 50/1day
Details Information
Product Description
Detail Information
Place of Origin
WUHAN
Brand Name
CSSC
Certification
TED298025250
Model Number
DP-MS1AA
Usage:
Position Sensor,Vibration Sensor,Inertial Navigation,inertial Sensor,Speed Sensor
Output:
Digital Sensor,Analog Sensor,Other,INS,inertial Sensor
Theory:
Capacitance Sensor,Other,Optical Sensor,Current Sensor,GPS Navigation
Type:
Gps Navigator,Inertial Navigation System,Gps Tracker
Product Name:
Inertial Navigation Systems,Compass Sensors,Accelerometer,INS,Fiber Optic Gyros
Material:
Metal,Zinc,MEMS,300 Series Stainless Steel
Name:
Mini AHRS 3000 Attitude Heading Reference System,IMU300 High Accuracy Digital IMU,High Accuracy Strapdown MEMS INS Inertial Navigation Systems
Wide Operating Temperature:
-40~+85℃
Product Description
Performance Specifications


Parameter(Typical Values) Unit DP-MS1AA
Gyroscope Measurement Range °/s ±400
Bias Offset °/h 15
Bias Instability (Allan Variance) °/h 0.3
Bias Stability (10 s smoothing, 1σ, room temp) °/h 3
Bias over Full Temperature Range °/h 20
Bias Repeatability °/h 3
Angle Random Walk High-Reliability Integrated Navigation System-Low-Power Consumption MEMS Measurement Unit 0°/ 0.15
Scale Factor Nonlinearity ppm 100
Scale Factor Repeatability ppm 100
Bandwidth Hz 250
Cross Coupling % 0.1
Accelerometer Measurement Range g ±80
Bias Stability (10 s smoothing, 1σ, room temp) mg 1
Bias Variation over Temperature mg 0.5
Bias Repeatability mg 5
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




High-Reliability Integrated Navigation System-Low-Power Consumption MEMS Measurement Unit 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
High-Reliability Integrated Navigation System-Low-Power Consumption MEMS Measurement Unit
  • name
  • name
  • name
  • name
High-Reliability Integrated Navigation System-Low-Power Consumption MEMS Measurement Unit
MOQ: 1
Standard Packaging: 30cm*30cm*28cm
Delivery Period: 14days
Payment Method: T/T
Supply Capacity: 50/1day
Detail Information
Product Description
Detail Information
Place of Origin
WUHAN
Brand Name
CSSC
Certification
TED298025250
Model Number
DP-MS1AA
Usage:
Position Sensor,Vibration Sensor,Inertial Navigation,inertial Sensor,Speed Sensor
Output:
Digital Sensor,Analog Sensor,Other,INS,inertial Sensor
Theory:
Capacitance Sensor,Other,Optical Sensor,Current Sensor,GPS Navigation
Type:
Gps Navigator,Inertial Navigation System,Gps Tracker
Product Name:
Inertial Navigation Systems,Compass Sensors,Accelerometer,INS,Fiber Optic Gyros
Material:
Metal,Zinc,MEMS,300 Series Stainless Steel
Name:
Mini AHRS 3000 Attitude Heading Reference System,IMU300 High Accuracy Digital IMU,High Accuracy Strapdown MEMS INS Inertial Navigation Systems
Wide Operating Temperature:
-40~+85℃
Minimum Order Quantity:
1
Packaging Details:
30cm*30cm*28cm
Delivery Time:
14days
Payment Terms:
T/T
Supply Ability:
50/1day
Product Description
Performance Specifications


Parameter(Typical Values) Unit DP-MS1AA
Gyroscope Measurement Range °/s ±400
Bias Offset °/h 15
Bias Instability (Allan Variance) °/h 0.3
Bias Stability (10 s smoothing, 1σ, room temp) °/h 3
Bias over Full Temperature Range °/h 20
Bias Repeatability °/h 3
Angle Random Walk High-Reliability Integrated Navigation System-Low-Power Consumption MEMS Measurement Unit 0°/ 0.15
Scale Factor Nonlinearity ppm 100
Scale Factor Repeatability ppm 100
Bandwidth Hz 250
Cross Coupling % 0.1
Accelerometer Measurement Range g ±80
Bias Stability (10 s smoothing, 1σ, room temp) mg 1
Bias Variation over Temperature mg 0.5
Bias Repeatability mg 5
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




High-Reliability Integrated Navigation System-Low-Power Consumption MEMS Measurement Unit 1

Tags: 

mems based inertial navigation system,

mems inertial measurement unit,

mems imu inertial navigation system

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