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Attitude Determination-EMES Inertial Navigation System
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Attitude Determination-EMES Inertial Navigation System
  • name
  • name
  • name
  • name

Attitude Determination-EMES Inertial Navigation System

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
RTG325028230
Model Number
MEMS 004
Product Description
Performance Specifications
Parameter Unit Type 004
Heading Accuracy(RMS) Heading ° 0.1(2m base line)
Pitch / Roll ° 0.2
Position Accuracy Horizontal m 1.5m(Single Point)(RTK:0.8cm+1ppm)

(RMS) Vertical m 3m(Single Point)(RTK:0.8cm+1ppm)
Velocity Accuracy(RMS) m/s 0.1
Gyroscope Measurement Range °/s ±400
Bias Stability (10 s smoothing, 1σ, room temp) °/h 10
Bias Variation over Temperature (10 s smoothing, RMS) °/h 60
Bias Repeatability °/h 20
Angle Random Walk Attitude Determination-EMES Inertial Navigation System 0°/ 0.5
Cross Coupling % 0.2
Accelerometer Measurement Range g ±10
Bias Stability (10 s smoothing, 1σ, room temp) mg 0.05
Bias Variation over Temperature (10 s smoothing, RMS) mg 2
Bias Repeatability mg 0.2
Cross Coupling % 0.1
Data Update Rate Hz 100(customizable)
Operating Voltage V 9~36
Power Consumption W 5
Operating Temperature ℃ -45~80
Dimensions mm 88×68×46
Weight g ≤300g
Interfaces
2 × RS-422 / RS-232 (navigation output)

1 × RS-232 (differential output)

1 × PPS output

1 × CAN output


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
Attitude Determination-EMES Inertial Navigation System
  • name
  • name
  • name
  • name
Attitude Determination-EMES Inertial Navigation System
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
RTG325028230
Model Number
MEMS 004
Minimum Order Quantity:
1
Packaging Details:
30cm*30cm*28cm
Delivery Time:
30days
Payment Terms:
T/T
Supply Ability:
50/1day
Product Description
Performance Specifications
Parameter Unit Type 004
Heading Accuracy(RMS) Heading ° 0.1(2m base line)
Pitch / Roll ° 0.2
Position Accuracy Horizontal m 1.5m(Single Point)(RTK:0.8cm+1ppm)

(RMS) Vertical m 3m(Single Point)(RTK:0.8cm+1ppm)
Velocity Accuracy(RMS) m/s 0.1
Gyroscope Measurement Range °/s ±400
Bias Stability (10 s smoothing, 1σ, room temp) °/h 10
Bias Variation over Temperature (10 s smoothing, RMS) °/h 60
Bias Repeatability °/h 20
Angle Random Walk Attitude Determination-EMES Inertial Navigation System 0°/ 0.5
Cross Coupling % 0.2
Accelerometer Measurement Range g ±10
Bias Stability (10 s smoothing, 1σ, room temp) mg 0.05
Bias Variation over Temperature (10 s smoothing, RMS) mg 2
Bias Repeatability mg 0.2
Cross Coupling % 0.1
Data Update Rate Hz 100(customizable)
Operating Voltage V 9~36
Power Consumption W 5
Operating Temperature ℃ -45~80
Dimensions mm 88×68×46
Weight g ≤300g
Interfaces
2 × RS-422 / RS-232 (navigation output)

1 × RS-232 (differential output)

1 × PPS output

1 × CAN output


Tags: 

mems based inertial navigation system,

mems inertial measurement unit,

mems imu inertial navigation system

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