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Vehicle Navigation IMU Inertial Sensor 6 Axis GPS Ship UAV Motion

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Vehicle Navigation IMU Inertial Sensor 6 Axis GPS Ship UAV Motion
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Features
Specifications
Usage: Vehicle Navigation
Range: ±300
Resolution: <0.005
Acceleration Sensitivity: <10°/h/g,rms Direction
Angle Random Walk: <0.15
Interface Type: Micro-DB9,RS422
Horizontal Position Estimation Accuracy: 2M
Pure Inertial Position: <40m@1min
High Light:

6 Axis IMU Inertial Sensor

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Navigation IMU Inertial Sensor

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UAV IMU Inertial Measurement Unit

Basic Infomation
Place of Origin: Guangdong, China
Brand Name: RION
Certification: CE
Model Number: IMU560-422
Payment & Shipping Terms
Packaging Details: CARTON
Delivery Time: 7 days
Payment Terms: T/T, Paypal
Supply Ability: 1000 Bag/Bags per Month
Product Description

Vehicle navigation sensor 6 axis GPS IMU ship inertial motion sensor UAV inertial sensor

 

Download datasheet please click below 

IMU560 IMU COMBINED INERTIAL NAVIGATION SYSTEM.pdf...

 

Application

★ High-speed train measurement and control system

★ Marine and underwater surveying and mapping

★ Surveying and mapping POS system

★ Ship and ocean engineering

★ Vehicle positioning and navigation

★ UAV navigation and control

★ Vehicle navigation and measurement and control system

 

The IMU560 series is a GPS/INS MEMS integrated navigation system built by RION.

 

The IMU560 series is positioned as a vehicle/shipborne general inertial and integrated navigation product

target market:

(1) moving through

(2) Car navigation

(3) Dynamic attitude measurement

 

 

Specifications

 

IMU560 PARAMETER UNIT
Roll/pitch 1σ (dynamic) 0.3 °
HEADING POSITION ESTIMATION ACCURACY Heading Accuracy 1σ 0.3 ° (GPS effective) °
0.5°(GPSunlock 5min) °

Pure Inertial Position

Estimation Accuracy 1σ

<40m@1min(GPS unlock) m@1min
Output Frequency 1~100 Hz
GYRO Range ±300 °/s
Zero Bias Instability(Allan) 10 °/h
Zero Bias Stability(10s Mean) 15 °/h
Zero Bias Repeatability 15 °/h
Nonlinear Error <0.1% of FS  
Scale Factor Nonlinearity1 <0.02 %
Scale Factor Change ( 25 ° C) ±0.3 %
Resolution <0.01 °/s
Acceleration Sensitivity <0.0028 °/s/g,rms
Angle Random Walk <0.15 °/√hr
Noise Intensity 0.014 °/s/√hr
Bandwidth 100 Hz
ACCELEROMETER Range ±4 g
Zero Bias Stability 0.2 mg
Full Temperature Zero Bias 1.7 mg
Scale Factor Stability <0.1 %
Resolution 0.1 mg
Nonlinear 2 0.1 %
Noise Intensity 200 ug/√hr
Bandwidth 100 Hz
MAGNETOMETER Range ±2 Gauss
MAGNETIC AZIMUTH Range ±180 °
Accuracy ±1.0 °
Air pressure Pressure range 1000~120000  
Barometric error ±250 Pascal
STANDARD GPS PARAMETERS Start Time Cold start: 29s hot start: 1s
Sensitivity -166dBm
Speed 0.05m/s
Azimuth Accuracy 0.3°,P=50%@30m/s
level reckoned accuracy 2m
ENVIRONMENTAL CHARACTERISTICS Vibration Resistant 10grms,10~1000Hz
Impact Resistance 100g@11ms,3 Axial Direction (Half Sinusoid)
Range Of Working Temp. -40°C~+85°C
ELECTRICAL INTERFACE Input Current <100mA
Input Voltage 9-36V(Ripple 50mV)
Interface Type J30J-9ZKP
COMPATIBLE SATELLITE MODE GPS L1C/A, SBAS L1C/A, GLONASS L1OF, BEIDOU B1
WEIGHT ≤100g (Excluding cables)
 

INSTALLATION AXIS

Vehicle Navigation IMU Inertial Sensor 6 Axis GPS Ship UAV Motion 0

IMU560 use NED coordinate, right hand coordinate, axis direction above.

By the rotation direction Z-Y-X, when X forward direction point to the front of carrier, then the angle rotating Z axis is yaw, Y axis pitch, X axis roll.

 

SIGNAL DEFINITION
 
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Get in touch with us
Contact Person : Alice Du
Tel : 86-15625295088
Fax : 86-755-29761269
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