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Shenzhen Rion Technology Co., Ltd.
Shenzhen Rion Technology Co., Ltd.
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Navigation Dual GPS IMU Sensor Low Bias MEMS For Precision Farming

Product Details

Place of Origin: China

Brand Name: RION

Certification: CE

Model Number: INS600

Payment & Shipping Terms

Minimum Order Quantity: 1

Price: 3200

Packaging Details: carton box

Delivery Time: 10 days for sample order

Payment Terms: T/T

Supply Ability: 500/month

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Specifications
Highlight:

Low Bias GPS IMU Sensor

,

Dual GPS IMU Sensor

,

MEMS IMU Inertial Measurement Unit

Roll/pitch Accuracy:
0.2°
Heading Drift (1min):
0.15°
Gyro Range:
300°/s
Gyro Zero Bias Instability:
10°/h
Accelerometer Range:
4g
Accelerometer Zero Bias Stabili:
0.2mg
Roll/pitch Accuracy:
0.2°
Heading Drift (1min):
0.15°
Gyro Range:
300°/s
Gyro Zero Bias Instability:
10°/h
Accelerometer Range:
4g
Accelerometer Zero Bias Stabili:
0.2mg
Description
Navigation Dual GPS IMU Sensor Low Bias MEMS For Precision Farming

INS600 RTK INTEGRATED NAVIGATION SYSTEM.pdf

 

Navigation GPS sensor dual GPS IMU low bias MEMS IMU with 2 GPS

 

FEATURE

★ Gyro bias instability 10°/h (Allan Variance)

★ Accelerometer bias 1.7mg(within 4g range)

 

 

▶ INTRODUCTION

The INS600 series is a dual-antenna GPS/INS integrated navigation system built by RION. The dual-antenna differential positioning measurement unit (IMU) is precisely calibrated in the full temperature to meet the performance requirements in different environments. The multi-data Kalman filter fusion algorithm is realized by a built-in navigation computer, and outputs real-time accurate carrier posture, heading information, three-dimensional position and velocity information, and various inertial device information. The appearance is exquisite, the structure is small, the installation is convenient, the use is flexible, and the operation is more stable and reliable.

 

APPICATION

★ Precision farming ★ Car navigation & measurement & control system

★ Surveying and mapping POS system ★ Ocean and underwater mapping

★ Industrial park unmanned vehicle ★ Ship and ocean engineering

★ High-speed train measurement and control system ★ Flight control

 

 

▶ PARAMETERS

 

INS600    
System Roll/pitch(1σ) 0.2°

GPS loss-lock accuracy

(vehicle-mounted CEP)

Position drift(1km or 3min) 0.2%,with odometer
Heading drift (1min) 0.15°
Gyro Measuring range 300°/s

Zero bias instability

(Allen variance)

10°/h

Zero bias stability

(1s smooth)

15°/h
Zero bias repeatability 15°/h
Full temperature zero bias 0.1°/s
Scale factor nonlinearity 200ppm
Scale factor repeatability 200ppm
Resolution <0.01°/s
Acceleration sensitivity <0.0028°/s/g,rms all direction
Angle random walk 0.15°/√hr
Bandwidth 200Hz
Delay <2ms
Accelerometer Range 4g
Zero bias stability 0.2mg
Full temperature zero bias 1.7mg
Scale factor repeatability 200ppm
Resolution 0.1mg
Nonlinearity 0.1%
Bandwidth 200Hz
Satellite Navigation Board Position(CEP) 1.2m,2cm+1ppm(RTK)
Speed(1s) 0.03 m/s
Heading(1s) 0.08°(base line 2m)
Frequency band GPS L1,L2,L2C,Beidou B1,B2
Interface Input voltage 12V
Working current 0.55A
Interface Type 10 core aviation plug
Main engine Size 155*120*55mm
Weight 708g
Antenna Size 152*152*62.2mm
Weight(single) 433.5g
Data line Size(length) 5M
Weight(single piece) 30g

 

▶ DIMENSION

Navigation Dual GPS IMU Sensor Low Bias MEMS For Precision Farming 0

 

▶ PIN DEFINITION

 

Pin Definition Description
A GND Power ground
B +12VDC Power +(0.55A)
C RS422_TX_N RS422 send-
D    
E    
F    
G RS422_RX_P RS422 receive+
H    
J RS422_TX_P RS422 send+
K RS422_RX_N RS422 receive-
 

Navigation Dual GPS IMU Sensor Low Bias MEMS For Precision Farming 1

 

 

 

 

 

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