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INS600 RTK Precision Farming Dual Antenna GPS / INS Integrated Navigation System

INS600 RTK Precision Farming Dual Antenna GPS / INS Integrated Navigation System
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Gyro Bias Instability: 10°/h (Allan Variance)
Accelerometer Bias: 1.7mg(within 4g Range)
Roll/pitch(1σ): 0.2°
Measuring Range: 300°/s
Gyro Measuring Range Zero Bias Instability (Allen Variance) Zero Bias Stability(1s Smooth): 15°/h
Zero Bias Instability (Allen Variance): 10°/h
Accelerometer Range: 4G
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vRTK Precision Farming Dual Antenna


INS600 Integrated System


1.7mg INS Integrated Navigation System

Basic Infomation
Place of Origin: China
Brand Name: RION
Model Number: INS600
Payment & Shipping Terms
Packaging Details: carton with safety sponge
Delivery Time: 1-2 weeks
Supply Ability: 200pcs per month
Product Description

INS600 RTK Precision Farming Dual-antenna GPS/INS Integrated Navigation System 





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

★ Accelerometer bias 1.7mg(within 4g range)




★ 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





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.




INS600 RTK Precision Farming Dual Antenna GPS / INS Integrated Navigation System 0INS600   PARAMETERS
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)

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(1σ) 0.03 m/s
Heading(1σ) 0.08°(base line 2m)
Frequency band GPS L1,L2,L2C,Beidou B1,B2
Interface Input voltage 9~36V
Working current 0.55A(12V)
Interface Type 12 core aviation plug
Main engine Size 120*120*55mm
Weight 708g
Antenna Size 152*152*62.2mm
Weight(single) 433.5g
Data line Size(length) 5M
Weight(single piece) 30g

*Delivery qualification test index

  • Within ±100°/s, the symmetry and nonlinearity are required to be <200ppm within ±100°/s, test angular rate is 0, ±0.1, ±0.2, ±0.5, ±1, ±2, ±5±n*5, n = 1,2 , 3...
  • Measure ±1g and full scale separately



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