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4G GPS/INS Integrated Navigation System INS600 Precision Farming Dual Antenna

Categories IMU Inertial Measurement Unit
Brand Name: RION
Model Number: INS600
Place of Origin: China
MOQ: 1pcs
Price: US$2900.00
Supply Ability: 200pcs per month
Delivery Time: 1-2 weeks
Packaging Details: carton with safety sponge
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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4G GPS/INS Integrated Navigation System INS600 Precision Farming Dual Antenna

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


▶ GENERAL DESCRIPTION


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.


▶ FEATURE


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

★ Accelerometer bias 1.7mg(within 4g range)


▶ 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


SPECIFICATIONS

INS600PARAMETERS
SystemRoll/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°
GyroMeasuring range300°/s

Zero bias instability

(Allen variance)

10°/h
Zero bias stability(1s smooth)15°/h
Zero bias repeatability15°/h
Full temperature zero bias0.1°/s
Scale factor nonlinearity200ppm
Scale factor repeatability200ppm
Resolution<0.01°/s
Acceleration sensitivity<0.0028°/s/g,rms all direction
Angle random walk0.15°/√hr
Bandwidth200Hz
Delay<2ms
AccelerometerRange4g
Zero bias stability0.2mg
Full temperature zero bias1.7mg
Scale factor repeatability200ppm
Resolution0.1mg
Nonlinearity0.1%
Bandwidth200Hz
Satellite Navigation BoardPosition(CEP)1.2m,2cm+1ppm(RTK)
Speed(1σ)0.03 m/s
Heading(1σ)0.08°(base line 2m)
Frequency bandGPS L1,L2,L2C,Beidou B1,B2
InterfaceInput voltage9~36V
Working current0.55A(12V)
Interface Type12 core aviation plug
Main engineSize120*120*55mm
Weight708g
AntennaSize152*152*62.2mm
Weight(single)433.5g
Data lineSize(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

Quality 4G GPS/INS Integrated Navigation System INS600 Precision Farming Dual Antenna for sale
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