INS600 Antenna Inertial Navigation Sensor High Performance IMU With 2 GPS
Brand Name:RION
Certification:CE
Model Number:INS600
Minimum Order Quantity:1
Delivery Time:10 days for sample order
Payment Terms:T/T
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4th Floor Block 1, COFCO(FUAN) Robotics Industrial Park , Da Yang Road No. 90, Fuyong Distict, Shenzhen City, China
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INS600 RTK INTEGRATED NAVIGATION SYSTEM.pdf
INS600 dual GPS antenna high performance IMU with 2 GPS inertial navigation sensor
▶ 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 ★ Flight control
▶ 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.
▶ 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
▶ 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- |
INS600 Antenna Inertial Navigation Sensor High Performance IMU With 2 GPS
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