Product Details
Place of Origin: China
Brand Name: RION
Model Number: INS600
Payment & Shipping Terms
Minimum Order Quantity: 1pcs
Price: US$2900.00
Packaging Details: carton with safety sponge
Delivery Time: 1-2 weeks
Supply Ability: 200pcs per month
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 |
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 |
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
★ Flight control
▶ SPECIFICATIONS
| INS600 |
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) |
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(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
