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Categories | Inertial Navigation System |
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Brand Name: | Firepower |
Model Number: | INS100 |
Certification: | CE |
Place of Origin: | CHINA |
MOQ: | 1 |
Price: | negotiable |
Payment Terms: | L/C,T/T |
Supply Ability: | 100/Month |
Delivery Time: | 2 week for sample |
Packaging Details: | Wooden box |
Gyro Range: | ±300°/s |
Accelerometer Range: | ±50g |
Random Walk: | 0.05 °/h |
Gyro Bias Stability: | ≤0.3°/h(1σ) |
Pitch Angle Holding Accuracy: | ≤0.2°/h |
Gyro Bandwidth: | 300Hz |
Scale Factor Nonlinearity: | ≤200ppm |
North Seeking Time: | ≤5min |
Company Info. |
Shenzhen Fire Power Control Technology Co., LTD |
Verified Supplier |
View Contact Details |
Product List |
Tactical Grade High-Accuracy GNSS Inertial Navigation System for Vessel Tracking
Product Description
Main functions of the integrated navigation system are as follows:
Main Parameters
Gyro technology
Project | Indicators | Remark | |
Gyro | Measuring range | -300°/s ~+300°/s | |
Resolution | ≤0.5°/h | ||
Bias residual | -1.0°/h ~+1.0°/h | ||
Random walk | 0.05 o / h | ||
Biasstability at room temperature | ≤0.3°/h(1σ) | 10 seconds smoothing, 1H test result | |
Biasstability at full temperature | ≤0.5°/h(1σ) | 10 seconds smoothing, 1H test result | |
Normal-temperature Biasrepeatability | ≤0.3°/h(1σ) | Statistics of 6 test data | |
Biasrepeatability at full temperature | ≤0.5°/h(1σ) | Take 2 Biasdata at full temperature, high temperature, low temperature and normal temperature respectively | |
Scale factor nonlinearity | ≤200ppm | Full temperature and constant temperature | |
Scale factor repeatability | ≤200ppm(1σ) | Full temperature and constant temperature | |
Gyro start time | ≤5s | ||
Gyro bandwidth | 300Hz | Design assurance, batch testing | |
Installation error residual of three-axis gyroscope | ≤30" |
Accelerometer technical indicators
Project | Indicators | Remark | |
Acceleration | Measuring range | -50g ~ +50g | Design and selection guarantee |
Scale factor nonlinearity | ≤200ppm | Design and selection guarantee | |
Biasstability at full temperature | ≤100ug(1σ) | 10 seconds smoothing, 1H test result | |
Biasrepeatability at full temperature | ≤100ug(1σ) | Take 2 Biasdata at full temperature, high temperature, low temperature and normal temperature respectively | |
Scale factor repeatability | ≤100ppm(1σ) | Design and selection guarantee | |
Random walk | ≤0.02m/s/h1/2 | ||
Add up the starting time | ≤5s | ||
Triaxial addition installation error residual | ≤30" |
Alignment accuracy
Integrated navigation accuracy (satellite effective)
Project | Indicators | Remark | |
Alignment accuracy | North seeking time | ≤5min | Generally, the standard is 3min or 5min. |
Heading Angle Alignment Repeatability | ≤1°/cosL | 1σ | |
Pitch Alignment Repeatability | ≤0.05° | 1σ | |
Roll Angle Alignment Repeatability | ≤0.05° | 1σ | |
North-seeking mode | Optional | It can realize swaying base alignment, GPS auxiliary alignment during travel, odometer auxiliary alignment during travel and main inertial navigation transfer alignment. |
Inertial navigation accuracy (invalid satellite)
Project | Indicators | Remark | |
Inertial navigation accuracy | Accuracy of course angle maintenance | ≤2°/h | |
Pitch Angle Holding Accuracy | ≤0.2°/h | ||
Accuracy of roll angle maintenance | ≤0.2°/h | ||
Pure inertial positioning accuracy | ≤20m(100s) | CEP, without external information assistance | |
Position positioning accuracy of odometer integrated navigation | ≤ 0.2% (mileage greater than 3 km) | ||
Position positioning accuracy of odometer integrated navigation | ≤1m(50s) |
Size
Main Application Fields
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