Shenzhen Fire Power Control Technology Co., LTD
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China,Shenzhen ,Guangdong
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Verified Supplier
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- Micro-nano Integrated Fiber Optic Gyroscope GNSS/INS Integrated Inertial
- Product Details
- Company Details
Product Specification
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| Payment Terms |
T/T |
Supply Ability |
100 pcs per month |
| Delivery Time |
2 weeks for sample |
Packaging Details |
Sponge and box |
| Material |
Stainless steel |
Size |
68mm*71mm*60mm |
| Power |
9-36V |
Gyro range |
±300°/s |
| Gyro Zero Bias Stability |
≤1.0°/h |
Acc Range |
±50g |
| Acc Zero Bias Stability |
≤100ug |
Self-north-seeking heading accuracy |
≤1.5°/cosL |
| Azimuth measurement accuracy |
≤0.2° |
Vibration |
20~2000Hz |
| Communication Interface |
CAN/RS422/Network |
Weight |
≤0.51kg |
| Brand Name |
Firepower |
Model Number |
INS100 |
| Certification |
CE |
Place of Origin |
Shenzhen, China |
| High Light |
Micro-nano integrated fiber optic gyroscope
，GNSS/INS integrated fiber optic gyroscope
，Micro-nano integrated inertial navigation system
|
INS-100 is a high-precision integrated navigation system. It is equipped with three self-developed 40 fiber optic gyroscopes,three-self MEMS accelerometers and GNSS modules, and realizes high-precision positioning and navigation in complex environments through multi-sensor fusion and integrated navigation algorithm. The product has high reliability and strong environmental adaptability. The products can be widely used in intelligent driving, UAV, surveying and mapping, marine compass, stable platform, photoelectric pod, underwater vehicle and other fields.
Main functions of the integrated navigation system are as follows: 1. The initial alignment function is completed by using the output of the inertial device, and the shaking base alignment and the moving alignment can be carried out;
2. The GPS information received from outside can be used to complete the integrated navigation function and output information such as angle, speed and position.
3. After the satellite signal is lost, the inertial device output and the odometer input can be used to continue the navigation calculation;
4. It can output high performance and high sampling rate gyro raw output and add raw data for stable platform control.
5. The program and configuration parameters can be upgraded online through the serial port.
| Project | Indicators | Remark |
| | Measuring range | -300°/s ~+300°/s | |
| Resolution | ≤0.5°/h | |
| Bias residual | -1.0°/h ~+1.0°/h | |
| Random walk | 0.05 o / h | |
| Bias stability at room temperature | ≤0.3°/h(1σ) | 10 seconds smoothing, 1h test result |
| Bias stability at full temperature | ≤0.5°/h(1σ) | 10 seconds smoothing, 1h test result |
| Normal-temperature Bias repeatability | ≤0.3°/h(1σ) | Statistics of 6 test data |
| Bias repeatability 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 |
| Bias stability at full temperature | ≤100ug(1σ) | 10 seconds smoothing, 1H test result |
| Bias repeatability 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" | |
| 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 |
| | Optional | It can realize swaying base alignment, GPS auxiliary alignment during travel, odometer auxiliary alignment during travel and main
inertial navigation transfer alignment. |
Integrated navigation accuracy (satellite effective)
| Project | Indicators | Remark |
| | 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 | | 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) | |
About company
Company Details
Bronze Gleitlager
,
Bronze Sleeve Bushings
and
Graphite Plugged Bushings
from Quality China Factory
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Business Type:
Manufacturer,Exporter,Trading Company,Seller
-
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Total Annual:
10000000-15000000
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Employee Number:
60~100
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Ecer Certification：
Verified Supplier
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