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Fiber optic gyroscope-Strapdown Inertial/Satellite Integrated Navigation System
JIO-F100S Fiber optic gyroscope-Strapdown Inertial/Satellite Integrated Navigation System is composed of high-precision closed-loop fiber-optic gyroscope, quartz Flexible accelerometer and high-end GNSS receiving board, through multi-sensor fusion and guidance Realization of aerial calculation algorithm, providing high-precision navigation attitude,speed and position information to the outside world information to meet high-precision measurement and control requirements.
Model:JIO-F100S
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Product Description
JIOPTICS installation of fiber optic gyroscope to provide ease of integration flexibility, and our developers toolkit to rapid prototyping, not only meet the specification requirements, also provide high-quality performance meet the demand of end users.
Our services
JIOPTICS is a professional and efficient team. Provide OEM/ODM services for you, contact us to customize your exclusive fiber optical gyroscope
Product Features
- 0.8nmile/h navigation grade accuracy
- Multi-mode selection, vehicle mode/airplane mode
- Static initial alignment 3min / shaking base initial alignment 8min
- Fault self-check
- Rich interfaces, support RS232, RS422, CAN and other standard interfaces
- High reliability
- Multi-mode selection, vehicle mode/airplane mode
- Static initial alignment 3min / shaking base initial alignment 8min
- Fault self-check
- Rich interfaces, support RS232, RS422, CAN and other standard interfaces
- High reliability
Application scenarios
-Intelligent excavation system in mining area
- Baseline inertial navigation for large UAVs
- marine compass
- self-propelled gun orientation
- Vehicle positioning and orientation
- High precision mobile measurement
- High precision and stable platform
- Baseline inertial navigation for large UAVs
- marine compass
- self-propelled gun orientation
- Vehicle positioning and orientation
- High precision mobile measurement
- High precision and stable platform
Electrical Characteristics
- Power supply: 24~36V DC (typ.)
- Rated power: 30W (max)
- Rated power: 30W (max)
Fiber optic gyroscope-Strapdown Inertial/Satellite Integrated Navigation System Mechanical Dimensions
Technical parameter:
| Attributes | Parameter | Index |
| Position hold | Odometer Combo | 0.001D (D is mileage) |
| GNSS combination | 1.2m | |
| Pure inertia | 0.8nmile/h | |
| Attitude accuracy | Initial alignment | 0.003° |
|
Attitude hold (GNSS disabled, pure inertia) |
0.002°/10min（RMS） | |
| Transient power | ≤100W (<3s) | |
| Heading accuracy | self-seeking north | 0.05°×sec(Lati), where Lati means latitude (RMS) |
|
Heading hold (GNSS disabled, pure inertia) |
0.003°/10min（RMS） | |
| Speed accuracy |
Speed hold (GNSS disabled, pure inertia) |
0.3m/s/10min（RMS） |
|
Optical fiber Gyro |
Measuring range | ±400°/s |
| Zero bias stability | ≤0.01°/h | |
| Quartz Flexible Accelerometer | Measuring range | ±20g |
| Zero bias stability | ≤20µg(10s average) | |
| Communication Interface | RS232 |
1 channel (baud rate 9.6kbps~921.6kbps, default 115.2kbps Frequency up to 1000Hz, default 200Hz) |
|
|
RS422 |
6 channels (Baud rate 9.6kbps~921.6kbps, default 115.2Kbps Frequency up to 1000Hz, default 200Hz) |
| Structural properties | Size | 199 mm × 180 mm × 219.5 mm (L×W×H) |
| Weight | A single set of inertial navigation is not more than 8.0kg (optional for aviation applications is not more than 6.5kg) | |
| Use environment | Storage temperature | -40℃~65℃ |
| Relative humidity | ≤80% |
Application example
Hot Tags: Fiber optic gyroscope-Strapdown Inertial/Satellite Integrated Navigation System, Manufacturers, Suppliers, Factory, China, Made in China, Customized, High Quality
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