Product Features FS100 fiber optic 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.
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% |
