FS300-42 Optical Fiber Integrated Navigation System
ACTUS INDEX
| Project | Test conditio | Index |
| Positioning accuracy | GNSS opera, a la biga | 1.5m |
| GNSS valet, RTK | 2cm+ppm | |
| Purissimum inertiae horizontalis situm (Alignment efficientiam) | 80m/5min.CEP. 500m/10min.CEP. 1.5nm/30min.CEP. | |
| Airspeed combination positioning positioning horizontales (in tabula adhibetur, et ante compositionem airspeed decurrere est. Testis velocitatis fugae 150km/h accipit exemplum et campus ventus stabilis est) | 0.8nm/30min (CEP) | |
| Scilicet accurate | Una antennae (RMS) | 0,1° (condiciones vehiculum, opus decurrere) |
| Antennae Dual (RMS) | 0.2 ° / L (L baseline longitudo) (RMS) | |
| Scilicet observatio (RMS) | 0.2°/30min.RMS.0.5°/h | |
| Self-quaerentes Septentrionalis accurationem (RMS) | 0.2° SecL, dual alignment pro 15min 1.0° SecL, unitas 5-10 minutes | |
| Habitus accurate | GNSS valid | 0.02°.RMS. |
| Habitus retentione (GNSS defectum) | 0.2°/30min.RMS.0.5°/h.RMS. | |
| Velocitas veritas | GNSS validum est, unum punctum L1/L2 | 0.1m/s.RMS. |
| Gyroscope | range mensuræ | ± 400°/s |
| Nulla bias stabilitatis | ≤0.3°/h | |
| Accelerometer | range mensuræ | ±20g |
| Nulla bias stabilitatis | ≤100µg | |
| Dimensiones physicae et notae electricae | Voltage | 9-36V DC |
| Potentia consummatio | ≤12W (stabilis) | |
| I Interface | 2 canalis RS232,1 alveus RS422,1 alveus PPS (LVTTL/422 level) | |
| Dimension | 92.0 mm×92.0mm×90.0mm | |
| Environmental notae | Operating Temperature | -40℃~+60℃ |
| Repono temperatus | -45℃~+70℃ | |
| Vibratio | 5~2000Hz, 6.06g (impulsa effusio) | |
| Impact | 30g, 11ms (cum effusio Concursores) | |
| vitae spatium | > XV annis | |
| Continua opus tempus | >24h |
