FS300-42 Optical Fiber Integrated Navigation System
Kev ua tau zoo INDEX
| Proj | Kev kuaj mob | Index ua |
| Positioning raug | GNSS ua haujlwm, a la carte | 1,5m ua |
| GNSS siv tau, RTK | 2 cm + 1 ppm | |
| Ntshiab inertial kab rov tav positioning (Alignment efficiency) | 80m / 5 feeb(CEP) 500m / 10 min(CEP) 1.5nm / 30 feeb(CEP) | |
| Airspeed sib xyaw ua ke kab rov tav txoj hauj lwm tuav (Nws yog siv rau ntawm lub nkoj, thiab muaj tig maneuver ua ntej airspeed ua ke. Qhov kev ntsuam xyuas yuav siv sij hawm 150km / h ya davhlau ceev raws li piv txwv, thiab cua teb yog ruaj khov) | 0.8nm/30min (CEP) | |
| Cov ntaub ntawv raug | Tib kav hlau txais xov (RMS) | 0.1 ° (Lub tsheb tej yam kev mob, yuav tsum tau maneuver) |
| Dual kav hlau txais xov (RMS) | 0.2 ° / L (L yog lub hauv paus ntev) (RMS) | |
| Course khaws cia (RMS) | 0.2 ° / 30 feeb(RMS),0.5 ° / h | |
| Kev nrhiav tus kheej sab qaum teb qhov tseeb (RMS) | 0.2 ° SecL, dual alignment rau 15 min 1.0 ° SecL, chav tsev rau 5-10 feeb | |
| Tus cwj pwm raug | GNSS siv tau | 0.02° Nws(RMS) |
| Kev tuav tswj tus cwj pwm (GNSS ua tsis tiav) | 0.2 ° / 30 feeb(RMS),0.5 ° / h(RMS) | |
| Kev nrawm nrawm | GNSS siv tau, ib qho taw qhia L1 / L2 | 0.1m / s(RMS) |
| Gyroscope | Kev ntsuas ntau | ± 400 ° / s |
| Zero bias stability | ≤0.3° / h | |
| Accelerometer | Kev ntsuas ntau | ± 20g |
| Zero bias stability | ≤100µg | |
| Lub cev qhov ntev thiab cov yam ntxwv hluav taws xob | Qhov hluav taws xob | 9-36V DC |
| Kev siv fais fab | ≤12W (kwv yees) | |
| I Interface | 2 channel RS232,1 channel RS422,1 channel PPS (LVTTL / 422 qib) | |
| Dimension | 92.0mm × 92.0mm × 90.0 hli | |
| Environmental yam ntxwv | Ua haujlwm kub | -40 ℃ ~ + 60 ℃ |
| Cia kub | -45 ℃ ~ + 70 ℃ | |
| Kev vibration | 5 ~ 2000Hz, 6.06g (nrog kev poob siab) | |
| Kev cuam tshuam | 30g, 11ms (nrog kev poob siab) | |
| Lub neej ntev | > 15 xyoo | |
| Lub sijhawm ua haujlwm tsis tu ncua | > 24 h |
