Hom 90 RLG inertial navigation system
PERMANCE Indicators
| System raug Qhov System raug | Pure Inertial Navigation / Ntshiab Inertial Navigation | 1.0nmile/4h, CEP | |
| Integrated Navigation/Navigation nrog GNSS | ≤5m, 1s _ | ||
| Lub taub hau lub taub hau / taub hau | 0.01°, RMS | ||
| Horizontal cwj pwm (yob thiab suab) Horizontal cwj pwm (roll & suab) | 0.005°, RMS | ||
| Ntshiab Inertial Velocity | 1.0 m/s, RMS | ||
| GNSSKev koom ua kenavigation Velocity | 0.1 m/s, RMS | ||
| Qhov taw qhia ntawm Inertial li Gyro thiab Accelerometer Parameters | laser gyroscope _ Gyroscope | Range/Xav | ± 600 ° / s |
| Bias Stability | ≤ 0.002 deg / h, 1s | ||
| Bias Repeatability | ≤ 0.002 deg / h, 1s | ||
| Scale Factor tsis-linearity | 1ppm ua | ||
| Accelerometer Accelerometer | Range/Xav | ± 15g | |
| Bias Stability | ≤10μg, 1s | ||
| Zero bias repeatability Bias Repeatability | ≤10μg, 1s | ||
| Scale Factor tsis-linearity | 15 ppm | ||
| teem sijhawm Lub Sijhawm Ua Haujlwm | Txias Pib | ≤ 15 feeb | |
| Re- Pib | ≤ 10 feeb _ | ||
| Air/In-Flight Start | ≤ 15 feeb | ||
| Lub sijhawm ua haujlwm Lub sijhawm ua haujlwm | Lub sijhawm ua haujlwm tsis tu ncua / Lub sijhawm ua haujlwm | ntau tshaj 10h | |
| Interface nta interface | Kev them nyiaj yug voltage / Voltage | 18 ~ 36VDC | |
| Kev siv fais fab | ≤ 40W @ 24VDC | ||
| Hluav taws xob interface / Hluav taws xob | RS232 × 2 RS422 × 3 TSI × 2 Ethernet × 1 1 npx x1 | ||
| Cov ntaub ntawv hloov tshiab tus nqi (configurable) | 200Hz@115.2kbps _ _ _ | ||
| Siv ib puag ncig Ib puag ncig | Ua haujlwm kub | -40 ° C ~ + 65 ° C | |
| Cia kub / Cia kub | -55 ° C ~ + 85 ° C | ||
| Siv Altitude/Altitude | 20000 m | ||
| Cov av noo | 95% (+ 25 ° C) | ||
| Kev vibration / vibration | 5g @ 20 ~ 2000Hz | ||
| Shock / poob siab | 40 g, 11 ms, 1/2 Sine | ||
| Lub cev muaj zog Lub cev | Dimensions / Loj (L * W * H) | 370 x ib275x 244 hli _ | |
| Nyhav/ Nyhav | 19kg ua | ||
Lus Cim: Cov qauv tuaj yeem hloov kho raws li tus neeg siv khoom xav tau.
