Hom 50 RLG inertial navigation system
PERMANCE Indicators
System raug Qhov System raug | Pure Inertial Navigation / Ntshiab Inertial Navigation | 0.8 nmile/1h, CEP | |
Integrated Navigation/Navigation nrog GNSS | ≤5m, 1s _ | ||
Lub taub hau lub taub hau / taub hau | 0.05°, RMS | ||
Horizontal cwj pwm (yob thiab suab) Horizontal cwj pwm (roll & suab) | 0.01°, RMS | ||
Ntshiab Inertial Velocity | 1.5 m/s, RMS | ||
GNSS Integrated navigation 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 | ≤ 0.01 deg / h, 1s | ||
Zero bias repeatability Bias Repeatability | ≤ 0.01 deg / h, 1s | ||
Scale Factor tsis-linearity | 10 ppm | ||
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 | ≤ 8 min | |
Rov pib dua | ≤ 5 feeb _ | ||
Air/In-Flight Start | ≤ 10 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) | 240 x 202 x 169 hli | |
Nyhav/ Nyhav | 9kq ua |
Lus Cim: Cov qauv tuaj yeem hloov kho raws li tus neeg siv khoom xav tau.