RLG Ib-Axis Indexing Inertial Navigation System
Khoom piav qhia
RL1-90 Inertial Navigation System yog ntau yam thiab txhim khu kev qha navigation tov.Nws txuas nrog Hom 90 Ring Laser Gyroscope thiab Quartz Flexible Accelerometer kom xa cov ntaub ntawv qhia tseeb, suav nrog kev ceev, txoj haujlwm, thiab tus cwj pwm.Lub kaw lus seamlessly integrates nrog auxiliary cuab yeej xws li GNSS, altimeters, thiab airspeed meters, catering rau cov kev xav tau ntawm huab cua thiab av nqa.
Cov kab ke no pom cov ntawv thov dav dav thoob plaws ntau lub chaw nqa khoom, suav nrog cov tso tsheb hlau luam, tsheb tub rog, dav hlau, drones, nkoj, tsheb, tsheb ciav hlau ceev, tsheb tsis siv neeg, tsheb sib txuas lus satellite, thiab kev ua haujlwm drilling.Nws muaj kev tswj xyuas meej ntawm kev ya davhlau, tus cwj pwm stabilization, riam phom stabilization platforms, qhov chaw, thiab kev taw qhia.
Nrog nws cov thev naus laus zis thiab kev tsim qauv zoo, RL1-90 Inertial Navigation System yog qhov kev xaiv txhim khu kev qha rau kev ua kom tau raws li qhov yuav tsum tau ua hauv kev lag luam thiab kev siv ntau yam.
PROUGT NTA
l Sing-axis indexing mechanism rau kev ua yuam kev mitigation
l High precision nplhaib laser gyro thiab quartz accelerometer
l Kev xaiv zoo li qub lossis txav puag ncig nws tus kheej ua kom zoo
l Kev tsis ua yuam kev calibration thiab them nyiaj nyob rau hauv tag nrho cov kub ntau yam
l Kev xaiv sib txawv input interfaces rau GNSS / Odometer / DVL
l Configurable navigation hom
l Zoo heev ib puag ncig haum
l Cov qauv tub rog
ATSEEM CEEB
l Kev tsav tsheb hauv qab hiav txwv
l Txoj hauj lwm thiab sab qaum teb-nrhiav rau av tsheb
l Stabilization thiab tswj kev txav cov cab kuj
l Kev ntsuas tus cwj pwm rau kev thov kev thov
MAIN FUNCTIONS
l Nws muaj kev ua haujlwm ntawm kev tso tawm cov ntaub ntawv xws li cov chaw nqa khoom, lub taub hau, lub kaum ntse ntse, tus nqi qis thiab ceev hauv lub sijhawm;
l Nws muaj cov qauv ua haujlwm xws li kev ua haujlwm ntshiab inertial thiab INS / GNSS (xws li Beidou) kev sib xyaw ua ke;
l Muaj cov haujlwm tau txais cov ntaub ntawv satellite navigation muab los ntawm lub sijhawm sab nraud system zaus cov khoom siv;
l Nws muaj kev ua haujlwm ntawm kev ua haujlwm hauv av nws tus kheej thiab txhawb kev ua haujlwm ntawm huab cua sib dhos;
l Nws muaj kev ua haujlwm xws li kev ntsuas hluav taws xob ntawm tus kheej, ntsuas tus kheej ib ntus, daim ntawv qhia txog xwm txheej, kev them nyiaj ua yuam kev, thiab kev cia tsis hloov pauv.
PKEV PAB CUAM
| System raug Qhov System raug | Pure Inertial Navigation / Ntshiab Inertial Navigation | 2.0nmile/3d, PEB | |
| 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 | ||
| 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 | ≤ 0.002 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 | |
| Rov pib dua | ≤ 10 min | ||
| 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 (Φ * H) | ≤ 346 x 435 mm | |
| Nyhav/ Nyhav | 45kg ua | ||
Lus Cim: Cov qauv tuaj yeem hloov kho raws li tus neeg siv khoom xav tau.
