RLG Duo-Axis Indexing Inertial Navigationis
Depictio producti
RL2-90 Inertia Navigatio, acies solutionis certae navigationis.Genus 90 anuli laseris gyroscopi et vicus accelerometro flexibili instructus, accurate celeritatis, positionis et habitus notitias praebet.Inconsutibiliter integrat metris GNSS, altimetris et metris aereis velocibus, idoneos faciens vectoribus aere et terra.Utrum in lacus, vehicula armata, aircraft, fuci, naves, vel velocitas plenas rail, haec ratio certam fugae imperium, habitus stabilizationem et positiones efficit.Cum summa diligentia in tam pura navigatione inertiae ac modorum navigationis integratae, RL2-90 particeps tua est credita pro certa et accurata navigatione in variis applicationibus.
PRODUCT PARS
l Duo-axis indexing mechanism erroris mitigationem
l Princeps accurate anulus laser gyro et vicus accelerometer
l Libitum static vel movere basi auto-alignment
l Error parametri calibratiis et compensatio in plena temperatus range
l Libitum interfaces diversae initus pro GNSS/Odometer/DVL
l modos navigationis configurable
l optimum environmental convenientia
l signa militaria
APPLICATION Areas
l sub-maris vehiculum navigationis
l Positioning et a septentrione in terra vehiculum invenire
l Stabilization et imperium ad movens carrier
l Habitus mensurae postulandi applicationes
MAIN functiones
l Munus habet notitiarum outputationis ut tabellarius positio, caput, habitus angulus, rate angularis et celeritas in tempore reali;
l Modos laborat ut navigationem insitam puram et INS/GNSS (including Beidou) integratam navigationem;
l Possident munus recipiendi satellitem navigationis instructum ab externa temporis systema frequentia vexillum apparatum;
l Habet terram sui noctis et functionem noctis sustinet aeris;
l Habet functiones sicut potestatem experimenti sui, periodici sui ipsius probationis, status relationis, institutionis erroris excambium, ac non-volatile tabularium.
PERFORMANCE INDICATORS
| Ratio accurationis Ratio Accuracy | Pura Inertiae Navigation / pura Inertial Navigation | 2.0nmile/5d, PEAK | |
| Integrated Navigation / Navigation cum GNSS | ≤5m, 1σ | ||
| Petere angulus / Heading | 0.01°, RMS | ||
| Habitus horizontalis (volumen et picem) Habitus horizontalis (tortamque & picem) | 0.005°, RMS | ||
| Pura Inertia Velocitas | 1.0 m/s , RMS | ||
| GNSS Integrated navigation Velocity | 0. 1 m/s , RMS | ||
| Indicatores insita cogitationes Gyro et Accelerometer Parameters | Laser gyroscope _ Gyroscope | Range/Range | ± 6 00 deg/s |
| Bias Stability | ≤0.002 deg/h, 1σ | ||
| Bias Repeatability | ≤0.002 deg/h, 1σ | ||
| Scale Factor non-linearitatis | 1 ppm | ||
| Accelerometer Accelerometer | Range/Range | ± 15g | |
| Bias Stability | ≤10μg, 1σ | ||
| Nulla bias repeatability Bias Repeatability | ≤10μg, 1σ | ||
| Scale Factor non-linearitatis | 15 ppm | ||
| color tempore Gratia diei et noctis | Frigus Committitur | ≤ 15 min | |
| Re- Start | ≤ 10 min | ||
| Air/in-Fuga Committitur | ≤15min | ||
| Horas opus Operatio Tempus | Continua opus temporis / Operationis Tempus | plus quam 10h * | |
| Interface Features interface | Supple voltage/Voltage | 18~36VDC | |
| Potentia consummatio | ≤ 40W @ 24VDC | ||
| Electrical interface / Electrical | RS232 2 RS422 3 CAN 2 Aer 1 1pps 1 | ||
| Data Update Rate (configurable) | 200Hz@115.2kbps | ||
| Usus environment Environmental | Operating Temperature | -40°C~+65°C | |
| Repono temperatus / at Temperature | -55°C~+85°C | ||
| Usus Altitude / Altitude | 20000m | ||
| Umor | 95% (+25°C) | ||
| Vibratio/Vibratio | 5g @20~2000Hz | ||
| Inpulsa / Concursores | 40 g, 11 ms, 1/2 Sine | ||
| Corporalis proprietatibus Corporalis | Dimensiones/ Size (Φ*H) | 540 x 536mm | |
| Pondus / pondus | 55 kg | ||
Nota: Structura nativus secundum requisita usoris potest esse.
