Typus LXX LASER Strapdown Inertiae navigationis
Depictio producti
RL70 Navigatio Inertiae ratio summus perficientur est solutio in Typus 70 Ring Laser Gyroscope et Quartz Flexibilis Accelerometer.Inconsutilem cum GNSS, altimetris, et metris aeris velocitatibus integrat, accurate informationes navigationis praebet pro vectoribus aeris et terrae.Haec ratio aptum est lacus, vehicula armata, aircraft, fuci, naves, autocineta, velocitas plenas blasphemiae, vehicula inanibus, systematibus communicationis satellitibus et operationibus exercendis.Navigationem accuratam efficit cum CEP 0,6 nmile in puro modo inertiae et minus quam 5m in modo GNSS integrali.Systema accurationem eximiam praebet in angulo, positione horizontali (volumine et pice), velocitatem inertiam puram et velocitatem integratam GNSS.Cum fide et versatilitate sua, RL70 est optima electio pro variis applicationibus navigationis.
PRODUCT PARS
l Anulus laser gyro medius gradus et vicus accelerometer
l Libitum static vel movens basim auto-alignmentError parametri calibrationis et excambium 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 Mare navigation vehiculum
l Sub aqua vehiculum navigationis et positioning
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 | 0.6 nmile/1h, CEP | |
| Integrated Navigation / Navigation cum GNSS | ≤5m , 1σ _ | ||
| Petere angulus / Heading | 0.03°, RMS | ||
| Habitus horizontalis (volumen et picem) Habitus horizontalis (tortamque & picem) | 0.006°, RMS | ||
| Pura Inertia Velocitas | 1 .5 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 | ≤0.005 deg/h, 1σ | ||
| Nulla bias repeatability Bias Repeatability | ≤0.005 deg/h, 1σ | ||
| Scale Factor non-linearitatis | 5 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 | ≤ 8 min | |
| Re- Start | ≤ 5min _ | ||
| Air/in-Fuga Committitur | ≤10min | ||
| 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 (L*W*H) | 140 x 233 x 112 mm _ | |
| Pondus / pondus | 3 kg | ||
Nota: Structura nativus secundum requisita usoris potest esse.
