RLG Single-Axis Indexing Inertial Navigationis
Depictio producti
RL1-90 Navigatio Inertia Ratio versatilis et certa est solutio navigationis.Type 90 Ring Laser Gyroscope et Quartz Flexibile Accelerometer coniungit ut accurate informationes navigationis, inclusa velocitate, positione et habitudine, coniungat.Systema compagem integrat cum instrumentis auxiliaribus ut GNSS, altimetris et metris air- citis, necessitatibus portantium aeris et terrae praebens.
Haec ratio latas applicationes invenit per varias tabulas tabellariorum, inclusas lacus, vehicula armata, aircraft, fuci, naves, autocineta, alta velocitate railia, vehicula inanibus, systematis communicationis satellitum mobiles et operationes exercendas.Certam potestatem praebet fugae, habitus stabilizationis, arma stabilizationis suggestorum, positio, orientationis.
Cum progressu technologiae ac robusto consilio, RL1-90 Navigatio Inertiae Systema certa electio est ad occurrendum requisita navigationis in variis industriis et applicationibus.
PRODUCT PARS
l Sing-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/3d, 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) | ≤ 346 x 435 mm | |
| Pondus / pondus | 45 kg | ||
Nota: Structura nativus secundum requisita usoris potest esse.
