Prix FOB
Obtenir le dernier prix350 ~ 450 USD / Piece
|1 Piece Minimum Order
Pays:
China
N ° de modèle:
SKU RLG-GD90B
Prix FOB:
350 ~ 450 USD / Piece Obtenir le dernier prix
Localité:
Chengdu, China
Prix de commande minimale:
350 per Piece
Commande minimale:
1 Piece
Packaging Detail:
Shockproof packaging
Heure de livraison:
15 days~45 days
Capacité de Fournir:
500 Piece per Day
Payment Type:
Western Union, D/P, L/C, T/T
Groupe de produits :
China
Personne àcontacter Devin
Chengdu, Sichuan
RLG-GD*0CÂ inertial navigation system is an inertial navigation system based on type *0 ring laser gyroscope and quartz flexible accelerometer. It can be combined with auxiliary equipment such as GNSS, altimeter, airspeed meter, etc., and can provide air carrier, ground carrier, etc. Navigation information such as speed, position, and attitude.
The Type *0 series inertial navigation system can be widely used in carrier platforms such as tanks, various types of armored vehicles, self-propelled artillery, rockets, various types of aircraft, drones, ships, automobiles, high-speed rail, unmanned vehicles, mobile satellite communication systems, and drilling. Flight control, attitude stabilization, weapon stabilization platform, positioning and orientation, etc.
System accuracy
System Accuracy |
Pure Inertial Navigation/Pure Inertial Navigation | 2.0nmile/5d, Â PEAK | ||||||||||||||||||||||
Integrated Navigation/Navigation with GNSS | ≤5m , 1σ _ | |||||||||||||||||||||||
Heading angle /Heading | 0.*1°, RMS | |||||||||||||||||||||||
Horizontal attitude (roll and pitch )
Horizontal Attitude (roll & pitch) |
0.**5°, RMS | |||||||||||||||||||||||
Pure Inertial Velocity | 1.0 m/s , RMS | |||||||||||||||||||||||
GNSS Integrated navigation Velocity | 0. 1 m/s , RMS | |||||||||||||||||||||||
Indicators of
inertial devices Gyro and Accelerometer Parameters |
laser gyroscope _
Gyroscope |
Range/Range | ± 6 *0 deg/s | |||||||||||||||||||||
Bias Stability | ≤0.**2 deg/h, 1σ | |||||||||||||||||||||||
Bias Repeatability | ≤0.**2 deg/h, 1σ | |||||||||||||||||||||||
Scale Factor non-linearity | 1 ppm | |||||||||||||||||||||||
Accelerometer
Accelerometer |
Range/Range | ± *5g _ | ||||||||||||||||||||||
Bias Stability | ≤*0μg , 1σ | |||||||||||||||||||||||
Zero bias repeatability
Bias Repeatability |
≤*0μg , 1σ | |||||||||||||||||||||||
Scale Factor non-linearity | *5 ppm | |||||||||||||||||||||||
align time
Alignment Time |
Cold Start | ≤ *5 min | ||||||||||||||||||||||
Re-Start | ≤ *0 min _ | |||||||||||||||||||||||
Air/In-Flight Start | ≤*5min | |||||||||||||||||||||||
Working hours
Operation Time |
Continuous working time/Operation Time | more than *0h | ||||||||||||||||||||||
Interface Features
interface |
Supply voltage/Voltage | *8~*6VDC | ||||||||||||||||||||||
Power Consumption | ≤ *@******************** | |||||||||||||||||||||||
Electrical interface/Electrical |
RS**2 × 2
RS**2 × 3 CAN × 2 Ethernet × 1 1pps × 1 |
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Data Update Rate (configurable) |
**0Hz
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