FOB Price
Get Latest Price350 ~ 450 USD / Piece
|1 Piece Minimum Order
Country:
China
Model No:
SKU RLG-GD70A
FOB Price:
350 ~ 450 USD / Piece Get Latest Price
Place of Origin:
Chengdu, China
Price for Minimum Order:
350 per Piece
Minimum Order Quantity:
1 Piece
Packaging Detail:
Shockproof packaging
Delivery Time:
15 days~45 days
Supplying Ability:
500 Piece per Day
Payment Type:
Western Union, D/P, L/C, T/T
Product Group :
China
Contact Person Devin
Chengdu, Sichuan
RLG-GD*0A 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 | 0.6 nmile/1h, CEP | ||||||||||||||||||||||
Integrated Navigation/Navigation with GNSS | ≤5m , 1σ _ | |||||||||||||||||||||||
Heading angle /Heading | 0.*3°, RMS | |||||||||||||||||||||||
Horizontal attitude (roll and pitch )
Horizontal Attitude (roll & pitch) |
0.**6°, RMS | |||||||||||||||||||||||
Pure Inertial Velocity | 1 .5 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.**5 deg/h, 1σ | |||||||||||||||||||||||
Zero bias repeatability
Bias Repeatability |
≤0.**5 deg/h, 1σ | |||||||||||||||||||||||
Scale Factor non-linearity | 5 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 | ≤ 8 min | ||||||||||||||||||||||
Re-Start | ≤ 5min _ | |||||||||||||||||||||||
Air/In-Flight Start | ≤*0min | |||||||||||||||||||||||
Working hours
Operation Time |
Continuous working time/Operation Time | more than *0h | ||||||||||||||||||||||
Interface Features
interface |
Supply voltage/Voltage | *8~*6VDC | ||||||||||||||||||||||
Power Consumption | ≤ *@********************/td> | |||||||||||||||||||||||
Electrical interface/Electrical |
RS**2 × 2
RS**2 × 3 CAN × 2 Ethernet × 1 1pps × 1 |
|||||||||||||||||||||||
Data Update Rate (configurable) |
**0Hz
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