离岸价格
Get Latest Price350 ~ 450 / Piece
|1 Piece Minimum Order
国:
China
モデル番号:
SKU RLG-GD70A
离岸价格:
350 ~ 450 / Piece Get Latest Price
ロケーション:
Chengdu, China
最低注文量の価格:
350 per Piece
最低注文量:
1 Piece
パッケージの詳細:
Shockproof packaging
納期:
15 days~45 days
供給能力:
500 Piece per Day
支払いタイプ:
Western Union, D/P, L/C, T/T
製品グループ :
China
連絡先担当者 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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