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Aircraft Flight Control Fiber Optic Gyroscope GPS Position And Orientation System
Aircraft Flight Control Fiber Optic Gyroscope GPS Position And Orientation System
Aircraft Flight Control Fiber Optic Gyroscope GPS Position And Orientation System
Aircraft Flight Control Fiber Optic Gyroscope GPS Position And Orientation System
Specifications
Brand Name :
JOHO
Model Number :
AINS-20
Place of Origin :
CHINA
MOQ :
1set
Price :
Negotation
Payment Terms :
L/C, T/T
Supply Ability :
100Sets/year
Delivery Time :
15days
Packaging Details :
Standard Packing
Type :
Fiber Optic Vertical Gyro
Headig Accuracy(GPS Valid) :
0.1deg (Length of Baseline 2m)
Attitude (GPS Valid) :
0.05deg
Position Accuracy (GPS Valid) :
3m (Cep) , 2cm+1ppm(Cep) (Post-Differentiation)
Continuous Working Time :
12h
Applications :
Aircraft Flight Control and Navigation
Export Markets :
Global
Heading :
0~360°,
Description

Aircraft Flight Control Fiber Optic Gyroscope GPS Position And Orientation System

Employing high accuracy FOG, Q-flex accelerometers, dual-frequency GPS position & orientation system, barometric altimeter and advanced integration navigation and attitude measurement algorithm, the performance of Attitude and Azimuth Integrated Navigation Fiber Optic Vertical Gyro has been dramatically improved. Combining built-in high accuracy IMU (inertial measurement unit) with satellite, it could output high accuracy position, speed, attitude, angular speed and acceleration information. While the satellite signal is completely covered, system would enter into pure inertial mode. By use of high accuracy FOG, it could still keep good attitude measurement accuracy in certain time. Integrated with barometric altimeter, it could make correction and get higher accuracy height information.


Application


Aircraft flight control and navigation
Ship-borne & vehicle-borne navigation system
Inertial stability control system
E-traffic measurement system
Industrial & agricultural measurement and application


Technical Specifications

Range
Heading 0~360°,
Pitch angle ±90°
Roll angle ±180°
Angular rate ±300°/s
Acceleration ±10g
Positioning & orientation accuracy
Heading accuracy (GPS valid) 0.1° (length of baseline 2m, 1σ)
Attitude (GPS valid) 0.05° (1σ)
Position accuracy (GPS valid) 3m (CEP) , 2cm+1ppm(CEP) (post-differentiation)
Velocity accuracy (GPS valid) 0.1m/s (rms), (1σ)
Preparation time
Start time ≤10s
Stable time System working normally after GPS and heading valid (specified time depends on surrounding environment, open field 2min)
Power supply
Power supply DC12~32V, 24V±10% (rating)
Power consumption ≤25W
Reliability
MTBF 2000h
Continuous working time ≥12h
Physical parameters
System weight ≤3.6kg (excluding antenna and feeder line)
Physical dimension 191mm×166mm×131.5mm (X, Y, Z)
Product tags

navigation gyroscope

,

configuration digital tilt sensor

,

steering angle sensor
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Aircraft Flight Control Fiber Optic Gyroscope GPS Position And Orientation System

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Product Detail
Brand Name :
JOHO
Model Number :
AINS-20
Place of Origin :
CHINA
MOQ :
1set
Price :
Negotation
Payment Terms :
L/C, T/T
Contact Supplier
Aircraft Flight Control Fiber Optic Gyroscope GPS Position And Orientation System
Aircraft Flight Control Fiber Optic Gyroscope GPS Position And Orientation System

Wuhan JOHO Technology Co., Ltd

Verified Supplier
10 Years
hubei, wuhan
Since 2012
Business Type :
Manufacturer, Exporter, Seller
Main Products :
Electro Optical Tracking System, Electro Optical Sensor System, Electro Optical Targeting System
Total Annual :
10,000,000-20,000,000
Employee Number :
40~99
Certification Level :
Verified Supplier
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