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Wuhan Joho Technology Co., Ltd.

Fiber Optic Gyro, Fiber Optic Vertical Gyro, Gyro manufacturer / supplier in China, offering Fiber Optic Vertical Gyro Ains-10, 8~14um Uncooled Thermal Imaging Core, Attitude and Azimuth Integrated Navigation System (Fiber Optic Vertical Gyro) and so on.

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Fiber Optic Vertical Gyro Ains-10

FOB Price: Get Latest Price
Min. Order: 1 Piece
Port: Wuhan, China
Production Capacity: 500 Units/Year
Payment Terms: T/T

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Basic Info
  • Model NO.: AINS-10
  • Trademark: Wuhan JOHO Technology
  • Specification: CE
  • HS Code: 90148000
  • Applications: Ship-Borne and Vehicle Borne Navigation
  • Transport Package: Safety Case
  • Origin: China
Product Description
Attitude and Azimuth Integrated Navigation System AINS-10

Featured with independent of outside information, excellent concealment, strong anti-interference, all weather operations, inertial navigation system is a complete autonomic navigation system which could provide diverse navigation parameters. However, its output error is accumulated along with time. Global position satellite (GPS) has higher navigation accuracy, but it is easy to be interfered, suffered from discontinuous output and incomplete output information etc. In order to integrate the advantages of these two navigation methods and effectively improve product performance, as well as strength product's reliability, availability, environment adaptability and dynamics, we utilizing multi-sensor data fusion technology to combine satellite positioning, orientation and inertial measurement, and release new attitude and position integration navigation system.

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
Range
Heading0~360°
Pitch angle90°
Roll angle180°
Position accuracy2cm+1ppm
Data
Output frequency100Hz
GPS data refresh rate5Hz
Data storage abilityStorage system able to continuous working 8h
Environment parameters
Working temperature-40~+60   centigrade 
Storage temperature-45~+70   centigrade 
Humidity95% (30  centigrade  )
Vibration5g (20Hz~2kHz, random), 30min
Shock30g (11ms, half-sine wave, 3 times for each axis)
Salt sprayMeet GJB150 standard for ship cabin usage
Reliability
MTBF2000h
Continuous working time≥12h
Physical parameters
System weight≤4.5kg (excluding antenna and feeder line)
Physical dimension170mm×160mm×166mm
Power supply
Power supply10-32VDC, 26W, (self Li-on battery able to work continuous 8h)
Fiber gyro
Null bias stability0.5°/hr (1σ)
Null bias repeatability0.5°/hr (1σ)
Random walk coefficient0.05°/√hr
Scale factory non-linearity100ppm (1σ)
Scale factory repeatability100ppm (1σ)
Dynamic range±300°/s
Quartz accelerometer
Bias<3mg
Current scale factor1.2±0.15 mA/g
Second-order nonlinear coefficient<50μg/g 2
Scale factor/ Temperature coefficient<30 ppm/  centigrade 
Bias month stability<50μg
Scale factor/month stability<30 ppm
Bias temperature coefficient<±50μg/  centigrade 
Shock30g 11ms 1/2sin
GPS
Positioning & orientation time
Positioning time typical value≤45s
Orientation time typical value≤60s
Reacquisition time<5s
Positioning & orientation accuracy
Heading accuracy0.1° (length of baseline 2m)
Pitch angle0.2° (length of baseline≥2m
Position accuracy2m CEP autonomous, no SA RTK 2cm+1ppm
Velocity accuracy0.02m/s
Timing accuracy50ns
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Ms. Tracey Chen
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