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Fiber optic gyroscope-Attitude measurement system
  • Fiber optic gyroscope-Attitude measurement systemFiber optic gyroscope-Attitude measurement system
  • Fiber optic gyroscope-Attitude measurement systemFiber optic gyroscope-Attitude measurement system

Fiber optic gyroscope-Attitude measurement system

JIO-FOG100A Fiber optic gyroscope-Attitude measurement system is a triaxial of freedom attitude based on micro-mechanical technology (MEMS) Measurement system, built-in high-performance MEMS gyroscope and MEMS accelerometer, through the filtering algorithm calculates the pitch angle, roll angle and heading angle of the carrier in real time.

Model:JIO-FOG100A

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Product Description

Optionally matched with a magnetometer to achieve high-precision north finding, and output 3-axis angular velocity and 3-axis acceleration is used for motion control.
JIOPTICS offers a full Fiber optic gyro product suite serving a broad range of requirements from tactical to navigation grade.
JIOPTICS installation of fiber optic gyroscope to provide ease of integration flexibility, and our developers toolkit to rapid prototyping, not only meet the specification requirements, also provide high-quality performance meet the demand of end users.

Our services

JIOPTICS is a professional and efficient team. Provide OEM/ODM services for you, contact us to customize your exclusive fiber optical gyroscope

Product Characteristic

- Better than 0.1° attitude accuracy
- Attitude measurement range ±90°
- Operating temperature range: -40~65℃
- Vibration environment: 10~2000Hz, 6g (RMS)
- Rich interface types, support RS232, RS422, CAN and other standard interfaces
- Waterproof seal design

Electrical Characteristics

- Power supply: 5V (typ.), customizable wide voltage input 12~36V
- Rated power: 0.5W (max)
- Ripple: 100mV (peak-to-peak)

Mechanical Dimensions



Fiber optic gyroscope-Attitude measurement system Technical parameters

Parameter Test Conditions Typical value Max value Unit
Dynamic measurement range

450 º/s
Zero bias stability Allan variance, Z axis 0.8
º/h
Allan variance, X-axis and Y-axis 1.6
º/h
10s average, X, Y axis (-40℃~+80℃, constant temperature) 6
º/h
1s average, X, Y axis (-40℃~+80℃, constant temperature) 9
º/h
Zero offset Zero offset range ±0.2
º/s
Zero bias change over the full temperature range ±0.06
º/s
Start-to-start repeatability 0.006
º/s
Day-to-day start repetition 0.009
º/s
Influence of Linear Acceleration on Zero Bias 0.002
º/s
The influence of vibration on zero offset, the change before and after vibration 0.002
º/s
The influence of vibration on zero offset, the change before vibration 0.002
º/s
Scale Factor Scale factor accuracy, Z axis 0.3
%
Scale factor accuracy, X, Y axis 0.6
%
Scale factor nonlinearity, Z axis 0.01
%FS
Scale factor nonlinearity, X, Y axis 0.02
%FS
Angle random walk
0.001
°/√hr
Noise density
0.001
°/s/√hr
Resolution
3.052×10−7
º/s/LSB
Bandwidth
200
Hz

Accelerometer parameters

Parameter Test conditions Typical value Max value Unit
Dynamic measurement range
16
g
Zero bias stability Allan variance 0.03
mg
10s average (-40℃~+80℃, constant temperature) 0.2
mg
1s average (-40℃~+80℃, constant temperature) 0..3
mg
Zero offset Zero offset range 5
mg
Zero offset variation (peak-to-peak) over the full temperature range 5
mg
Start-to-start repeatability 0.5
mg
Day-to-day start repetition 0.8
mg
Zero Bias Temperature Coefficient 0.05 0.1 mg/℃
Scale factor Scale factor accuracy 0.5
%
Scale factor nonlinearity 0.1
%FS
Speed random walk
0.029
m/s/√hr
Noise density
0.025
mg/√Hz
Resolution
1.221×10−8
g/LSB
Bandwidth
200
Hz

Magnetometer parameters (optional)

Parameter Test conditions Typical value Max value Unit
Dynamic measurement range
2.5
gauss
Zero offset Non-magnetic environment 15
mgauss

Heading accuracy

Parameter Test conditions Typical value Max value Unit
Magnetic heading accuracy
0.5
°

Horizontal attitude accuracy

Parameter Test conditions Typical value Max value Unit
Pitch angle accuracy
0.1
°
Roll angle accuracy
0.1
°

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