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Contents
Long term navigation key parameter
FOG principle
Key orders of magnitude
Key features
Comparison with other technologies
IXBLUE catalog examples
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Earth rotation vector module error
Composite bias : bias + effect of scale factor error on
moduleComposite bias
Earth Rotation
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Earth rotation vector module error
Composite bias : bias + effect of scale factor error on
moduleComposite bias
Earth Rotation
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FOG - Sagnac effect
Digital Signal
Processing
COIOptical
source
Optical
Coupler
« All-Digital »
Processing
Function
Modulation
Module
Optical Fiber
Coil
Optical
detector
Detection
Module
Digital Signal
Processing
« All-Digital »
Processing
Function
Modulation
Module
Optical
detector
Detection
Module
NO ROTATION
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FOG - Sagnac effect
Digital Signal
Processing
COIOptical
source
Optical
Coupler
« All-Digital »
Processing
Function
Modulation
Module
Optical Fiber
Coil
Optical
detector
Detection
Module
Digital Signal
Processing
« All-Digital »
Processing
Function
Modulation
Module
Optical
detector
Detection
Module
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Some interesting orders of magnitude
Best present results for fiber gyro :
Wavelength : l = 1550 nm
Fiber length L few km few 109 l
Bias stability : 0.001 deg/h over 28 deg/second (p phase shift) i.e. 10-8 of the wavelength
Relative detection of optical path length : few 10-18 !
With a relative variation of 7 x 10-6 / ºC for light velocity in the silica fiber !
RECIPROCITY (perfect common-mode rejection)
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Actual configuration of a fiber gyro
Polarization-preserving fiber coil with typically 100 m to 10 km (manufactured by iXBlue).
Proton-exchanged LiNbO3 integrated-optic circuit very high polarizer rejection (manufactured by
iXBlue).
Y-junction and pair of push-pull low-voltage phase modulators.
Broad-spectrum source : unpolarized erbium ASE source for best performance (manufactured by
iXBlue).
All-digital processing electronics (invented by iXblue).
Fiber
Coil
Broadband Light
Source
Coupler
Multi-function
IOC
Detector
A
/
D
Digital
LogicsD
/
A
Rotation signal
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FOG comparison with other technologies
FOG has no lock-in zone
Always true in open-loop design.
In closed loop design, no dead zone in principle, but a “dead zone “ may appear
if electronics design is not perfect (cross talk between modulation & detection
chains)
In RLG (Ring Laser Gyro), lock-in is by-passed with dithering : this increases
ARW, and provides acoustic noise
FOG has not (yet ?) reached a performance limit , while RLG faces a “non
reciprocity”
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FOG is easily scalable
QUADRANSOCTANS
AHRS
PHINS
INS
MARINS
INS
IMU 50 IMU 90 IMU 120 IMU 200
Average Diameter (mm) 45 68 94 171
Bias Stability* (°/h) 0,05 0,025 0,01 0,001
Typical ARW (10-4 °/√h) 60 35 10 2
* Bias stability over the temperature range, -10 to +80°C à 1 σ
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FOG 50 APPLICATIONS
Marine and Navy IMO gyrocompass
Land survey, stabilization
Military land navigation
Airborne survey
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FOG 90
OCTANS
ADVANS
LANDINS
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FOG 90 APPLICATIONS
Navy & marine gyrocompass
Land survey
Military land navigation
Artillery (qualified on 105 mm gun)
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FOG 120 APPLICATIONS
Navy & Marine navigation system
Land military navigation
Artillery (on 155 mm gun)
Airborne survey
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CONCLUSION
FOG technology is very reliable, very robust and has extremely long life time
44 FOG axes are on orbit around Earth cumulating more than 9300000
hours (106 years) without failure
FOG technology provides navigation for many marine applications :
Reliable and no maintenance gyrocompass,
Low power consumption inertial navigation system (especially suitable for AUV)
High performance navigation system for surface vessels and submarines