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Session 6. Session 8. Session 7. Session 1. Session 5. Session 4. Session 3. Session 2. Applications of the Fiber Optic Sagnac Interferometer. Blue Road Research. Sagnac Interferometer. Blue Road Research. Session 3, Page 1. Part I Rotation Sensing Part II
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Session 6 Session 8 Session 7 Session 1 Session 5 Session 4 Session 3 Session 2 Applications of the Fiber Optic Sagnac Interferometer Blue Road Research
Sagnac Interferometer Blue Road Research Session 3, Page 1 Part I Rotation Sensing Part II Quasi-Static and Time Varying Sensing
Rotation Sensor Characteristics Blue Road Research Session 3, Page 2 Rate Gyro = KV = Rotation rate K = Scale factor V = Output signal
Definition of Terms Blue Road Research Session 3, Page 3 • Rate integration gyro - Integrates angular rate to get angular output • Fixed bias - Output rotation rate with zero input rotation rate • Bias drift - Change in output rate over time (temperature, wear, etc.) • Scale factor - Linearity and hysteresis
Rotation Sensor Performance Factors Blue Road Research Session 3, Page 4 • Sensitivity • Lowest measurable rotation rate • Spectral noise characteristics • Dynamic range • Turn on time
The Sagnac Effect ccw cw cw path: 2R+ RL/c R ccw path: 2R - RL/c Net path difference: 2RL/c ZR = 2RL/(c) Blue Road Research Session 3, Page 5
The Sagnac Effect ccw cw ZFcw = (Fo+F)(Ln/c) F ZFccw = FoLn/c ZF = FLn/c Setting ZR = ZF Renders F = 2R/n Blue Road Research Session 3, Page 6
Fiber Optic Gyro Competition Blue Road Research Session 3, Page 7 • Mechanical Gyros • Advantages • Established industrial base • Disadvantages • Bearing wear • Start-up time • Reliability
Fiber Optic Gyro Competition Blue Road Research Session 3, Page 8 • Ring Laser Gyros • Advantages • Established industrial base • Replaced mechanical gyros for navigation • Disadvantages • Mechanical dither • Ultraclean vacuum tube technology
Fiber Optic Gyro Tradeoffs Blue Road Research Session 3, Page 9 • All solid state • Packing flexibility • Potentially very long lifetimes • Small size • Low cost
Ring Laser Gyro Assembly Partially transparent mirror Anode Cathode Blue Road Research Session 3, Page 10
Ring Laser Gyro Readout Optics cw beam ccw beam Split detector Rolling fringe pattern Blue Road Research Session 3, Page 11
Ring Laser Lock In Zone Blue Road Research Session 3, Page 12
Open Loop Fiber Optic Gyro Light source Polarizer Modulator Detector Fiber optic loop Blue Road Research Session 3, Page 13
Detection Signals Blue Road Research Session 3, Page 14
Open Loop Fiber Optic Gyro Output Blue Road Research Session 3, Page 15
Closed Loop Fiber Optic Gyro Fiber optic coil Light source Polarizer Modulator Detector Integrator Frequency shifter VCO Oscillator Blue Road Research Session 3, Page 16
Scale Factor Open loop fiber gyro Closed loop fiber gyro = ZR[c/2RL] = F(n/2R) Dependence on wavelength Blue Road Research Session 3, Page 17
Correction of Scale Factor -F F Blue Road Research Session 3, Page 18
First Closed Loop Fiber Optic Gyro Blue Road Research Session 3, Page 18A
First Solid State Fiber Optic Gyro Blue Road Research Session 3, Page 18B
2.5” 1980 Fiber Optic Gyro Blue Road Research Session 3, Page 18C
1982 Oil Drilling FOG Blue Road Research Session 3, Page 18C
1983 Closed Loop FOGs Blue Road Research Session 3, Page 18C
First Honeywell Production FOG Blue Road Research Session 3, Page 18C
Litton (NG) FOG IMU Blue Road Research Session 3, Page 18C
The Open Loop Fiber Optic Gyro Marketplace Blue Road Research Session 3, Page 19 • Automobiles and trucks • Pointing and tracking • Robot navigation • Aircraft attitude control • Short range air navigation
The Closed Loop Fiber Optic Gyro Marketplace Blue Road Research Session 3, Page 20 • Medium to long range aircraft • Spacecraft • Missiles • Launch vehicles • Platforms making rapid turns
FOG Manufacturers Blue Road Research Session 3, Page 21 • Hitachi • Closed loop automotive and low cost FOGs • Delivered over supports high end automobiles like Lexus navigators, thousands of units per year • Japan Aviation Electronics • Intermediate grade FOGs for Japan self-defense force, variety of commercial applications, soccer field grass cutters, cleaning robots, mini-crop spraying helicopters…
FOG Manufacturers (continued) Blue Road Research Session 3, Page 22 • Honeywell • Supplies 3 axis FOG navigator for German Dornier commuter aircraft, 777 back up navigator • Leader in commercial aircraft navigation and space based FOG • Northrup • 3 axis closed loop AHRS units with 0.1-1.0 deg/hr performance to full military specifications • Working on full navigation grade 0.01 deg/hr FOGs targets competing with Honeywell on commercial aircraft
FOG Manufacturers (continued) Blue Road Research Session 3, Page 24 • Mitsubishi Precision Company • Flight tested first space based FOG on Feb. 22, 1990 aboard S-520-11 rocket • Makes both open and closed loop FOGs • Photonetics • Closed loop 0.1 deg/hr FOGs to support ship navigation
Estimated FOG Market Size Blue Road Research Session 3, Page 26 • 1995 - $50,000,000 • 2000 - $100,000,000 • 2005 - $150,000,000 • Combination of commercial and military/government funded markets
Fiber Optic Gyro References Blue Road Research Session 3, Page 27 • S. Ezekiel and H.J. Arditty, Editors, “Fiber Optic Rotation Sensors”, Springer-Verlag, New York, 1982. • E. Udd, Editor, “Fiber Optic Gyros: 10th Anniversary Conference”, SPIE Proc., Vol. 719, 1986. • R.B. Smith, Editor, “Selected Papers on Fiber Optic Gyros”, SPIE Milestone Series, Vol. MS 8, 1989.
Fiber Optic Gyro References (continued) Blue Road Research Session 3, Page 28 • S. Ezekiel and E. Udd, “Fiber Optic Gyros: 15th Anniversary Conference”, SPIE Proc., Vol. 1585, 1991. • H. Lefevre, “The Fiber Optic Gyroscope”, Artech House, 1993. • W.K. Burns, Editor, “Optical Rotation Sensing”, Academic Press, 1994.
Part II Blue Road Research Session 3, Page 29 Quasi-Static and Time Varying Sensing Using the Fiber Optic Sagnac Interferometer
Time Varying Environmental Effects-Acoustics Light source Center Detector Acoustic Wave Blue Road Research Session 3, Page 30
Optimized Fiber Coil Configurations Variable coating Shielded Fiber Blue Road Research Session 3, Page 31
Effects of Shielding/Position Induced phase shift unshielded coil Induced phase shift shielded coil Blue Road Research Session 3, Page 32
Time Varying Effects Fiber Coil Length L dy y Response of Fiber G(y,P) Blue Road Research Session 3, Page 33
Example Cases Blue Road Research Session 3, Page 34 I. G(y,P) = A = Constant, R[P(t)] = 0 II. G(y,P) = 0, 0<y<L/2 G(y,P) = A = Constant, L/2<y<L, R[P(t)] = AnL2/4c]dP/dt for P = Bsin(t) R[P(t)] = [ABnL2/4c] sin(t)
Quasi-Static Sensing-Strain Polarizer Light source Fo+F Frequency shifter Detector Fo Blue Road Research Session 3, Page 35
Quasi-Static Sensing Blue Road Research Session 3, Page 36 ZF = F(Ln/c) Suppose ZF = Constant 0 = dF(Ln/c)+FdL(n/c) dF/F = -dL/L
Sagnac Strain Sensor Cabling Light source Detector Frequency shifter Fiber cable Blue Road Research Session 3, Page 37
Earth Movement Detection System Fault line Fiber cables Earth movement Blue Road Research Session 3, Page 38
Monitoring Oil Platform Motion Fiber optic strain sensor Blue Road Research Session 3, Page 39
Stress on Power Lines Fiber strain sensor surrounded by conductive cable elements Blue Road Research Session 3, Page 40
Distributed Sagnac Sensors Blue Road Research Session 3, Page 41 • Changing modes from time varying to quasi-static • Interlaced Sagnac loops • Combination of the Sagnac and Mach-Zehnder interferometers
Changing Mode Distributed Sensor Light source Fo Polarizer Switches Detector Fo+F Frequency shifter Blue Road Research Session 3, Page 42
Interlaced Sagnac Loops Light source, 2 Light source, 1 WDMs I Detector, 1 Detector, 2 Position Blue Road Research Session 3, Page 43
Sagnac/Mach-Zehnder Light source, 1 Sagnac Detector, 1 Mach-Zehnder Detector, 2 Light source, 2 Blue Road Research Session 3, Page 44