anisoplanatic wavefront error estimation using coherent imaging

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1 © 2009 Lockheed Martin Corporation. All Rights Reserved. Anisoplanatic Wavefront Error Estimation using Coherent Imaging Anisoplanatic Wavefront Error Estimation using Coherent Imaging Rick Kendrick 1 , Joe Marron 2 , Bob Benson 1 1 Lockheed Martin Advanced Technology Center Palo Alto, California 2 Lockheed Martin Coherent Technologies Louisville, Colorado Rick Kendrick 1 , Joe Marron 2 , Bob Benson 1 1 Lockheed Martin Advanced Technology Center Palo Alto, California 2 Lockheed Martin Coherent Technologies Louisville, Colorado 15 th Coherent Laser Radar Conference June 2009

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Page 1: Anisoplanatic Wavefront Error Estimation using Coherent Imaging

1© 2009 Lockheed Martin Corporation. All Rights Reserved.

Anisoplanatic Wavefront Error Estimation using Coherent Imaging

Anisoplanatic Wavefront Error Estimation using Coherent Imaging

Rick Kendrick1, Joe Marron2, Bob Benson1

1Lockheed Martin Advanced Technology CenterPalo Alto, California

2Lockheed Martin Coherent TechnologiesLouisville, Colorado

Rick Kendrick1, Joe Marron2, Bob Benson1

1Lockheed Martin Advanced Technology CenterPalo Alto, California

2Lockheed Martin Coherent TechnologiesLouisville, Colorado

15th Coherent Laser Radar ConferenceJune 2009

Page 2: Anisoplanatic Wavefront Error Estimation using Coherent Imaging

2© 2009 Lockheed Martin Corporation. All Rights Reserved.

Page 3: Anisoplanatic Wavefront Error Estimation using Coherent Imaging

3© 2009 Lockheed Martin Corporation. All Rights Reserved.

Previous CLRC PapersPrevious Previous CLRCCLRC PapersPapers

Novel Multi-Aperture 3D Imaging SystemsJ.C. Marron, R. L. Kendrick*, T. A. Höft, and N. Seldomridge

Lockheed Martin Coherent Technologies135 South Taylor Ave.Louisville, CO 80027

Page 4: Anisoplanatic Wavefront Error Estimation using Coherent Imaging

4© 2009 Lockheed Martin Corporation. All Rights Reserved.

AnisoplanatismAnisoplanatismAnisoplanatism

Local Oscillator

Page 5: Anisoplanatic Wavefront Error Estimation using Coherent Imaging

5© 2009 Lockheed Martin Corporation. All Rights Reserved.

AgendaAgendaAgenda

• Bar Target Imaging Experiment• Data Analysis Process• Anisoplanatism• Point Source Array Experiment• Comparison to closed form calculation• Depth of focus demonstration• Summary

•• Bar Target Imaging ExperimentBar Target Imaging Experiment•• Data Analysis ProcessData Analysis Process•• AnisoplanatismAnisoplanatism•• Point Source Array ExperimentPoint Source Array Experiment•• Comparison to closed form calculationComparison to closed form calculation•• Depth of focus demonstrationDepth of focus demonstration•• SummarySummary

Page 6: Anisoplanatic Wavefront Error Estimation using Coherent Imaging

6© 2009 Lockheed Martin Corporation. All Rights Reserved.

Table Mountain Test RangeTable Mountain Test RangeTable Mountain Test Range

Target StandTarget Stand Imaging SystemImaging System100 meters100 meters

1.2 meter beam height1.2 meter beam height

Page 7: Anisoplanatic Wavefront Error Estimation using Coherent Imaging

7© 2009 Lockheed Martin Corporation. All Rights Reserved.

Sensor ArrangementSensor ArrangementSensor Arrangement

ScintecScintec ScintillometerScintillometer

Active ImagerActive Imager

Page 8: Anisoplanatic Wavefront Error Estimation using Coherent Imaging

8© 2009 Lockheed Martin Corporation. All Rights Reserved.

Cn2 = 6.5e-13L=100 m

Typical Scintillometer ReadingTypical Typical ScintillometerScintillometer ReadingReading

Sunny, Cloudless day with Little windSunny, Cloudless day with Little wind

Page 9: Anisoplanatic Wavefront Error Estimation using Coherent Imaging

9© 2009 Lockheed Martin Corporation. All Rights Reserved.

Data analysis stepsData analysis stepsData analysis steps

2004006008001000

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2004006008001000

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Image Plane: Sharpness = 1.2122

20406080100120

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16 pupil images16 pupil images

Fringes from LO Fringes from LO interferenceinterference

FFTFFT

FFTFFT

Complex Object Complex Object InformationInformation

Complex Pupil Complex Pupil Function Function ++

Maximize Sharpness by adding phase estimateMaximize Sharpness by adding phase estimate(48 (48 ZernikesZernikes))

FFTFFT

FFTFFT

Calculate SharpnessCalculate SharpnessΣΣ(Intensity(Intensity 22))

Final ImageFinal Image

Page 10: Anisoplanatic Wavefront Error Estimation using Coherent Imaging

10© 2009 Lockheed Martin Corporation. All Rights Reserved.

Set: 1244

Cn2 = 5.11 e-13

r0 = 0.0083

Iso patch= 0.0046

Fixed Aberrations Fixed Aberrations RemovedRemoved

Atmospheric Atmospheric Aberrations Aberrations

RemovedRemoved

Set: 1451

Cn2 = 5.51 e-14

r0 = 0.0317

Iso patch= 0.0176

Set: 1544

Cn2 = 6.0 e-15

r0 = 0.120

Iso patch= 0.0666

D= 50 mmD= 50 mmWavelength = 532 nmWavelength = 532 nm16 speckle realizations16 speckle realizationsTarget moved for each Target moved for each realizationrealization

Page 11: Anisoplanatic Wavefront Error Estimation using Coherent Imaging

11© 2009 Lockheed Martin Corporation. All Rights Reserved.

AnisoplanatismAnisoplanatismAnisoplanatism

Region over which the sharpness metric is maximizedRegion over which the sharpness metric is maximized

Set: 1244

Cn2 = 5.11 e-13

r0 = 0.0083

Iso patch= 0.0046

MTFMTF = 0.26= 0.26 MTFMTF = 0.43= 0.43 MTFMTF = 0.61= 0.61

Page 12: Anisoplanatic Wavefront Error Estimation using Coherent Imaging

12© 2009 Lockheed Martin Corporation. All Rights Reserved.

Point Source ArrayPoint Source ArrayPoint Source Array

• Retro Array is on 20 mm centers– 12.7 mm diameter

•• Retro Array is on 20 mm centersRetro Array is on 20 mm centers–– 12.7 mm diameter12.7 mm diameter

Page 13: Anisoplanatic Wavefront Error Estimation using Coherent Imaging

13© 2009 Lockheed Martin Corporation. All Rights Reserved.

Point Source Array Point Source Array Point Source Array

Raw DataRaw Data Sharpened for one Sharpened for one field pointfield point

Page 14: Anisoplanatic Wavefront Error Estimation using Coherent Imaging

14© 2009 Lockheed Martin Corporation. All Rights Reserved.

Phase Versus SeeingPhase Versus SeeingPhase Versus Seeing

• Cosine of the (phase difference )^2•• Cosine of the (phase difference )^2Cosine of the (phase difference )^2

(14:46)(14:46)rroo =5.6 mm=5.6 mm

(15:28)(15:28)rroo = 51 mm= 51 mm

Page 15: Anisoplanatic Wavefront Error Estimation using Coherent Imaging

15© 2009 Lockheed Martin Corporation. All Rights Reserved.

Anisoplanatism Versus SeeingAnisoplanatismAnisoplanatism Versus SeeingVersus Seeing

1540 sharpened over entire image

• Time Cn2 ro

• 1446 9.85 E-13 5.6 mm• 1502 2.20 E-13 13.8 mm• 1528 2.49 E-14 51.0 mm• 1540 5.83 E-15 122.0 mm

•• Time Time CCnn22 rroo

•• 1446 1446 9.85 E9.85 E--13 13 5.6 mm5.6 mm•• 1502 1502 2.20 E2.20 E--13 13 13.8 mm13.8 mm•• 1528 1528 2.49 E2.49 E--14 14 51.0 mm51.0 mm•• 1540 1540 5.83 E5.83 E--15 15 122.0 mm122.0 mm

Frame = 1 Sharpness = 2.4904

50 100 150 200 250

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Pupil Phase Screen

20 40 60 80 100 120

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Frame = 1 Sharpness = 2.0134

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Pupil Phase Screen

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Phase Map1446 sharpened over entire image

Phase Map

Page 16: Anisoplanatic Wavefront Error Estimation using Coherent Imaging

16© 2009 Lockheed Martin Corporation. All Rights Reserved.

Predicted phase error as a function of field angle

The phase difference structure function, The phase difference structure function, SS((rr,,θθ), derived by Fried,* is evaluated ), derived by Fried,* is evaluated in these calculations for a horizontal path (constant in these calculations for a horizontal path (constant CCnn

22). The separation of ). The separation of two points in the aperture is denoted by two points in the aperture is denoted by rr, and , and θθ is the angular separation is the angular separation between point sources. Denoting by between point sources. Denoting by ΔΔΦΦ the difference in phase between the difference in phase between the two sources after the mean value is removed, the aperturethe two sources after the mean value is removed, the aperture--average average square of the phase difference, ensemblesquare of the phase difference, ensemble--averaged, is given byaveraged, is given by

[1][1]

……where where x = r / D x = r / D and r is the radial position within the aperture and and r is the radial position within the aperture and DD is the is the aperture diameter. The aperture diameter. The MTFMTF for the circular aperture is given byfor the circular aperture is given by

[2][2]

In using In using eqeq. [1] we have neglected a weak dependence of . [1] we have neglected a weak dependence of SS on azimuth within on azimuth within the aperture. When the aperture. When DD/r/roo is not large, is not large, eq.[1eq.[1] predicts mean] predicts mean--square phase square phase differences that can be significantly smaller than the simple exdifferences that can be significantly smaller than the simple expression pression ((θθ//θθisoiso))55/3/3 which is appropriate for very large which is appropriate for very large DD/r/roo..

* David L. Fried. “Anisoplanatism in adaptive optics,” J. Opt. Soc. Am. A, 72, 52-61, (Jan 1982).

rr

θθLL

Aperture, DAperture, D

Page 17: Anisoplanatic Wavefront Error Estimation using Coherent Imaging

17© 2009 Lockheed Martin Corporation. All Rights Reserved.

AnisoplanatismAnisoplanatism Experiment Experiment vs. Theoryvs. Theory

ApertureAperture--average of the phase difference at points in the aperture for vaaverage of the phase difference at points in the aperture for varying rying seeing conditions. seeing conditions.

The error bars indicate the one sigma variability in the data. Note that the variability is much larger for large values of Cn

2 as expected.

Lines = experimental data

Points = closed form calculation

Page 18: Anisoplanatic Wavefront Error Estimation using Coherent Imaging

18© 2009 Lockheed Martin Corporation. All Rights Reserved.

-3 -2 -1 0

1

Image Plane: Sharpness = 1.0782

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Best Focus at ~700 meters

Corrected image

Waves of Focus

3 waves corresponds to about a 600 meter range shift

700 m

100 m

The Jeep is ~ 700 metersThe stand is ~ 100 metersThe beam went through the stand about where the bar target is shown

Depth of Focus DemonstrationDepth of Focus DemonstrationDepth of Focus Demonstration

32

Page 19: Anisoplanatic Wavefront Error Estimation using Coherent Imaging

19© 2009 Lockheed Martin Corporation. All Rights Reserved.

SummarySummarySummary

• Reasonable agreement between experiment and theory.

• This work continues at longer ranges and with more severe atmospheric turbulence.

•• Reasonable agreement between Reasonable agreement between experiment and theory.experiment and theory.

•• This work continues at longer ranges This work continues at longer ranges and with more severe atmospheric and with more severe atmospheric turbulence.turbulence.

Atmospheric turbulence correction using digital holographic detection: experimental results

Joseph C. Marron, 1,* Richard L. Kendrick, 2 Nathan Seldomridge, 1

Taylor D. Grow1 and Thomas A. Höft1

1Lockheed Martin Coherent Technologies, 135 S. Taylor Ave.,Louisville, CO 80027, USA 2 Lockheed Martin Advanced Technology Center, 3251 Hanover Street, Palo Alto, CA 94304 USA

*Corresponding author: [email protected]

Out Soon in:OPTICS EXPRESS

Page 20: Anisoplanatic Wavefront Error Estimation using Coherent Imaging

20© 2009 Lockheed Martin Corporation. All Rights Reserved.

THANK YOU