adaptive-optics compensation temporal scaling laws for aero-optical disturbances
DESCRIPTION
Adaptive-optics compensation temporal scaling laws for aero-optical disturbances Matthew R. Whiteley, Ph.D. Eric P. Magee, Ph.D. March 22, 2007. MZA Associates Corporation 6651 Centerville Business Pkwy Ste B Dayton, OH 45459-2678 Voice: (937) 432-6560 x237 [email protected]. Overview. - PowerPoint PPT PresentationTRANSCRIPT
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MZA Associates Corporation
MRW – 3/22/20071FOR OFFICIAL USE ONLY
Adaptive-optics compensation temporal
scaling laws for aero-optical disturbances
Matthew R. Whiteley, Ph.D.
Eric P. Magee, Ph.D.
March 22, 2007
MZA Associates Corporation
6651 Centerville Business Pkwy Ste B
Dayton, OH 45459-2678
Voice: (937) 432-6560 x237
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MZA Associates Corporation
MRW – 3/22/20072FOR OFFICIAL USE ONLY
Overview
Scaled USAFA wind tunnel aero-optical disturbancesAdaptive optics compensation with classical control
Bandwidth limitations for idealized AO Scaling relations, power laws, and compensation frequencies
Effect of latency on aero-optics compensation Frequency-domain analysis with classical AO error rejection
Sample of adaptive AO control for aero-optics
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MZA Associates Corporation
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USAFA Wind Tunnel Measurements:8x8 Wavefront Sensor Data
12” turret model with 3” wavefront reconstructions
Mounted in USAFA wind tunnel Optical measurements @ M = 0.4 High-bandwidth wavefront sensor
8x8 subaperture array (moderate-to-low) 78.125 kHz sample rate (fast) Photos courtesy University of Notre Dame
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MZA Associates Corporation
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Nature of Aero-Optical Disturbances
sideview
topview
HEL
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MZA Associates Corporation
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Wavefronts Scaled for ATL:Dt = 1.27 m, vp = 0.3 Mach, hp = 10kft
120
°
UNFILTERED LOW FREQUENCY (< 144 Hz) HIGH FREQUENCY (> 144 Hz)
130
°
P-V = 2.27 λ
P-V = 2.81 λ
P-V = 0.13 λ
P-V = 1.20 λ
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Aero-Optics Power Spectrum
Cumulative power 120° and 130° turret angle—normalized to power @ 130°
Increase above ~100 HZ attributed to shear-layer
Comparison of disturbance power spectrum for 120° and 130° turret angle
Enhancement in disturbance at 130° primarily at higher frequency
shear layer
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MZA Associates Corporation
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Simulation & Controller Characteristics
With 0 latency in the simulation, error rejection is given by
Simulation & theoretical error rejection compare favorably
Closed-loop tracking and higher-order sensing/compensation
Simple integrator control
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Compensation Results with Variable AO Bandwidth
Open loop Strehl ratio = 0.26, closed-loop @ 500 Hz bandwidth = 0.76
Disturbance is dominated by low-frequency components Well-compensated with 200 Hz AO loop
High-frequency OPD limits compensation
Turret = 130°
Open loop Strehl ratio = 0.38, closed-loop @ 500 Hz bandwidth = 0.93
Shear-layer disturbance is negligible Compensation performance
governed by low-frequency disturbances
Turret = 120°
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Compensation Scaling Analysis
Compensation data tested for power-law scaling behavior
Linear fit of natural log of normalized phase variance to natural log of compensation bandwidth gives power-law fitting parameters
Compensation power-law can be written in the following form:
Aero-optics compensation scaling frequency fA gives bandwidth at which disturbance is reduced by a factor of 2
Analogous to scaling law for compensation of free-stream turbulence
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Compensation Scaling Results130° Turret Angle
UNFILTERED
LOW FREQUENCY
HIGH FREQUENCY
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AO Latency: Implications to Aero-Optics
Practical AO systems suffer degradation due to net latency Sensor integration, read-out,
reconstruction/processing, DM response, etc.
Error rejection takes on more general form under these conditions
Incorporate this model directly in aero-optics compensation analysis
Can consider this as a composite of low-frequency and high-frequency phenomena
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Effect of AO Latency:130° Turret Angle
Error rejection with latency used with disturbance PSDs to quantify residual Strehl
Degradation with AO latency is driven by presence of high-frequency aero-optics
Shear-layer compensation requires high-bandwidth, low-latency control
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WaveTrain Adaptive Controller
classical
adaptive
WFSslopesinput
ACTcommands
output
augmentation
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AO Simulation Results:Classical and Adaptive Control
Filtered high-frequency shear layer Classical AO with 440 µsec latency
degrades compensation of shear layer 50 Hz bandwidth + latency with
adaptive control similar to 500 Hz classical control with 0 latency
Unfiltered aero-optics disturbance Classical AO control optimized for
100 Hz – 150 Hz bandwidth Alternative adaptive control reduces
degradation due to latency and limited bandwidth
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MZA Associates Corporation
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Summary / Conclusions
Classical AO compensation effective against low-frequency, large-magnitude disturbances Constitute the bulk of aero-optical OPD at the turret angles examined
Bandwidth requirements achievable with reasonable sensors & standard control 1-2 kHz sample rate with 100-200 Hz error rejection bandwidth
High-frequency shear-layer disturbances require a high-bandwidth and low-latency control system
Adaptive control will help recover high-bandwidth degradations in compensation Other compensation methods such as flow control may still be necessary
to sufficiently correct shear-layer disturbances Flow control can also benefit from adaptive AO control
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MZA Associates Corporation
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Acknowledgement
This work was part of a Phase I SBIR effort sponsored by AFRL/DES (Starfire Optical Range) Contract #FA9451-06-M-0128 Technical monitor: Dr. Larry Weaver
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Backup
The following slides are backup
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MZA Associates Corporation
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Wavefront Scaling to ATL
Scaling of OPD magnitude 451-frame sequences for 2 runs delivered to MZA by Notre Dame Data was stored such that it could be scaled to desired conditions
Scaling of OPD temporal evolution Keep Strouhal number (fDt/M) constant for test vs. scaled conditions
Desired conditions for ATL Dt = 50 in (1.27 m) M = 0.3 ρ = 0.918 kg/m3 (~ US Std 1976 @ 10 kft)