diffraction opticsdial/ece425/notes9.pdf · diffraction optics physical basis • considers the...
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metrical optics
e wavefronts
ptics viewpoint,
response of of the exit pupil n)
DR. ROBERT A. SCHOWENGERDT [email protected]
DIFFRACTION OPTICS
Physical basis
• Considers the wave nature of light, unlike geo
• Optical system apertures limit the extent of th
• Even a “perfect” system, from a geometrical owill not form a point image of a point source
• Such a system is called diffraction-limited
Diffraction as a linear system
• Without proof here, we state that the impulsediffraction is the Fourier transform (squared) of the optical system (see Gaskill for derivatio
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nction (PSF)
rier transform of
ind and
DR. ROBERT A. SCHOWENGERDT [email protected]
• impulse response called the Point Spread Fu
• image of a point source
• The transfer function of diffraction is the Fouthe PSF
• called the Optical Transfer Function (OTF)
Diffraction-Limited PSF
• Incoherent light, circular aperture
where J1 is the Bessel function of the first k
the normalized radius r’ is given by,
PSF r'( ) 2J1 r'( )
r'--------------
2=
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1.22π
DR. ROBERT A. SCHOWENGERDT [email protected]
where
• The first zero occurs at , or
Compare to the course notes on 2-D Fourier transforms
r'πDλf-------r
πrλN--------= =
D aperture diameter=
f focal length=
N f-number=
λ wavelength of light=
r 1.22λfD------ 1.22λN== r' =
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8 10
)
DR. ROBERT A. SCHOWENGERDT [email protected]
0
0.2
0.4
0.6
0.8
1
0 2 4 6
PS
F
normalized radius r'
2-D view (contrast-enhanced“Airy pattern”
central bright region, to first-
zero ring, is called the “Airy disk”
radial profile
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DR. ROBERT A. SCHOWENGERDT [email protected]
• Example calculation of PSF size
• system specs:
D = 1cm
f = 50mm
N = f/D = 5
λ = 0.55µm (green)
• radius of PSF = 1.22λN = 3.36µm
• very small!
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ncy is given by,
DR. ROBERT A. SCHOWENGERDT [email protected]
Diffraction-Limited OTF
• Incoherent light, circular aperture
where the normalized radial spatial freque
and the cutoff frequency is given by,
where
OTF ρ'( ) 2π--- ρ'( )acos ρ' 1 ρ'
2––=
ρ' ρ ρc⁄=
ρcDλf------ 1
λN--------= =
D aperture diameter=
f focal length=
N f-number=
λ wavelength of light=
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” function
ter of spatial
1
DR. ROBERT A. SCHOWENGERDT [email protected]
In 2-D spatial frequency space, the OTF is nearly a “cone
OTF is a low-pass filfrequencies
0
0.2
0.4
0.6
0.8
1
0 0.2 0.4 0.6 0.8
OT
F
normalized spatial frequency (ρ/ρc)
u
v
OTF
ρ = ρc
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363cycles/mm
utoff frequency of
al viewing
DR. ROBERT A. SCHOWENGERDT [email protected]
Example calculation of OTF cutoff frequency
• system specs:
D = 1cm
f = 50mm
N = f/D = 5
λ = 0.55µm (green)
• cutoff frequency = 1/λN = 0.363cycles/µm =
• very high! (the human vision system has a cabout 10cycles/mm (object scale) at normdistance)
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t and system
u,v
)
x
MTF
(
u,v
)
ut x( ) A B 2πuox( )sin+=
uox)
DR. ROBERT A. SCHOWENGERDT [email protected]
Modulation Transfer Function (MTF)
• Amplitude part of complex OTF
• signal modulation
• modulation is a measure of signal contrast
• for sinewave, , modulation = B/A
• Use MTF to predict image contrast, given objec
• output modulation(u,v) = input modulation(
• for sinewave input (object) to LSI system
the output (image) is
MTF u v,( ) OTF u v,( ) output signal modulationinput signal modulation------------------------------------------------------------= =
signal modulation max min–max min+--------------------------=
A B 2πuox( )sin+
inp
output x( ) A MTF uo( )B 2π(sin+=
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ulation MTF uo( ) BA---⋅=
u = 4u0
TFg system
DR. ROBERT A. SCHOWENGERDT [email protected]
and the image modulation at spatial frequency uo is image mod
MTF
u
1
input
output
u0 2u0 4u0
u = u0 u = 2u0
0.8
0.5
0.1
“typical” Mfor imagin
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LES
iffraction-
DR. ROBERT A. SCHOWENGERDT [email protected]
DIFFRACTION IMAGING EXAMP
Sine-wave imaged by circular aperture, dlimited
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cutoff-frequency, uc
atial frequency, u
convolution
DR. ROBERT A. SCHOWENGERDT [email protected]
opticssp
Input pattern
Output pattern
System response
(image)
(object)
(PSF)
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, diffraction-
DR. ROBERT A. SCHOWENGERDT [email protected]
Square-wave imaged by circular aperture
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cutoff-frequency, uc
spatial frequency, u
convolution
DR. ROBERT A. SCHOWENGERDT [email protected]
limited optics
Input pattern
Output pattern
System response
(image)
(object)
(PSF)
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sufficient energy
rce
se energy –>
DR. ROBERT A. SCHOWENGERDT [email protected]
Line and Edge Spread Functions
• PSF is often difficult to measure because of in
• Use a line source (slit) to increase energy –>
Line Spread Function (LSF)• Integrate PSF along direction of the line sou
• Use edge source (knife edge) to further increa
LSFx x( ) PSF x y,( ) yd
∞–
∞
∫=
LSFy y( ) PSF x y,( ) xd
∞–
∞
∫=
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ment
tem
f the PSF is not
DR. ROBERT A. SCHOWENGERDT [email protected]
Edge Spread Function (ESF)• Integrate LSF up to position of ESF measure
• Equivalent to step response in electronic sys
• ESF is a monotonic function of position
• LSF is the derivative of the ESF,
• Both LSF and ESF are orientation-dependent, iisotropic
ESFx x( ) LSFx α( ) αd
∞–
x
∫=
ESFy y( ) LSFy α( ) αd
∞–
y
∫=
LSFx x( )xd
dESFx x( )=
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tations to
DR. ROBERT A. SCHOWENGERDT [email protected]
• Must measure LSF and ESF at multiple orienreconstruct full 2-D PSF
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SF AND OTF
n are:
x(x)
Fx(x)
1-Dderivative
DR. ROBERT A. SCHOWENGERDT [email protected]
RELATIONSHIPS BETWEEN PSF, LSF, E
• For example, the relationships in the x-directio
PSF(x,y)
OTF(u,v) LSF
2-Done-sided
1-D
ES
1-DFourier
Transform
TransformFourier
OTF(u,0)profile
one-sided 1-D integration
integration
1-Dintegration
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MAGING
DR. ROBERT A. SCHOWENGERDT [email protected]
SECTION III – INTEGRATED ISYSTEM ANALYSIS
Scanning
Image Quality
System Simulation
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ctor(s)
s
DR. ROBERT A. SCHOWENGERDT [email protected]
SCANNING
Instantaneous image on focal plane dete
Scan the field-of-view
• Object-space scanning (mirror moves)
Show that the object-space scan angle itwice that of the mirror scan angle
object
θ
2θ
detector
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)
DR. ROBERT A. SCHOWENGERDT [email protected]
• Image-space scanning (detector moves)
• Translation scanning (camera or object moves
object
detector
object
detector
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te sensing
wavelengthdispersionnner
m scanner
DR. ROBERT A. SCHOWENGERDT [email protected]
Examples from airborne or satellite remosystems
What types of scanning are these examples?
1-D arraywhiskbroom scanner
GFOV
FOV cross-trackin-track
line scanner
2-D arraypushbroom sca
pushbroo
FOV: Field-Of-View (radians)
GFOV: Ground-projected FOV (km)
(aka “swath width”)
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ll area of the
mber of photons
terval equal to
ere W is the
ere is also image
DR. ROBERT A. SCHOWENGERDT [email protected]
Scanning is equivalent to convolution
• At each instant, the detector integrates a smaimage
• Integration time at each sample determines nucollected
• Generally, a scanned image is sampled at an indetector size
• undersampledWhy is one sample/detector element undersampled?
• PSF of scanning detector is rect(x/W,y/W), whdetector size
• If sample integration time is not negligible, thsmear
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is the amount of
gration time/ blurred)
r during pixel
tector width:
)---
DR. ROBERT A. SCHOWENGERDT [email protected]
• PSF of linear image smear is rect(x/S), where Ssmear during the integration time:
• Image smear sometimes used to increase intepixel, and therefore SNR (even though image is
• Total scanning PSF
• Combine scanning detector and image smeaintegration (normalize by volume PSF)
• if S = W, i.e. image smear is equal to one de
S image velocity x integration time=
vimgtint=
PSFscan x y,( ) rect x W⁄ y W⁄,( ) * rect x S⁄( )volumePSF
---------------------------------------------------------------------------=
rect x W⁄( ) * rect x S⁄( )[ ]rect y W⁄(volumePSF
------------------------------------------------------------------------------------------=
PSFscan x y,( ) tri x W⁄( )rect y W⁄( )volumePSF
----------------------------------------------------=
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systems
electronic
age quality
humanvision
subsystem
tina*
neuralnetwork
brain
DR. ROBERT A. SCHOWENGERDT [email protected]
IMAGE QUALITY
An imaging system consists of several sub
* points of signal transduction, optical <—>
Want to maintain the highest possible imthrough this process
lightsource
scene
imageacquisitionsubsystem
transmissionsubsystem
displaysubsystem*
optics detector* electronics
coder decoder
optics
re
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o closely spaced
mination
image
es when the first f the other pattern
easure
DR. ROBERT A. SCHOWENGERDT [email protected]
Spatial Resolution
• “Resolution” refers to the ability to detect twobjects in an image
• Many different ways to measure resolution
• Rayleigh Criterion
• quantitative; does not depend on visual exa
• appropriate for diffraction-limited optical
• two point sources —> two Airy patterns
• resolution is the separation of the two imagzero of one pattern coincides with the peak o
• does not incorporate noise into resolution m
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hey are just
λN
DR. ROBERT A. SCHOWENGERDT [email protected]
• Target-Specific Criteria
• separation of two particular objects when t“resolved”
• depends on visual examination
• incorporates noise into resolution measure
R Rayleigh = 1.22
Airypattern1
Airypattern2
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g imagery
DR. ROBERT A. SCHOWENGERDT [email protected]
targetimaging system PSF and resultin
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requency to
5 6
5 6
DR. ROBERT A. SCHOWENGERDT [email protected]
• Usually have fixed system PSF; vary target fevaluate resolution
target
imagingsystemPSF
image oftarget
1 2 3 4
1 2 3 4
profileof image
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e bar
et which is “just ually
DR. ROBERT A. SCHOWENGERDT [email protected]
• Define a line pair = one dark bar & one whit
• Define resolution to be measured by the targresolved” (correct number of bars can be visdistinguished along their entire length)
• Rbar = 1/d4 (line pairs/mm)
where d4 = mm/line pair for target 4
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5 6
DR. ROBERT A. SCHOWENGERDT [email protected]
• image noise lowers resolution
• Rbar = 1/d3 (line pairs/mm)
1 2 3 4
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ystem
it motion, in-
DR. ROBERT A. SCHOWENGERDT [email protected]
SENSOR SIMULATION
Landsat Thematic Mapper (TM) satellite s
Whiskbroom scanner
• side-to-side scanning, cross-track
• satellite orbtrack
whiskbroom scanner
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• Three major spatial response components
DR. ROBERT A. SCHOWENGERDT [email protected]
optics detector electronics
cross-track
in-trackcross-track
only
30m GIFOV
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al photography
to align orbit
scan tion - ixels
DR. ROBERT A. SCHOWENGERDT [email protected]
• Simulate input scene with high resolution aeri
rotatedwith TM
and direc2m p
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ample to 30m
DR. ROBERT A. SCHOWENGERDT [email protected]
• Apply each component PSF at 2m and downs
optics optics and detector
optics, detector and electronics
downsample2m —> 30m GSI
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ths later
DR. ROBERT A. SCHOWENGERDT [email protected]
Compare to real TM of same area, acquired 4 mon
simulated TM real TM (magnified)
(contrast-adjusted)
real TM
(magnified)
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f silver halide in
image
ia
DR. ROBERT A. SCHOWENGERDT [email protected]
PHOTOGRAPHIC GRANULARITY
• photographic density is aggregated “grains” odeveloped film
• causes random noise at every pixel in scanned
• Ex: aerial photograph of Dulles Airport, Virgin
enlargement
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versus DN
DR. ROBERT A. SCHOWENGERDT [email protected]
• Signal-dependent noise
• Standard deviation in Digital Numbers (DNs)
6
8
10
12
14
16
0 50 100 150 200
σ DN
µDN
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es
g
DR. ROBERT A. SCHOWENGERDT [email protected]
ELECTRO-OPTICAL SCANNER NOISE
• Due to
• line scan calibration (gain and offset) chang
• detector-to-detector calibration differences
• interference with other electronics
• saturation hysteresis
• Common problem
• Can be removed effectively by image processin
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erent noise
dom pixel noise
DR. ROBERT A. SCHOWENGERDT [email protected]
aerial video aperiodic scanline noise Landsat–4 MSS coh
Landsat–1 MSS bad scanline noise
Landsat–4 TM banding noise
AVIRIS scanline and ran
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DR. ROBERT A. SCHOWENGERDT [email protected]
Signal-to-Noise Ratio (SNR)
• Measure of image quality
• Several common definitions:
SN Rstd
σsignal
σnoise-----------------=
SN Rvar
σsignal2
σnoise2
-----------------=
SNRdB 10 SNR( )log=
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SNRstd 2=SNRvar 4=SNRdB 6=
SNRstd 10=SNRvar 100=SNRdB 20=
DR. ROBERT A. SCHOWENGERDT [email protected]
• Generally correlated with visual quality
SNRstd 1=SNRvar 1=SNRdB 0=
SNRstd 5=SNRvar 25=SNRdB 14=
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noise
DR. ROBERT A. SCHOWENGERDT [email protected]
• Visual quality depends on noise type
noiseless
global random noise detector striping