Basic radiometry and SNR equations for CCD, ICCD...
Transcript of Basic radiometry and SNR equations for CCD, ICCD...
Basic radiometry and SNRequations for CCD, ICCD and
EMCCD imagersUrban Brandstrom,1
1 Swedish Institute of Space Physics, Kiruna, Sweden
Presentation at:
http://alis.irf.se/˜urban/AGF351/Braendstroem-UNIS.pdf
UNIS 2011-11-15 – p. 1
Radiometry vs. photometryHolst [1998] defines the term radiometry, as the
“energy or power transfer from a source toa detector”
UNIS 2011-11-15 – p. 6
Radiometry vs. photometryHolst [1998] defines the term radiometry, as the
“energy or power transfer from a source toa detector”
while photometry is defined as
“the transfer from a source to a detectorwhere the units of radiation have beennormalised to the spectral sensitivity ofthe eye.”
UNIS 2011-11-15 – p. 6
Radiometry vs. photometryHolst [1998] defines the term radiometry, as the
“energy or power transfer from a source toa detector”
while photometry is defined as
“the transfer from a source to a detectorwhere the units of radiation have beennormalised to the spectral sensitivity ofthe eye.”
Unfortunately the term photometry is often usedinstead of radiometry
UNIS 2011-11-15 – p. 6
Radiometry“Mathematics is often called the queen of thesciences. Radiometry should then be called thewaiting maid or servant. It is not especially elegant;it is not very popular, has not been trendy; but it isessential in almost every part of opticalengineering.” Wolfe [1998]
UNIS 2011-11-15 – p. 7
Solid angleThe solid angle Ω sweeps out the area A on theunit sphere (4π)
Ω =A
r2[sr]
Think of it as a 3D generalisation of the radian(arc length on the unit circle)
UNIS 2011-11-15 – p. 8
RadianceAlso known as radiant steranceIn energy units:
LE =∂2Φ(λ)
∂As∂Ω
[
W
m2 sr
]
In quantum units:
Lγ =λ
hcLE
[
photons
s m2 sr
]
UNIS 2011-11-15 – p. 10
Spectral radianceAlso known as spectral radiant steranceIn energy units:
LλE =∂L
∂λ
[
W
m2 µm sr
]
In quantum units:
Lλγ =λ
hcLλE
[
photons
s m2 µm sr
]
UNIS 2011-11-15 – p. 11
Spectral radiant emittanceAlso known as spectral radiant exitance
Mλγ =∂Φ
∂As
=
[
photons
s m2
]
Flux per source area.What you get from a calibration source.In energy units:
MλE =hc
λMλγ
[
W
m2 µm sr
]
UNIS 2011-11-15 – p. 12
Spectral irradianceAlso known as spectral radiant incidance
Eλe =∂Φ
∂A=
[
photons
s m2
]
Flux per detector area.What you get on a detector (or whatever)In energy units:
EλE =hc
λEλγ
[
W
m2 µm sr
]
UNIS 2011-11-15 – p. 13
IrradianceAt apperture:
Eγapp=
Φγapp
Aapp
=LγAsTaΩds
Aapp
=
[
photons
s m2
]
At image plane (assuming circular apperture):
Eγi=
Φγapp
Ai
= Lγ
As
Ai
Tπd2
app
4r2s
=
[
photons
s m2
]
(1)
UNIS 2011-11-15 – p. 15
Photometric units
Φv = KM
∫ 750nm
380nm
V (λ)Mp(λ)dλ [lm]
scoptic—rods photoptic—cones After Holst [1998]
UNIS 2011-11-15 – p. 16
Photometric units
scoptic—rods (KM = 1746 lm/W) photoptic—cones(K = 683 lm/W) After Holst [1998]
UNIS 2011-11-15 – p. 17
Photometric unitsΦv lm luminous fluxLv cd/m2 or nits luminanceMv lux or lm/m2 luminous emmitanceEv lux or lm/m2 illumniance
UNIS 2011-11-15 – p. 18
The foot-lambertA foot-lambert or footlambert (fL, sometimes fl orft-L) is a unit of luminance in U.S. customaryunits and some other unit systems. Afoot-lambert equals 1/π candela per square foot,or 3.426 candela per square meter (thecorresponding SI unit).
1 [ftL] =1
π
[
cd
ft2
]
≈ 3.426
[
cd
m2
]
UNIS 2011-11-15 – p. 19
The Rayleigh (1)Consider a cylindrical column of cross-sectionalarea 1 m2 extending away from the detector intothe source.The volume emission rate from a volumeelement of length dl at distance l isǫ(l, t, λ) photons m−3 s−1. The contribution to Lγ isgiven by:
dLγ =ǫ(l, t, λ)
4πdl
[
photons
s m2 sr
]
(2)
UNIS 2011-11-15 – p. 21
The Rayleigh (2)Integrating along the line of sight l [m]:
4πLγ =
∫ ∞
0
ǫ(l, t, λ)dl(3)
This quantity is the column emission rate, whichHunten et al. [1956] proposed as a radiometric unitfor the aurora and airglow.
UNIS 2011-11-15 – p. 22
The Rayleigh (3)In SI-units the Rayleigh becomes[Baker and Romick, 1976]:
1 [Rayleigh] ≡ 1 [R] , 1010
[
photons
s m2 (column)
]
(4)
The word column denotes the concept of anemission-rate from a column of unspecifiedlength, as discussed above. It should be notedthat the Rayleigh is an apparent emission rate,not taking absorption or scattering into account.
UNIS 2011-11-15 – p. 23
The Rayleigh (4)However (unfortunately. . . )
“the Rayleigh can be used as defined without anycommitment as to its physical interpretation, eventhough it has been chosen to make interpretationconvenient.” Hunten et al. [1956]
And then there is the clarifications by: Baker[1974]; Baker and Romick [1976]; Chamberlain [1995]
UNIS 2011-11-15 – p. 24
. . . God said:Go to, let us go down, and there confound theirlanguage, that they may not understand oneanother’s speech. [Bible Gen11:7]
UNIS 2011-11-15 – p. 26
. . . God said:Go to, let us go down, and there confound theirlanguage, that they may not understand oneanother’s speech. [Bible Gen11:7]And there was: stilb, Rayleighs, footlamberts, Irradiance,spectral-radiant sterance, lumens, lux, candela, radiometry,nit, luminance, illuminance, emittance, apostilb, phot, skot,lambert, foot-candle, photometry, DIN, ASA, ISO. . .
UNIS 2011-11-15 – p. 26
. . . God said:Go to, let us go down, and there confound theirlanguage, that they may not understand oneanother’s speech. [Bible Gen11:7]And there was: stilb, Rayleighs, footlamberts, Irradiance,spectral-radiant sterance, lumens, lux, candela, radiometry,nit, luminance, illuminance, emittance, apostilb, phot, skot,lambert, foot-candle, photometry, DIN, ASA, ISO. . .
—Help! We are sinking!
UNIS 2011-11-15 – p. 26
The 4π confusionTherefore, we propose that photometricmeasurements of the airglow and aurora bereported in terms of 4πB rather than the surfacebrightness B itself. Further, we suggest that 4πB
be given the unit “rayleigh” (symbol R), where B isin units of 106 quanta cm−2 s−1 sr−1. Hence1 R = 106 quanta cm−2 (column)−1 s−1.
Hunten et al. [1956]
UNIS 2011-11-15 – p. 29
The 4π confusionTherefore, we propose that photometricmeasurements of the airglow and aurora bereported in terms of 4πB rather than the surfacebrightness B itself. Further, we suggest that 4πB
be given the unit “rayleigh” (symbol R), where B isin units of 106 quanta cm−2 s−1 sr−1. Hence1 R = 106 quanta cm−2 (column)−1 s−1.
Hunten et al. [1956]
So does both Hunten et al. [1956] and Chamberlain[1995] claim that 4π × 106 = 106 ???
UNIS 2011-11-15 – p. 29
Can we agree on this?The apparent radiance (Lγ) can be obtained fromthe column emission rate I (in Rayleighs)according to Baker and Romick [1976]:
Lγ =1010I
4π
[
photons
s m2 sr
]
(5)
UNIS 2011-11-15 – p. 30
Can we agree on this?The apparent radiance (Lγ) can be obtained fromthe column emission rate I (in Rayleighs)according to Baker and Romick [1976]:
Lγ =1010I
4π
[
photons
s m2 sr
]
(7)
Or is it:
Lγ = 1010I
[
photons
s m2 sr
]
(8)
UNIS 2011-11-15 – p. 30
Where are my photons?• Transmittance (atmosphere, optics, filters. . . )• Apperture of the optics
UNIS 2011-11-15 – p. 33
Where are my photons?• Transmittance (atmosphere, optics, filters. . . )• Apperture of the optics• Area of detector (pixel-area for imagers)
UNIS 2011-11-15 – p. 33
Where are my photons?• Transmittance (atmosphere, optics, filters. . . )• Apperture of the optics• Area of detector (pixel-area for imagers)• Number of photoelectrons collected in a pixel
ne−γ= QE(λ)Eγi
tintApix
[
e−]
(15)
UNIS 2011-11-15 – p. 33
Where are my photons?• Transmittance (atmosphere, optics, filters. . . )• Apperture of the optics• Area of detector (pixel-area for imagers)• Number of photoelectrons collected in a pixel
ne−γ= QE(λ)Eγi
tintApix
[
e−]
(17)
ne−γ≈ QE(λ)TtintApix
1010I
16f 2#
[
e−]
(18)
UNIS 2011-11-15 – p. 33
Notation〈X〉2 variance of X
〈X〉 standard deviation of X
X mean value of X
Photon arrival is Poisson distributedIt can be shown that for a Poisson distributedsignal variance is equal to the mean
UNIS 2011-11-15 – p. 37
Shot Noise
〈ne−s〉 =
√
CTEN
(
〈ne−γ〉2 + 〈ne−d
〉2)
=(20)
=
√
CTEN
(
ne−γ+ ne−d
)
≈(21)
≈√
ne−γ+ ne−d
(22)
UNIS 2011-11-15 – p. 43
Pattern Noise
〈ne−p〉 =
√
〈ne−FPN〉2 + 〈ne−PRNU
〉2 ≈ 〈ne−PRNU〉 ≈(23)
≈ Une−γ≈
ne−γ√ne−max
[
e−RMS
]
(24)
UNIS 2011-11-15 – p. 45
Signal-to-noise ratio for a CCD• Measured signal-to-noise ratio:
SNRCCD =DN signal
DN noise
≈ne−γ
〈ne−CCD〉(26)
UNIS 2011-11-15 – p. 47
Signal-to-noise ratio for a CCD• Measured signal-to-noise ratio:
SNRCCD =DN signal
DN noise
≈ne−γ
〈ne−CCD〉(29)
• thus for a CCD:
SNRCCD ≈ne−γ
√
ne−γ+ ne−d
+ 〈ne−r〉2
(30)
UNIS 2011-11-15 – p. 47
Signal-to-noise ratio for a CCD• Measured signal-to-noise ratio:
SNRCCD =DN signal
DN noise
≈ne−γ
〈ne−CCD〉(32)
• thus for a CCD:
SNRCCD ≈ne−γ
√
ne−γ+ ne−d
+ 〈ne−r〉2
(33)
• and for an ideal photon detector:
SNRγideal =√
ne−γ(34) UNIS 2011-11-15 – p. 47
Threshold of detectionThe threshold of detection is usually defined asSNR = 2 while the Noise Equivalent ExposureNEE , is obtained when SNR = 1. For a CCD themaximum signal, or Saturation EquivalentExposure, SEE is obtained when the charge wellcapacity ne−max
[e−], is reached. This occurs when:
ne−γ≥ ne−max
− ne−d(35)
In most cases the maximum charge-well capacityDN SEE [counts], is matched to the maximumADC output DN max.
UNIS 2011-11-15 – p. 48
Dynamic range (1)The Dynamic Range is defined as the peaksignal divided by the RMS noise and theDC-bias-level, (if any). The minimum ADCoutput, is subtracted in the case of a signedinteger output. DR is usually expressed indecibels.
DR = 20 log10
(
DN SEE − DN min
DN DC + DN NEE − DN min
)
[dB]
(36)
UNIS 2011-11-15 – p. 49
Dynamic range (2)An approximate theoretical value for DR isobtained by dividing the maximum signal by thetotal noise
DR ≈ 20 log10
ne−max− ne−d
〈ne−tot〉 [dB](37)
UNIS 2011-11-15 – p. 50
SNR for a CCD• Measured signal-to-noise ratio:
SNRCCD =DN signal
DN noise
≈ne−γ
〈ne−CCD〉
UNIS 2011-11-15 – p. 53
SNR for a CCD• Measured signal-to-noise ratio:
SNRCCD =DN signal
DN noise
≈ne−γ
〈ne−CCD〉
• For an ideal photon detector:
SNRγideal =√
ne−γ
UNIS 2011-11-15 – p. 53
SNR for a CCD• Measured signal-to-noise ratio:
SNRCCD =DN signal
DN noise
≈ne−γ
〈ne−CCD〉
• For an ideal photon detector:
SNRγideal =√
ne−γ
• and for a CCD:
SNRCCD ≈ne−γ
√
ne−γ+ ne−d
+ 〈ne−r〉2 UNIS 2011-11-15 – p. 53
SNR for an ICCDNoting that for an ICCD:
ne−γ,pc≈ QEpc
(λ)TtintM2FOApix
1010I
16f 2#
[
e−RMS
]
UNIS 2011-11-15 – p. 54
SNR for an ICCD• The signal-to-noise ratio for an ICCD can be
estimated as:
SNRICCD ≈ne−γ,pc
√
k2MCP (ne−γ,pc
+ ne−d,pc) +
ne−
d+〈n
e−
r〉2
g2
UNIS 2011-11-15 – p. 55
SNR for an ICCD• The signal-to-noise ratio for an ICCD can be
estimated as:
SNRICCD ≈ne−γ,pc
√
k2MCP (ne−γ,pc
+ ne−d,pc) +
ne−
d+〈n
e−
r〉2
g2
• As seen, increasing the gain of the imageintensifier makes the CCD noise-sourcesnegligible, but does not increase the SNR
beyond that. For very high gain, we see that:
SNRICCD ≈ne−γ,pc
√
2(ne−γ,pc+ ne−d,pc
) UNIS 2011-11-15 – p. 55
SNR for an emCCDThe signal-to-noise ratio for anelectron-multiplication CCD can be estimated as:
SNRemCCD ≈ne−γ
√
k2em (ne−γ
+ ne−d+ 〈ne−cic
〉2) +〈n
e−
r〉2
g2
Please note:For an EMCCD kem ≈
√2 while kMCP (ICCD) is
taken as√
2 here, which is somewhat too good tobe true. In real cases kMCP ≥ 1.6
UNIS 2011-11-15 – p. 56
SNR example: CCD vs. ICCD
0.1
1
10
100
1000
10000 100000 1e+06 1e+07 1e+08 1e+09 1e+10
SN
R
Column emission rate Rayleighs 557.7 nm
t=16.7 ms, T=0.5, f/3.9, ALIS CCDCAM5, PAI ICCD
Ideal CCD (a)ALIS CCD (b)
PAI ideal CCD (c)PAI ICCD (d)PAI CCD (e)
UNIS 2011-11-15 – p. 57
SNR vs. of integration time
0.1
1
10
100
1000
10000
0.001 0.01 0.1 1 10 100 1000 10000
SN
R
Integration time [s]
T=0.5, f/3.5, ALIS CCDCAM5 557.7 nm
1 MR (a) 100 kR (b) 10 kR (c) 1 kR (d)
100 R (e)
UNIS 2011-11-15 – p. 58
Where are my photons?• Transmittance (atmosphere, optics, filters. . . )• Apperture of the optics
UNIS 2011-11-15 – p. 59
Where are my photons?• Transmittance (atmosphere, optics, filters. . . )• Apperture of the optics• Area of detector (pixel-area for imagers)
UNIS 2011-11-15 – p. 59
Where are my photons?• Transmittance (atmosphere, optics, filters. . . )• Apperture of the optics• Area of detector (pixel-area for imagers)• Number of photoelectrons collected in a pixel
ne−γ= QE(λ)Eγi
tintApix
[
e−]
(44)
ne−γ≈ QE(λ)TtintApix
1010I
16f 2#
[
e−]
(45)
UNIS 2011-11-15 – p. 59
SNR and on-chip binning
0.1
1
10
100
1000
1 100 10000 1e+06 1e+08 1e+10
SN
R
Column emission rate Rayleighs 557.7 nm
t=1 s, T=0.5, f/3.5, ALIS CCDCAM5, PAI ICCD
bin 1,1 (a)bin 2,2 (b)bin 4,4 (c)bin 8,8 (d)
bin 16,16 (e)
UNIS 2011-11-15 – p. 60
SNR: CCD, ICCD and emCCD
0.1
1
10
100
1000
1000 10000 100000 1e+06 1e+07 1e+08 1e+09 1e+10
SN
R
Column emission rate Rayleighs 557.7 nm
t=1/25 s, T=0.5, f/1.6, bin=1x1
Ideal SI003AB (a)SI003AB (b)
Ideal PAI CCD (c)PAI ICCD (d)
Ideal CCD201-20 (g)CCD201-20 (h)
bin 2,2 CCD201-20 (h)
UNIS 2011-11-15 – p. 61
Fast: ≈ 2900 photons/pixel
0.01
0.1
1
10
100
1 10 100 1000 10000
SN
R
photons/pixel (assuming 90% QE)
EM ON vs. EM OFF at 10 MHz
Ideal CCD201-20EM OFF 10 MHz CCD201-20EM ON 10 MHz CCD201-20
UNIS 2011-11-15 – p. 63
Slow: ≈ 42 photons/pixel
0.1
1
10
100
1 10 100 1000
SN
R
photons/pixel (assuming 90% QE)
Slow readout EM ON vs. Conventional Ampl.
Ideal CCD201-201 MHz Con. CCD201-20
EM ON 1 MHz CCD201-20
UNIS 2011-11-15 – p. 65
IntercalibrationThis is the process of intercalibrating calibrationsources and to transfer absolute calibrationinformation between different instruments andresearch groups.
Hans Lauches intercalibration photometer (responsibleperson: 1981–1999 Lauche, 1999-2011 Widell, SSC,
2011– Brändström, IRF)UNIS 2011-11-15 – p. 68
Intercal. procedure• Calibrators are compared at calibration
workshops using a calibration-photometerwith 7 filters and a reference source.
UNIS 2011-11-15 – p. 70
Intercal. procedure• Calibrators are compared at calibration
workshops using a calibration-photometerwith 7 filters and a reference source.
• Last known absolute callibration of thecalibration equipment against a nationalstandard (NBS) was done by [Torr and Espy,1981].
UNIS 2011-11-15 – p. 70
Intercal. procedure• Calibrators are compared at calibration
workshops using a calibration-photometerwith 7 filters and a reference source.
• Last known absolute callibration of thecalibration equipment against a nationalstandard (NBS) was done by [Torr and Espy,1981].
• Known calibration workshops at the opticalmeetings were: Aberdeen 1981, Lindau 1983,Lysebu 1985, Saskatoon 1987, Lindau 1989,Wien 1991, Lindau 1999, Stockholm 2000,Oulu 2001, Kiruna 2006, Andøya 2007 andSodankylä 2011.
UNIS 2011-11-15 – p. 70
Intercal. workshops
0
5
10
15
20
25
1980 1985 1990 1995 2000 2005 2010
Number of participating calibrationsources in intercalibration workshops 1981-2011
UNIS 2011-11-15 – p. 71
Intercal. results
0.001
0.01
0.1
1
10
100
1000
3500 4000 4500 5000 5500 6000 6500 7000 7500
[Ray
leig
hs/A
ngst
rom
]
Wavelength [Angstrom]
Y275L1614920B
UNIS 2011-11-15 – p. 75
Intercal. errors
-30
-20
-10
0
10
20
30
4000 4500 5000 5500 6000 6500 7000
ratio
[%]
Wavelength [Angstrom]
Confusogram of calibration ratios [1985,1999,2000,2001 to 2006]
y275 1985y275 1999y275 2000y275 2001
l1614 1985l1614 1999l1614 2000l1614 2001920b 1985920b 1999920b 2000920b 2001
UNIS 2011-11-15 – p. 76
CalibrationCalibration is the process of answering thefollowing two basic questions:
1. What physical value does the pixel represent?(absolute calibration)
2. How is each pixel mapped to the observedobject? (geometrical calibration)
UNIS 2011-11-15 – p. 78
ChallengeRead the “28. Appendix” and compare toSigernes et al. [2008]. You might also want tocompare to Torr and Espy [1981]Calculate R/Å for the IRF-UJO-Y275 radioactivesource around 5577 Å using the result in “28.Appendix” and compare to latest intercalibrationresult from Sodankylä. (That source is marked15 µlm
UNIS 2011-11-15 – p. 80
Spectroscopic imaging
4000 4500 5000 5500 6000 6500 7000 7500 8000 8500 9000Wavelength [Å]
UNIS 2011-11-15 – p. 83
Selectable common volumes
−200 −100 0 100 200−150
−100
−50
0
50
100
MerasjaerviSilkimuotka
Tjautjas
surveilance
KirunaNikaluokta
Abisko
−100 0 100 200−150
−100
−50
0
50
Merasjaervi
Silkimuotka
Tjautjas
mag_zen
KirunaNikaluokta
Abisko
−200 −100 0 100 200
−200
−150
−100
−50
0
50
MerasjaerviSilkimuotka
TjautjasKiruna
south
Nikaluokta
Abisko
−200 −100 0 100
−100
−50
0
50
100
Merasjaervi
Silkimuotka
Tjautjas
Kiruna
core
Nikaluokta
Abisko
−400 −200 0 200 400
0
100
200
300
400
MerasjaerviSilkimuotka
TjautjasKiruna
east−west
NikaluoktaAbisko
−300 −200 −100 0 100 200
0
100
200
300
MerasjaerviSilkimuotka
TjautjasKirunaNikaluokta
Abisko
north
−200 0 200
0
100
200
300
400
MerasjaerviSilkimuotka
TjautjasKiruna
eiscat
NikaluoktaAbisko
Approximate field of view at 110 km
−200 0 200
0
100
200
300
400
MerasjaerviSilkimuotka
TjautjasKiruna
heating
NikaluoktaAbisko
o50 90o
[km]0−50 100−100 200−150
0
50
100
150
200
250
[km]
aφ
Azimuth
W E
S
α
x
Ny
zβ β
UNIS 2011-11-15 – p. 84
Auroral tomography
−50 0 5090
100
110
120
130
140
150
160
20:09:00A
ltitu
de (
km)
−50 0 5090
100
110
120
130
140
150
160
20:09:30
−50 0 5090
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160
20:10:00
Alti
tude
(km
)
−50 0 5090
100
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120
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140
150
160
20:10:30
−50 0 5090
100
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120
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20:11:00
Alti
tude
(km
)
North (km)−50 0 50
90
100
110
120
130
140
150
160
20:11:30
North (km)
40 km west of Kiruna
−50 0 5090
100
110
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150
160
20:09:00
Alti
tude
(km
)
−50 0 5090
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160
20:09:30
−50 0 5090
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160
20:10:00
Alti
tude
(km
)
−50 0 5090
100
110
120
130
140
150
160
20:10:30
−50 0 5090
100
110
120
130
140
150
160
20:11:00
Alti
tude
(km
)
North (km)−50 0 50
90
100
110
120
130
140
150
160
20:11:30
North (km)
70 km west of Kiruna
1997-02-16 ALIS/FAST/EISCAT
UNIS 2011-11-15 – p. 86
Auroral electron spectras,
from tomography,
4.5
5
5.5
6
6.5
7
7.5
8
8.5
9
200 400 600 800 1000 1200
100
101
102
time after 23:20:00 UT (s)
elec
tron
ene
rgy
log10
electron energy flux
UNIS 2011-11-15 – p. 89
Auroral electron spectras,
from tomography,
4.5
5
5.5
6
6.5
7
7.5
8
8.5
9
200 400 600 800 1000 1200
100
101
102
time after 23:20:00 UT (s)
elec
tron
ene
rgy
log10
electron energy flux
and from spectroscopicratios (right panel).
0.2
0.3
0.4
0.5
0.6
0.7
0.8
0.9
0 500 1000
−60
−40
−20
0
20
40
60
80
time after 23:20:00 UT (s)
N−
S d
ista
nce
Characteristic energy (keV)
0.15
0.2
0.25
0.3
0.35
0 500 1000
−60
−40
−20
0
20
40
60
80
time after 23:20:00 UT (s)
N−
S d
ista
nce
Oxygen scaling factor
40
60
80
100
120
140
160
0 500 1000
−50
0
50
time after 23:20:00 UT (s)
N−
S d
ista
nce
4278 A
30
40
50
60
70
80
90
100
110
0 500 1000
−50
0
50
time after 23:20:00 UT (s)
N−
S d
ista
nce
8446 A
50
100
150
200
250
0 500 1000
−50
0
50
time after 23:20:00 UT (s)
N−
S d
ista
nce
6300 A
After Gustavsson et al. [2001b], Phys. Chem. Earth 26.
UNIS 2011-11-15 – p. 89
filter/expose sequence
0 2 4 6 8 10 12 14 16 18 20
Bus
Kiruna
Optlab
Abisko
time (s)
Filter/exposure sequence: sync−rapid−aeronomi
UNIS 2011-11-15 – p. 91
RIOEALIS made the first unambigous observation of
high-latitude RIOE 1999-02-1617:40:15 17:40:35 17:40:55 17:41:15 17:41:35 17:41:55
0
1000
2000
3000
4000
17:43:55 17:44:05 17:44:15 17:44:25 17:44:35 17:44:45
0
1000
2000
3000
4000
After [Brandstrom et al., 1999], GRL, 26.
UNIS 2011-11-15 – p. 97
Tomography of RIOE
After Gustavsson et al. [2001a], JGR
106, 29
ALIS made the first tomo-graphic estimate of volumedistribution of RIOE.
UNIS 2011-11-15 – p. 98
A strange meteor trail
130
120
110
100
95
1
2
3
4
5
6
7
8
9
10
x 104
95
100
110
2000
2500
3000
3500
4000
4500
5000
4227 Å (left) 5893 Å (right)After Pellinen-Wannberg et al. [2004, GRL 31], GRL 31.
UNIS 2011-11-15 – p. 102
Polar-Stratospheric clouds
−20 −10 0
40
50
60
70
Triangulation
212223
24
25
26
After Enell [2002], IRF Sci. Rep. 278
UNIS 2011-11-15 – p. 103
Small structureThe aurora is extremly rich in small structure
“With respect to understanding thedynamic coupling between themagnetosphere and the auroralionosphere the observational bias towardbright aurora is physically unjustified”[Semeter 2001]
UNIS 2011-11-15 – p. 105
We do not understand:• Creation of narrow arcs• Diffuse aurora• Pulsating aurora
UNIS 2011-11-15 – p. 106
We do not understand:• Creation of narrow arcs• Diffuse aurora• Pulsating aurora• The role of the ionosphere in the
magnetosphere-ionosphere coupling
UNIS 2011-11-15 – p. 106
We do not understand:• Creation of narrow arcs• Diffuse aurora• Pulsating aurora• The role of the ionosphere in the
magnetosphere-ionosphere coupling• How are different scales related to each
other?
UNIS 2011-11-15 – p. 106
We do not understand:• Creation of narrow arcs• Diffuse aurora• Pulsating aurora• The role of the ionosphere in the
magnetosphere-ionosphere coupling• How are different scales related to each
other?
Thus we need instruments measuring differentscales with high temporal and spatial resolution,e.g. Polar/VIS, ASC, ALIS, ASK
UNIS 2011-11-15 – p. 106
ALIS 2010–2014• Electrodynamics of auroral structures: get
most out of EISCAT-UHF• ALIS/EISCAT/REIMEI• Improve temporal resolution: EMCCD• Review which sites to use• Ionospheric sounding rockets?• Collaboration for development of methods
and models• Calibration!!!• Improve access to data
UNIS 2011-11-15 – p. 107
In particularwe will work to answer the following specificquestions:
1. What is the temporal and spatial scaledistribution of small (less than a few km)auroral structures?.
2. What are the temporal and spatial variationsof the primary particle distributions causingsmall auroral structures?
3. What is the detailed 3D electrodynamics ofsmall auroral structures?
4. How does ionospheric feedback influenceauroral structure?
UNIS 2011-11-15 – p. 108
My brain hurts!
Mr. T. F. Gumby:—Doctor! Doctor! DOCTOR! DOCTOR! Doctor!
— Are you the brain specialist? — My brain hurts!
http://www.mwscomp.com/mpfc/gumbrain.htmlUNIS 2011-11-15 – p. 110
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