ARTICLE IN PRESS
Nuclear Instruments and Methods in Physics Research A 524 (2004) 169–194
Muon trackreconstruction and data selection techniques
in
AMANDA
J. Ahrens
a
, X. Bai
b
, R. Bay
c
, S.W. Barwick
d
, T. Becka
a
, J.K. Becker
e
, K.-
H. Becker
e
, E. Bernardini
f
, D. Bertrand
g
, A. Biron
f
, D.J. Boersma
f
,S.B
.
oser
f
,
O. Botner
h
, A. Bouchta
h
, O. Bouhali
g
, T. Burgess
i
, S. Carius
j
, T. Castermans
k
,
D. Chirkin
c
, B. Collin
l
, J. Conrad
h
, J. Cooley
m
, D.F. Cowen
l
, A. Davour
h
,
C. De Clercq
n
, T. DeYoung
o
, P. Desiati
m
, J.-P. Dewulf
g
, P. Ekstr
.
om
e
, T. Feser
a
,
M. Gaug
f
, T.K. Gaisser
b
, R. Ganugapati
m
, H. Geenen
e
, L. Gerhardt
d
, A. Gro
X
e
,
A. Goldschmidt
p
, A. Hallgren
h
, F. Halzen
m
, K. Hanson
m
, R. Hardtke
m
,
T.Harenberg
e
,T.Hauschildt
f
,K.Helbing
p
,M.Hellwig
a
,P.Herquet
k
,G.C.Hill
m
,
D. Hubert
n
, B. Hughey
m
, P.O. Hulth
i
, K. Hultqvist
i
, S. Hundertmark
i
,
J. Jacobsen
p
, A. Karle
m
, M. Kestel
l
,L.K
.
opke
a
, M. Kowalski
f
, K. Kuehn
d
,
J.I. Lamoureux
p
, H. Leich
f
, M. Leuthold
f
, P. Lindahl
j
, I. Liubarsky
q
, J. Madsen
r
,
P. Marciniewski
h
, H.S. Matis
p
, C.P. McParland
p
, T. Messarius
e
, Y. Minaeva
i
,
P. Mio
W
inovi
!
c
c
, P.C. Mock
d
, R. Morse
m
, K.S. M
.
unich
e
, J. Nam
d
, R. Nahnhauer
f
,
T. Neunh
.
offer
a
, P. Niessen
n
, D.R. Nygren
p
,H.
.
Ogelman
m
, Ph. Olbrechts
n
,
C. P
!
erez de los Heros
h
, A.C. Pohl
i
, R. Porrata
d
, P.B. Price
c
, G.T. Przybylski
p
,
K. Rawlins
m
, E. Resconi
f
, W. Rhode
e
, M. Ribordy
k
, S. Richter
m
, J. Rodr
!
ıguez
Martino
i
, D. Ross
d
, H.-G. Sander
a
, K. Schinarakis
e
, S. Schlenstedt
f
, T. Schmidt
f
,
D.Schneider
m
,R.Schwarz
m
,A.Silvestri
d
,M.Solarz
c
,G.M.Spiczak
r
,C.Spiering
f
,
M. Stamatikos
m
, D. Steele
m
, P. Steffen
f
, R.G. Stokstad
p
, K.-H. Sulanke
f
,
O. Streicher
f
, I. Taboada
s
, L. Thollander
i
, S. Tilav
b
, W. Wagner
e
, C. Walck
i
,
Y.-R. Wang
m
, C.H. Wiebusch
e,
*, C. Wiedemann
i
, R. Wischnewski
f
, H. Wissing
f
,
K. Woschnagg
c
, G. Yodh
d
a
Institute of Physics, University of Mainz, D55099 Mainz, Germany
b
Bartol Research Institute, University of Delaware, Newark, DE 19716, USA
c
Department of Physics, University of California, Berkeley, CA 94720, USA
d
Department of Physics and Astronomy, University of California, Irvine, CA 92697, USA
e
Fachbereich 8 Physik, BU Wuppertal, Gaussstrasse 20, D42119 Wuppertal, Germany
f
DESYZeuthen, D15738 Zeuthen, Germany
g
Universit
!
e Libre de Bruxelles, Science Faculty, Brussels, Belgium
h
Division of High Energy Physics, Uppsala University, S75121 Uppsala, Sweden
*Corresponding author. Tel.: +49-0-202-439-3531; fax: +49-0-202-439-2662.
E-mail address:
wiebusch@physik.uni-wuppertal.de (C.H. Wiebusch).
0168-9002/$ - see front matter
r
2004 Elsevier B.V. All rights reserved.
doi:10.1016/j.nima.2004.01.065
i
Department of Physics, Stockholm University, SE10691 Stockholm, Sweden
j
Department of Technology, Kalmar University, S39182 Kalmar, Sweden
k
University of MonsHainaut, 7000 Mons, Belgium
l
Department of Physics, Pennsylvania State University, University Park, PA 16802, USA
m
Department of Physics, University of Wisconsin, Madison, WI 53706, USA
n
Vrije Universiteit Brussel, Dienst ELEM, B1050 Brussels, Belgium
o
Department of Physics, University of Maryland, College Park, MD 20742, USA
p
Lawrence Berkeley National Laboratory, Berkeley, CA 94720, USA
q
Blackett Laboratory, Imperial College, London SW7 2BW, UK
r
Physics Department, University of Wisconsin, River Falls, WI 54022, USA
s
Department de F
!
ısica, Universidad Sim
!
on Bol
!
ıvar, Caracas, 1080, Venezuela
The AMANDA Collaboration
Received 24 September 2003; received in revised form 20 January 2004; accepted 27 January 2004
Abstract
The Antarctic Muon And Neutrino Detector
A
rray (AMANDA) is a high-energy neutrino telescope operating at the
geographic South Pole. It is a lattice of photo-multiplier tubes buried deep in the polar ice between 1500 and 2000 m
:
The primary goal of this detector is to discover astrophysical sources of high-energy neutrinos. A high-energy muon
neutrino coming through the earth from the Northern Hemisphere can be identified by the secondary muon moving
upward through the detector.
The muon tracks are reconstructed with a maximum likelihood method. It models the arrival times and amplitudes of
Cherenkov photons registered by the photo-multipliers. This paper describes the different methods of reconstruction,
which have been successfully implemented within
AMANDA
. Strategies for optimizing the reconstruction performance and
rejecting background are presented. For a typical analysis procedure the direction of tracks are reconstructed with
about 2
?
accuracy.
r
2004 Elsevier B.V. All rights reserved.
PACS:
95.55.Vj; 95.75.Pq; 29.40.Ka; 29.85.+c
Keywords:
AMANDA
; Trackreconstruction; Neutrino telescope; Neutrino astrophysics
1. Introduction
The Antarctic Muon And Neutrino Detector
Array
[1],
AMANDA
, is a large volume neutrino
detector at the geographic South Pole. It is a lattice
of photo-multiplier tubes (PMTs) buried deep in
the optically transparent polar ice. The primary
goal of this detector is to detect high-energy
neutrinos from astrophysical sources, and deter-
mine their arrival time, direction and energy.
When a high-energy neutrino interacts in the
polar ice via a charged current reaction with a
nucleon
N
:
n
c
þ
N
c
þ
X
;
ð
1
Þ
it creates a hadronic cascade, X, and a lepton,
c
¼
e
;
m
;
t
:
These particles generate Cherenkov
photons, which are detected by the PMTs. Each
lepton flavor generates a different signal in the
detector. The two basic detection modes are
sketched in Fig. 1.
A high-energy
n
m
charged current interaction
creates a muon, which is nearly collinear with the
neutrino direction; having a mean deviation angle
of
c
¼
0
:
7
?
?ð
E
n
=
TeV
Þ
?
0
:
7
[2], which implies an
accuracy requirement of
t
1
?
for reconstructing
the muon direction.
The high-energy muon emits a cone of Cher-
enkov light at a fixed angle
y
c
:
It is determined by
cos
y
c
¼ð
n
b
Þ
?
1
;
where
n
C
1
:
32 is the index of
ARTICLE IN PRESS
J. Ahrens et al. / Nuclear Instruments and Methods in Physics Research A 524 (2004) 169–194
170
refraction in the ice. For relativistic particles,
b
C
1
;
and
y
c
E
41
?
:
The direction of the muon is
reconstructed from the time and amplitude in-
formation of the PMTs illuminated by the
Cherenkov cone.
Radiative energy loss processes generate sec-
ondary charged particles along the muon trajec-
tory, which also produce Cherenkov radiation.
These additional photons allow an estimate of the
muon energy. However, the resolution is limited
by fluctuations of these processes. This estimate is
a lower bound on the neutrino energy, because it is
based on the muon energy at the detector. The
interaction vertex may be far outside the detector.
The
n
e
and
n
t
channels are different. The
electron from a
n
e
will generate an electro-
magnetic cascade, which is confined to a volume
of a few cubic meters. This cascade coincides with
the hadronic cascade X of the primary interaction
vertex. The optical signature is an expanding
spherical shell of Cherenkov photons with a lar-
ger intensity in the forward direction. The tau
from a
n
t
will decay immediately and also gene-
rate a cascade. However, at energies
>
1 PeV this
cascade and the vertex are separated by several
tens of meters, connected by a single track. This
signature of two extremely bright cascades is
unique for high-energy
n
t
;
and it is called a
double
bang event
[3].
The measurement of cascade-like events is
restricted to interactions close to the detector,
thus requiring larger instrumented volumes than
for
n
m
detection. Also the accuracy of the direction
measurement is worse for cascades than for long
muon tracks. However, when the flux is diffuse,
the
n
e
and
n
t
channels also have clear advantages.
The backgrounds from atmospheric neutrinos are
smaller. The energy resolution is significantly
better since the full energy is deposited in or near
the detector. The cascade channel is sensitive to all
neutrino flavors because the neutral current
interactions also generate cascades. In this paper,
we focus on the reconstruction of muon tracks;
details on the reconstruction of cascades are
described in Ref. [4].
The most abundant events in
AMANDA
are atmo-
spheric muons, created by cosmic rays interacting
with the Earth’s atmosphere. At the depth of
AMANDA
their rate exceeds the rate of muons from
atmospheric neutrinos by five orders of magni-
tude. Since these muons are absorbed by the earth,
a muon trackfrom the lower hemisphere is a
unique signature for a neutrino-induced muon.
1
The reconstruction procedure must have good
angular resolution, good efficiency, and allow
excellent rejection of down-going atmospheric
muons.
This paper describes the methods used to
reconstruct muon tracks recorded in the
AMANDA
experiment. The
AMANDA-II
detector is introduced
in Section 2. The reconstruction algorithms and
their implementation are described in Sections 3–5.
ARTICLE IN PRESS
cascade
muon
PMTs
c
spherical Cherenkov front
Cherenkov cone
Fig. 1. Detection modes of the
AMANDA
detector: Left: muon tracks induced by muon-neutrinos; Right: Cascades from electron- or tau-
neutrinos.
1
Muon neutrinos above 1 PeV are absorbed by the Earth. At
these ultra-high-energies (UHE), however, the muon back-
ground from cosmic rays is small and UHE muons coming
from the horizon and above are most likely created by UHE
neutrinos. The search for these UHE neutrinos is described in
Refs. [5,6].
J. Ahrens et al. / Nuclear Instruments and Methods in Physics Research A 524 (2004) 169–194
171
Section 6 summarizes event classes for which the
reconstruction may fail and strategies to identify
and eliminate such events. The performance
of the reconstruction procedure is shown in
Section 7. We discuss possible improvements
in Section 8.
2. The AMANDA detector
The
AMANDA-II
detector (see
Fig. 2) has been
operating since January 2000 with 677 optical
modules (OM) attached to 19 strings. Most of the
OMs are located between 1500 and 2000 m below
the surface. Each OM is a glass pressure vessel,
which contains an 8-in. hemispherical PMT and its
electronics.
AMANDA-B10
,
2
the inner core of 302
OMs on 10 strings, has been operating since 1997.
One unique feature of
AMANDA
is that it
continuously measures atmospheric muons in
coincidence with the
South Pole Air Shower
Experiment
surface arrays
SPASE-1
and
SPASE-2
[7]. These muons are used to survey the detector
and calibrate the angular resolution (see Section 7
and
Refs. [8,9]), while providing
SPASE
with
additional information for cosmic ray composition
studies [10].
The PMT signals are processed in a counting
room at the surface of the ice. The analog signals
are amplified and sent to a majority logic trigger
[11]. There the pulses are discriminated and a
trigger is formed if a minimum number of hit
PMTs are observed within a time window of
typically 2
m
s
:
Typical trigger thresholds were 16
hit PMT for
AMANDA-B10
and 24 for
AMANDA-II
.
For each trigger the detector records the peak
amplitude and up to 16 leading and trailing edge
times for each discriminated signal. The time
resolution achieved after calibration is
s
t
C
5ns
for the PMTs from the first 10 strings, which are
read out via coaxial or twisted pair cables. For the
remaining PMTs, which are read out with optical
fibers the resolution is
s
t
C
3
:
5ns
:
In the cold
environment of the deep ice the PMTs have low
noise rates of typically 1 kHz
:
The timing and amplitude calibration, the array
geometry, and the optical properties of the ice are
determined by illuminating the array with known
optical pulses from in situ sources [11]. Time
offsets are also determined from the response to
through-going atmospheric muons[12].
ARTICLE IN PRESS
light diffuser ball
HV divider
silicon gel
Module
Optical
pressure
housing
Depth
120 m
AMANDAII
AMANDAB10
Inner 10 strings:
zoomed in on one
optical module (OM)
main cable
PMT
200 m
1000 m
2350 m
2000 m
1500 m
1150 m
Fig. 2. The
AMANDA-II
detector. The scale is illustrated by the Eiffel tower at the left.
2
Occasionally in the paper we will refer to this earlier
detector instead of the full
AMANDA-II
detector.
J. Ahrens et al. / Nuclear Instruments and Methods in Physics Research A 524 (2004) 169–194
172
The optical absorption length in the ice is
typically 110 m at 400 nm with a strong wave-
length dependence. The effective scattering length
at 400 nm is on average
C
20 m
:
It is defined as
l
s
=
ð
1
?
/
cos
y
s
S
Þ
;
where
l
s
is the scattering length
and
y
s
is the scattering angle. The ice parameters
vary strongly with depth due to horizontal ice
layers, i.e., variations in the concentration of
impurities which reflect past geological events
and climate changes [13–19].
3. Reconstruction algorithms
The muon trackreconstruction algorithm is a
maximum likelihood procedure. Prior to recon-
struction simple pattern recognition algorithms,
discussed in Section 4, generate the initial esti-
mates required by the maximum likelihood recon-
structions.
3.1. Likelihood description
The reconstruction of an event can be general-
ized to the problem of estimating a set of unknown
parameters
f
a
g
;
e.g. trackparameters, given a set
of experimentally measured values
f
x
g
:
The
parameters,
f
a
g
;
are determined by maximizing
the likelihood
L
ð
x
j
a
Þ
which for independent
components
x
i
of
x
reduces to
L
ð
x
j
a
Þ¼
Y
i
p
ð
x
i
j
a
Þð
2
Þ
where
p
ð
x
i
j
a
Þ
is the probability density function
(p.d.f.) of observing the measured value
x
i
for
given values of the parameters
f
a
g
[20].
To simplify the discussion we assume that the
Cherenkov radiation is generated by a single
infinitely long muon track(with
b
¼
1) and forms
a cone. It is described by the following parameters:
a
¼ð
r
0
;
t
0
;
#
p
;
E
0
Þð
3
Þ
and illustrated inFig. 3. Here,
r
0
is an arbitrary
point on the track. At time
t
0
;
the muon passes
r
0
with energy
E
0
along a direction
#
p
:
The geome-
trical coordinates contain five degrees of freedom.
Along this track, Cherenkov photons are emitted
at a fixed angle
y
c
relative to
#
p
:
Within the
reconstruction algorithm it is possible to use a
different coordinate system, e.g.
a
¼ð
d
;
Z
;
y
Þ
:
The
reconstruction is performed by minimizing
?
log
ð
L
Þ
with respect to
a
:
The values
f
x
g
presently recorded by
AMANDA
are
the time
t
i
and duration
TOT
i
(
Time Over
Threshold
) of each PMT signal, as well as the
peakamplitude
A
i
of the largest pulse in each
PMT. PMTs with no signal above threshold are
also accounted for in the likelihood function. The
hit times give the most relevant information.
Therefore we will first concentrate on
p
ð
t
j
a
Þ
:
3.1.1. Time likelihood
According to the geometry in Fig. 3, photons
are expected to arrive at OM
i
(at
r
i
) at time
t
geo
¼
t
0
þ
#
p
?ð
r
i
?
r
0
Þþ
d
tan
y
c
c
vac
ð
4
Þ
with
c
vac
the vacuum speed of light.
3
It is
convenient to define a relative arrival time, or
time residual
t
res
?
t
hit
?
t
geo
ð
5
Þ
which is the difference between the observed hit
time and the hit time expected for a ‘‘direct
photon’’, a Cherenkov photon that travels un-
delayed directly from the muon to an OM without
scattering.
ARTICLE IN PRESS
c
θ
c
θ
OM
µ
d
x
Cherenkov light
t , , E
0 0 0
PMTaxis
η
p
r
r
i
Fig. 3. Cherenkov light front: definition of variables.
3
We note that Eq. (4) neglects the effect that Cherenkov light
propagates with group velocity as pointed out in Ref. [21].It
was shown inRef. [14]that for AMANDA this approximation
is justified.
J. Ahrens et al. / Nuclear Instruments and Methods in Physics Research A 524 (2004) 169–194
173
In the ideal case, the distribution,
p
ð
t
res
j
a
Þ
;
would be a delta function. However, in a realistic
experimental situation this distribution is broa-
dened and distorted by several effects, which are
illustrated in
Fig. 4. The PMT jitter limits the
timing resolution
s
t
:
Noise, e.g. darknoise of the
PMT, leads to additional hits which are random in
time. These effects can generate negative
t
res
values, which would mimic unphysical causality
violations. Secondary radiative energy losses along
the muon trajectory create photons that arrive
after the ideal Cherenkov cone. These processes
are stochastic, and their relative photon yield
fluctuates.
In
AMANDA
, the dominant effect on photon
arrival times is scattering in the ice.
4
The effect
of scattering depends strongly on the distance,
d
;
of the OM from the trackas illustrated in
Fig. 4.
Since the PMTs have a non-uniform angular
response,
p
ð
t
res
Þ
also depends on the orientation,
Z
;
of the OM relative to the muon track(see
Fig.
3). OMs facing away from the trackcan only see
light that scatters backtowards the PMT face. On
average this effect shifts
t
res
to later times and
modifies the probability of a hit.
The simplest time likelihood function is based
on a likelihood constructed from
p
1
;
the p.d.f. for
arrival times of single photons
i
at the locations of
the hit OMs
L
time
¼
Y
N
hits
i
¼
1
p
1
ð
t
res
;
i
j
a
¼
d
i
;
Z
i
;
y
Þ
:
ð
6
Þ
Note that one OM may contribute to this product
with several hits. The function
p
1
ð
t
res
;
i
j
a
Þ
is
obtained from the simulation of photon propaga-
tion through ice (see Section 3.2). However, this
description is limited, because the electrical and
optical signal channels can only resolve multiple
photons separated by a few 100 ns and
C
10 ns
;
respectively. Within this time window, only the
arrival time of the first pulse is recorded.
This first photon is usually less scattered than
the average single photon, which modifies the
probability distribution of the detected hit time.
The arrival time distribution of the first of
N
photons is given by
p
1
N
ð
t
res
Þ¼
Np
1
ð
t
res
Þ
Z
N
t
res
p
1
ð
t
Þ
d
t
??
ð
N
?
1
Þ
¼
Np
1
ð
t
tres
Þð
1
?
P
1
ð
t
res
ÞÞ
ð
N
?
1
Þ
ð
7
Þ
P
1
is the cumulative distribution of the single
photon p.d.f. The function
p
1
N
ð
t
res
Þ
is called the
multi-photo-electron (MPE) p.d.f. and corre-
spondingly defines
L
MPE
:
This concept can be extended to the more
general case of
p
k
N
ð
t
res
Þ
;
the p.d.f. for the
k
th
photon out of a total of
N
to arrive at
t
res
;
given by
p
k
N
ð
t
res
Þ¼
N
N
?
1
k
?
1
!
p
1
ð
t
res
Þð
1
?
P
1
ð
t
res
ÞÞ
ð
N
?
k
Þ
?ð
P
1
ð
t
res
ÞÞ
ð
k
?
1
Þ
ð
8
Þ
p
k
N
ð
t
res
Þ
specifies the likelihood of arrival times of
individual photoelectrons for averaged time series
of
N
photoelectrons. With waveform recording the
arrival times and amplitudes of individual pulses
can be resolved.
When the number of photoelectrons,
N
;
is not
measured precisely enough, multi-photon informa-
tion can be included via another method. Instead
ARTICLE IN PRESS
t
res
t
res
t
res
t
res
00
high
low
00
+ showers + scattering
close track
far track
+ noise
t
jitter
jitter jitter
jitter
Fig. 4. Schematic distributions of arrival times
t
tes
for different
cases: Top left: PMT jitter. Top right: the effect of jitter and
random noise. Bottom left: The effect of jitter and secondary
cascades along the muon track. Bottom right: The effect of
jitter and scattering.
4
In water detectors this effect is neglected[22]or treated as a
small correction[23].
J. Ahrens et al. / Nuclear Instruments and Methods in Physics Research A 524 (2004) 169–194
174
of measuring
N
;
the p.d.f. of the first photoelec-
tron can be calculated by convolving the MPE
p.d.f.
p
1
N
ð
t
;
d
Þ
with the Poisson probability
P
Poisson
N
ð
m
Þ
;
where
m
is the mean expected number
of photoelectrons as a function of the distance,
d
:
p
1
m
ð
t
res
Þ¼
1
N
X
N
i
¼
1
m
i
e
?
m
i
!
p
1
i
ð
t
res
Þ
¼
m
1
?
e
?
m
p
1
ð
t
res
Þ
e
?
m
P
1
ð
t
res
Þ
ð
9
Þ
This result is called the Poisson Saturated Ampli-
tude (PSA) p.d.f.
[24,25]
and correspondingly
defines
L
PSA
:
The constant
N
¼
1
?
e
?
m
renorma-
lizes the p.d.f. to unity.
The probability of (uncorrelated) noise hits is
small. They are further suppressed by a
hit cleaning
procedure (Section 5.3), which is applied before
reconstruction. They are included in the likelihood
function by simply adding a constant p.d.f.
p
0
:
3.1.2. Hit and nohit likelihood
The likelihood in the previous section relies only
on the measured arrival times of photons. How-
ever, the topology of the hits is also important.
PMTs with no hits near a hypothetical trackor
PMTs with hits far from the trackare unlikely.
A likelihood utilizing this information can be
constructed as
L
hit
¼
Y
N
ch
i
¼
1
P
hit
;
i
Y
N
OM
i
¼
N
ch
þ
1
P
no
?
hit
;
i
ð
10
Þ
where
N
ch
is the number of hit OMs and
N
OM
the
number of operational OMs. The probabilities
P
hit
and
P
no
?
hit
of observing or not observing a hit
depend on the trackparameters
a
:
Additional hits
due to random noise are easily incorporated:
P
no
?
hit
*
P
no
?
hit
?
P
no
?
hit
P
no
?
noise
and
P
hit
*
P
hit
¼
1
?
*
P
no
?
hit
:
Assuming that the probability
P
hit
1
is known for
a single photon, the hit and no-hit probabilities of
OMs for
n
photons can be calculated:
P
no
?
hit
n
¼ð
1
?
P
hit
1
Þ
n
and
P
hit
n
¼
1
?
P
no
?
hit
n
¼
1
?ð
1
?
P
hit
1
Þ
n
:
ð
11
Þ
The number of photons,
n
;
depends on
E
m
;
the
energy of the muon:
n
¼
n
ð
E
m
Þ
:
For a fixed track
geometry, the likelihood (Eq. (10)) can be used to
reconstruct the muon energy.
3.1.3. Amplitude likelihood
The peakamplitudes recorded by
AMANDA
can be
fully incorporated in the likelihood [26], which is
particularly useful for energy reconstruction. The
likelihood can be written as
L
¼
W
N
OM
Y
N
OM
i
¼
1
w
i
P
i
ð
A
i
Þð
12
Þ
where
P
i
ð
A
i
Þ
is the probability that OM
i
observes
an amplitude
A
i
;
with
A
i
¼
0 for unhit OMs.
W
and
w
i
are weight factors, which describe devia-
tions of the individual OM and the total number of
hit OMs from the expectation.
P
i
depends on the
mean number
m
of expected photoelectrons:
P
i
ð
A
i
Þ¼
P
hit
ð
1
?
P
th
i
Þ
P
ð
A
i
;
m
Þ
P
ð
/
A
i
S
;
m
Þ
:
ð
13
Þ
The probability
P
i
ð
A
i
Þ
is normalized to the
probability of observing the most likely amplitude
/
A
i
S
:
P
th
i
ð
m
Þ
is the probability that a signal of
m
does not produce a pulse amplitude above the
discriminator threshold. As before,
P
hit
¼
1
?
P
no
?
hit
;
where the no-hit probability is given
by Poisson statistics:
P
no
?
hit
¼
exp
ð?
m
Þð
1
?
P
noise
Þ
:
The probability of
A
i
¼
0 is a special case:
P
i
ð
0
Þ¼
P
no
?
hit
þ
P
hit
P
th
i
:
Energy reconstructions based on
this formulation of the likelihood will be referred
to as
Full E
reco
:
An alternative energy reconstruction technique
(see Section 3.2.4) uses a neural net which is fed
with energy sensitive parameters.
3.1.4. Zenith weighted (Bayesian) likelihood
Another extension of the likelihood
[27–29]
incorporates external information about the muon
flux via Bayes’ Theorem. This theorem states that
for two hypotheses
A
and
B
;
P
ð
A
j
B
Þ¼
P
ð
B
j
A
Þ
P
ð
A
Þ
P
ð
B
Þ
:
ð
14
Þ
Identifying
A
with the trackparameters
a
and
B
with the observations
x
;
Eq. (14) gives the prob-
ability that the inferred muon track
a
was in fact
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J. Ahrens et al. / Nuclear Instruments and Methods in Physics Research A 524 (2004) 169–194
175
responsible for the observed event
x
:
P
ð
x
j
a
Þ
is the
probability that
a
;
assumed to be true, would
generate the event
x
—in other words, the like-
lihood described in the previous sections.
P
ð
a
Þ
is
the prior probability of observing the track
a
;
i.e.,
the relative frequencies of different muon tracks as
a function of their parameters.
P
ð
x
Þ
;
which is
independent of the trackparameters
a
;
is a
normalization constant which ensures that
Eq. (14) defines a proper probability. Because the
likelihood is only defined up to an arbitrary
constant factor, this normalization may be ignored
in the present context.
In order to obtain
P
ð
a
j
x
Þ
;
one thus has to
determine the prior probability distribution,
P
ð
a
Þ
;
of how likely the various possible track directions
are a priori. The reconstruction maximizes the
product of the p.d.f.
and
the prior.
The flux of muons deep underground is reason-
ably well known from previous experiments. Any
point source of muons would be at most a small
perturbation on the flux of penetrating atmo-
spheric muons and muons created by atmospheric
neutrinos. The most striking feature of the back-
ground flux from atmospheric muons is the strong
dependence on zenith angle. For vertically down-
going tracks it exceeds the flux from neutrino
induced muons by about 5 orders of magnitude
but becomes negligible for up-going tracks. This
dependence, which is modeled by a Monte Carlo
calculation [30], acts as a zenith dependent weight
to the different muon hypotheses,
a
:
With this
particular choice, some tracks, which would
otherwise reconstruct as up-going, reconstruct as
down-going tracks. This greatly reduces the rate at
which penetrating atmospheric muons are mis-
reconstructed as up-going neutrino events [31].In
principle, a more accurate prior could be used. It
would need to include the depth and energy
dependence of the atmospheric muons as well as
the angular dependence of atmospheric neutrino-
induced muons.
Upon completion of this work, we learned that
this technique was developed independently by the
NEVOD neutrino detector collaboration[32]who
were able to extract an atmospheric neutrino from
a background of 10
10
atmospheric muons in a
small
ð
6
?
6
?
7
:
5m
3
Þ
surface detector.
3.1.5. Combined likelihoods
The likelihood function
L
time
of the hit times is
the most important for trackreconstruction.
However, it is useful to include other information
like the hit probabilities. The combined p.d.f. from
Eqs. (7)–(10) is
L
MPE
"
P
hit
P
no
?
hit
¼
L
MPE
ð
L
hit
Þ
w
ð
15
Þ
which is particularly effective. Here
w
is an
optional weight factor which allows the adjust-
ment of the relative weight of the two likelihoods.
This likelihood is sensitive not only to the track
geometry but also to the energy of the muon.
As discussed in Section 3.1.4, the zenith angle-
dependent prior function,
P
ð
y
Þ
;
can be included as
a multiplicative factor. This combination
L
Bayes
¼
P
ð
y
Þ
L
time
ð
16
Þ
has been used in the analysis of atmospheric
neutrinos
[30]. However, all of these improved
likelihoods are limited by the underlying model
assumption of a single muon track.
3.2. Likelihood implementation
The actual implementation of the likelihoods
requires detailed knowledge of the photon propa-
gation in the ice. On the other hand, efficiency
considerations and numeric problems favor a
simple and robust method.
The photon hit probabilities and arrival time
distributions are simulated as functions of all
relevant parameters with a dedicated Monte Carlo
simulation and archived in large look-up tables.
This simulation is described in Refs. [26,30,33]
The
AMANDA
Collaboration has followed differ-
ent strategies for incorporating this data into the
reconstruction. In principle the probability density
functions are taken directly from these archives.
However, one has to face several technical
difficulties due to the memory requirements of
the archived tables, as well as numeric problems
related to the normalization of interpolated bins
and the calculation of multi-photon likelihoods.
Alternatively, one can simplify the model and
parametrize these archives with analytical func-
tions, which depend only on a reduced set of
parameters. Comparisons of two independent
ARTICLE IN PRESS
J. Ahrens et al. / Nuclear Instruments and Methods in Physics Research A 524 (2004) 169–194
176
parametrizations [24,34] show that the direct and
parametrized approaches yield similar results in
terms of efficiency. This indicates that the para-
metrization itself is not limiting the reconstruction
quality; rather, as mentioned earlier, the recon-
struction is limited by the assumptions of the
model being fit. Therefore, we will concentrate on
only one parametrization.
3.2.1. Analytical parametrization
A simple parametrization of the arrival time
distributions can be achieved with the following
function, which we call
Pandel function
.Itisa
gamma distribution and its usage is motivated by
an analysis of laser light signals in the BAIKAL
experiment[35]. There, it was found that for the
case of an isotropic, monochromatic and point-
like light source,
p
1
ð
t
res
Þ
can be expressed in the
form
p
ð
t
res
Þ?
1
N
ð
d
Þ
t
?ð
d
=
l
Þ
t
ð
d
=
l
?
1
Þ
res
G
ð
d
=
l
Þ
?
e
?
t
res
1
t
þ
c
medium
l
a
??
þ
d
l
a
??
ð
17
Þ
N
ð
d
Þ¼
e
?
d
=
l
a
1
þ
t
c
medium
l
a
??
?
d
=
l
ð
18
Þ
without special assumptions on the actual optical
parameters. Here,
c
medium
¼
c
vac
=
n
is the speed of
light in ice,
l
a
the absorption length,
G
ð
d
=
l
Þ
the
Gamma function and
N
ð
d
Þ
a normalization factor,
which is given by Eq. (18). This formulation has
free parameters
l
and
t
;
which are unspecified
functions of the distance
d
and the other geome-
trical parameters. They are empirically determined
by a Monte Carlo model.
The Pandel function has some convenient
mathematical properties: it is normalized, it is
easy to compute, and it can be integrated
analytically over the time,
t
res
;
which simplifies
the construction of the multi-photon (MPE) time
p.d.f.. For small distances the function has a pole
at
t
¼
0 corresponding to a high probability of an
unscattered photon. Going to larger values of
d
;
longer delay times become more likely. For
distances larger than the critical value
d
¼
l
;
the
power index to
t
res
changes sign, reflecting that the
probability of undelayed photons vanishes: essen-
tially all photons are delayed due to scattering.
The large freedom in the choice of the two
parameter functions
t
(units of time) and
l
(units
of length) and the overall reasonable behavior is
the motivation to use this function to parametrize
not only the time p.d.f. for point-like sources, but
also for muon tracks [34]. The Pandel function is
fit to the distributions of delay times for fixed
distances
d
and angles
Z
(between the PMT axis
and the Cherenkov cone). These distributions are
previously obtained from a detailed photon
propagation Monte Carlo for the Cherenkov light
from muons. The free fit parameters are
t
;
l
;
l
a
and the effective distance
d
eff
;
which will be
introduced next.
When investigating the fit results as a function
of
d
and angle
Z
(see
Fig. 3), we observe that
already for a simple ansatz of constant
t
;
l
and
l
a
the optical properties in
AMANDA
are described
sufficiently well within typical distances. The
dependence on
Z
is described by an effective
distance
d
eff
which replaces
d
in Eq. (17). This
means that the time delay distributions for back-
ward illumination of the PMT is found to be
similar to a head-on illumination at a larger
distance. The following parameters are obtained
for a specific ice model, and are currently used in
the reconstruction:
t
¼
557 ns
;
d
eff
¼
a
0
þ
a
1
d
l
¼
33
:
3m
;
a
1
¼
0
:
84
l
a
¼
98 m
;
a
0
¼
3
:
1m
?
3
:
9 m cos
ð
Z
Þþ
4
:
6 m cos
2
ð
Z
Þ
:
ð
19
Þ
A comparison of the results from this parame-
trization with the full simulation is shown inFig. 5
for two extreme distances. The simple approxima-
tion describes the behavior of the full simulation
reasonably well. However, this simple overall
description has a limited accuracy, especially for
d
E
l
(not shown). Reconstructions, based on the
Pandel function with different ice models, and a
generic reconstruction, that uses the full simula-
tion results, yield similar results. These compar-
isons indicate that the results of the reconstruction
do not critically depend on the fine tuning of the
ARTICLE IN PRESS
J. Ahrens et al. / Nuclear Instruments and Methods in Physics Research A 524 (2004) 169–194
177
underlying ice models, and it justifies the use of the
above simple model.
3.2.2. Extension to realistic PMT signals
Although the Pandel function is the basis of a
simple normalized likelihood, it has several defi-
ciencies. It is not defined for negative
t
res
;
it ignores
PMT jitter, and it has a pole at
t
res
¼
0
;
which
causes numerical difficulties. These problems can
be resolved by convolving the Pandel function,
Eq. (17), with a Gaussian, which accounts for the
PMT jitter. Unfortunately such convolution re-
quires significant computing time.
Instead the Pandel function is modified by
extending it to negative times,
t
res
o
0
;
with a (half)
Gaussian of width
s
g
:
The effects of PMT jitter are
only relevant for small values of
t
res
:
For times
t
res
X
t
1
the original function is used, and the two
parts are connected by a spline interpolation (3rd
order polynomial). The result,
#
P
ð
t
res
Þ
;
is called
upandel function
.
Using
t
1
¼
ffiffiffiffiffiffi
2
p
p
s
g
and requiring further a
smooth interpolation and the normalization to
be unchanged, the polynomial coefficients
a
j
and
normalization of the Gaussian
N
g
can be calcu-
lated analytically
[34]. The free parameter
s
g
includes all timing uncertainties, not just the
PMT jitter. Good reconstruction results are
achieved for a large range 10
p
s
g
p
20 ns
:
3.2.3. P
hit
P
no
?
hit
Parametrization
The normalization
N
ð
d
Þ
in Eq. (18) is used to
construct a hit probability function,
P
hit
:
The
function
P
hit
n
with
P
hit
1
?
N
ð
d
Þ
;
is fit to the hit
probability determined by the full
AMANDA
detector
simulation, as a function of distance, orientation
and muon energy. The free parameters are the
Pandel parameters
t
and
l
;
l
a
;
#
d
and
˜
n
:
The
effective distance
#
d
;
is similar to the effective
distance in the Pandel parametrization. We define
˜
n as the power index of Eq. (11), which corre-
sponds to an effective number of photons. It is
important to understand that
N
ð
d
Þ
is not a hit
probability and
˜
n is not just a number of photons.
They are constructs, that are calibrated with a
Monte Carlo simulation. Technically, the power
index,
˜
n
?
N
in Eq. (11), factorizes into
˜
n
ð
Z
;
E
m
Þ¼
e
ð
Z
;
E
m
Þ
n
ð
E
m
Þ
:
The variable
n
;
where
n
¼
n
ð
E
Þ
;
is
related to the number of photons incident on the
PMT and its absolute efficiency. The factor
e
ð
Z
;
E
m
Þ
is related to the orientation dependent
PMT sensitivity but also accounts for the energy-
dependent angular emission profile of photons
with respect to the bare muon.
3.2.4. Energy reconstruction
The reconstruction of the trackgeometry is a
search for five parameters. If the muon energy is
added as a fit parameter, the minimization is
significantly slower. Therefore, the energy recon-
struction is performed in two steps. First, the track
geometry is reconstructed without the energy
parameter. Then these geometric parameters are
used in an energy reconstruction, that only
determines the energy. However, if the time
likelihood utilizes amplitude information, e.g. in
the combined likelihood, Eq. (7), or the PSA
likelihood, Eq. (9), the track parameters also
ARTICLE IN PRESS
time delay / ns
d = 8m
Delay prob / ns
time delay / ns
d = 71m
Delay prob / ns
10
−
4
10
−
3
10
−
2
10
−
1
0 200 400
10
−
7
10
−
6
10
−
5
10
−
4
10
−
3
0 500 1000 1500
Fig. 5. Comparison of the parametrized Pandel function (dashed curves) with the detailed simulation (blackhistograms) at two
distances
d
from the muon track.
J. Ahrens et al. / Nuclear Instruments and Methods in Physics Research A 524 (2004) 169–194
178
depend on the energy. In this case the energy and
geometric parameters must be reconstructed to-
gether. Currently, three different approaches are
used to reconstruct the muon energy. They are
compared in Section 7.3.
(1) The simplest method utilizes the
P
hit
P
no
?
hit
reconstruction (see Sections 3.1.2 and 3.2.3).
(2) The
Full E
reco
method (see Section 3.1.3)
models the measured amplitudes in a like-
lihood for reconstructing the energy. This
algorithm performs better, but it is more
dependent on the quality of the amplitude
calibration of the OMs.
(3) An alternative way to measure the energy is
based on a neural network
[36]. The neural
networkuses 6-6-3-1 and 6-3-5-1 feed-forward
architecture for
AMANDA-B10
and
AMANDA-II
,
respectively. The energy correlated variables
which are used as input are the mean of the
measured amplitudes (ADC), the mean and
RMS of the arrival times (LE) or pulse
durations (TOT), the total number of signals,
the number of OMs hit and the number of
OMs with exactly one hit.
Less challenging than a full reconstruction, a
lower energy threshold is determined by requiring
a minimum number of hit OMs. The number of hit
OMs is correlated with the energy of the muon.
Since celestial neutrinos are believed to have a
substantially harder spectrum than atmospheric
neutrinos, an excess of high multiplicity events
would indicate that a hard celestial source exists.
Values for this parameter determined from
AMANDA
data already set a tight upper limit on the diffuse
flux of high-energy celestial neutrinos [37].
3.2.5. Cascade reconstruction
The reconstruction of
cascade like events
is
described in detail elsewhere
[4]. The basic
approach is similar to the trackreconstruction. It
assumes events form a point light source with
photons propagating spherically outside with a
higher intensity in the forward direction. The
cascade reconstruction also uses the Pandel func-
tion (see Eq. (17)) with parameters that are specific
for cascades.
In several muon analyses, a cascade fit is used as
a competing model. In cases where the cascade fit
achieves a better likelihood than the track
reconstruction, the trackhypothesis is rejected.
In particular this is used as a selection criterion to
reject background events which are mis-recon-
structed due to bright secondary cascades.
4. First guess pattern recognition
The likelihood reconstructions need an initial
trackhypothesis to start the minimization. The
initial trackis derived from
first guess methods
,
which are fast analytic algorithms that do not
require an initial track.
4.1. Direct walk
A very efficient
first guess method
is the
direct
walk
algorithm. It is a pattern recognition algo-
rithm based on carefully selected hits, which were
most likely caused by direct photons.
The four step procedure starts by selecting
track
elements
, the straight line between any two hit
OMs at distance
d
;
which are hit with a time
difference
j
D
t
j
o
d
c
vac
þ
30 ns with
d
>
50 m
:
ð
20
Þ
The known positions of the OMs define the track
element direction
ð
y
;
f
Þ
:
The vertex position
ð
x
;
y
;
z
Þ
is taken at the center between the two
OMs. The time at the vertex
t
0
is defined as the
average of the two hit times.
In a next step, the number of
associated hits
(AH) are calculated for each trackelement.
Associated hits are those with
?
30
o
t
res
o
300 ns
and
d
o
25 m
ð
t
res
þ
30
Þ
1
=
4
(
t
in ns), where
d
is the
distance between hit OM and trackelement
and
t
res
is the
time residual
, which is defined in
Eq. (5). After selecting these associated hits, track
elements of poor quality are rejected by requiring:
N
AH
X
10 and
s
L
?
ffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffi
ðð
1
=
N
AH
Þ
X
i
ð
L
i
?
/
L
S
Þ
2
Þ
q
X
20 m
:
ARTICLE IN PRESS
J. Ahrens et al. / Nuclear Instruments and Methods in Physics Research A 524 (2004) 169–194
179
Here, the ‘‘lever arm’’
L
i
is the distance between
the vertex of the trackelement and the point on
the trackelement which is closest to OM
i
and
/
L
S
is the average of all
L
i
-values. Track
elements that fulfill these criteria qualify as
track
candidates
(TC).
Frequently, more than one trackcandidate is
found. In this case, a cluster search is performed for
all trackcandidates that fulfill the quality criterion
Q
TC
X
0
:
7
Q
max
where
Q
max
¼
max
ð
Q
TC
Þ
and
Q
TC
¼
min
ð
N
AH
;
0
:
3m
?
1
?
s
L
þ
7
Þ
:
ð
21
Þ
In the cluster search, the ‘‘neighbors’’ of each track
candidate are counted, where neighbors are track
candidates with space angle differences of less than
15
?
:
The cluster with the largest number of track
candidates is selected.
In the final step, the average direction of all
trackcandidates inside the cluster defines the
initial trackdirection. The trackvertex and time
are taken from the central track candidate in the
cluster. Well separated clusters can be used to
identify independent muon tracks in events which
contain multiple muons (see Section 6.1).
4.2. Linefit
The
linefit
[38] algorithm produces an initial
trackon the basis of the hit times with an optional
amplitude weight. It ignores the geometry of the
Cherenkov cone and the optical properties of the
medium and assumes light traveling with a velocity
v
along a 1-dimensional path through the detector.
The locations of each PMT,
r
i
;
which are hit at a
time
t
i
can be connected by a line
r
i
E
r
þ
v
?
t
i
:
ð
22
Þ
A
w
2
to be minimized is defined as
w
2
?
X
N
hit
i
¼
1
ð
r
i
?
r
?
v
?
t
i
Þ
2
ð
23
Þ
where
N
hit
is the number of hits. The
w
2
is
minimized by differentiation with respect to the
free fit parameters
r
and
v
:
This can be solved
analytically
r
¼
/
r
i
S
?
v
?
/
t
i
S
and
v
¼
/
r
i
?
t
i
S
?
/
r
i
S
?
/
t
i
S
/
t
2
i
S
?
/
t
i
S
2
ð
24
Þ
where
/
x
i
S
?ð
1
=
N
hit
Þ
P
N
hit
i
x
i
denotes the mean
of parameter
x
with respect to all hits.
The line-fit thus yields a vertex point
r
;
and a
direction
e
¼
v
LF
=
j
v
LF
j
:
The zenith angle is given
by
y
LF
??
arccos
ð
v
z
=
j
v
LF
jÞ
:
The time residuals (Eq. (5)) for this initial track
generally do not follow the distribution expected
for a Cherenkov model. If the
t
0
parameter of the
initial trackis shifted to better agree with a
Cherenkov model, subsequent reconstructions
converge better (see Section 5.2.3).
The absolute speed
v
LF
?j
v
j
;
of the line-fit is the
mean speed of the light propagating through the
one-dimensional detector projection. Spherical
events (cascades) and high energy muons have
low
v
LF
values, and thin, long events (minimally
ionizing muon tracks) have large values.
4.3. Dipole algorithm
The
dipole algorithm
considers the
unit
vector
from one hit OM to the subsequently hit OM as an
individual dipole moment. Averaging over all
individual dipole moments yields the global mo-
ment
M
:
It is calculated in two steps. First, all hits
are sorted according to their hit times. Then a
dipolemoment
M
is calculated
M
?
1
N
ch
?
1
X
N
ch
i
¼
2
r
i
?
r
i
?
1
j
r
i
?
r
i
?
1
j
:
ð
25
Þ
It can be expressed via an absolute value
M
DA
?
j
M
j
and two angles
y
DA
and
f
DA
:
These angles
define the initial track.
The dipole algorithm does not generate as good
an initial trackas the direct walkor the line-fit, but
it is less vulnerable to a specific class of back-
ground events: almost coincident atmospheric
muons from independent air showers in which
the first muon hits the bottom and the second
muon hits the top of the detector.
ARTICLE IN PRESS
J. Ahrens et al. / Nuclear Instruments and Methods in Physics Research A 524 (2004) 169–194
180
4.4. Inertia tensor algorithm
The
inertia tensor algorithm
is based on a
mechanical picture. The pulse amplitude from a
PMT at
r
i
corresponds to a virtual mass
a
i
at
r
i
:
One can then define the tensor of inertia
I
of that
virtual mass distribution. The origin is the center
of gravity
ð
COG
Þ
of the mass distribution. The
COG
-coordinates and the tensor of inertia com-
ponents are given by
COG
?
X
N
ch
i
¼
1
ð
a
i
Þ
w
?
r
i
and
I
k
;
l
?
X
N
ch
i
¼
1
ð
a
i
Þ
w
?½
d
kl
?ð
r
i
Þ
2
?
r
k
i
?
r
l
i
?
:
ð
26
Þ
The amplitude weight
w
X
0 can be chosen
arbitrarily. The most common settings are
w
¼
0
(ignoring the amplitudes) and
w
¼
1 (setting the
virtual masses equal to the amplitudes). The tensor
of inertia has three eigenvalues
I
j
;
j
e
f
1
;
2
;
3
g
;
corresponding to its three main axes
e
j
:
The
smallest eigenvalue
I
1
corresponds to the longest
axis
e
1
:
In the case of a long track-like event
I
1
5
f
I
2
;
I
3
g
and
e
1
approximates the direction of
the track. The ambiguity in the direction along the
e
1
axis is resolved by choosing the direction where
the average OM hit time is latest. In the case of a
cascade-like event,
I
1
E
I
2
E
I
3
:
The ratios between
the
I
j
can be used to determine the sphericity of the
event.
5. Aspects of the technical implementation
5.1. Reconstruction framework
The basic reconstruction procedure, sketched in
Fig. 6, is sequential. A fast reconstruction program
calculates the initial trackhypothesis for the
likelihood reconstruction. All reconstruction pro-
grams may use a reduced set of hits in order to
suppress noise hits and other detector artifacts.
Event selection criteria can be applied after each
step to reduce the event sample, and allow more
time consuming calculations at later reconstruc-
tion stages. This procedure may iterate with more
sophisticated but slower algorithms analyzing
previous results. The final step is usually the
production of
Data Summary Tape
(DST) like
information, usually in form of PAW
N
-tuples
[39]. A detailed description of this procedure can
be found inRef. [40].
The reconstruction frameworkis implemented
with the
recoos
program[41], which is based on the
rdmc
library [42] and the SiEGMuND software
package [43]. The
recoos
program is highly
modular, which allows flexibility in the choice
and combination of algorithms.
5.2. Likelihood maximization
The aim of the reconstruction is to find the
trackhypothesis which corresponds to the max-
imum likelihood. This is done by minimizing
?
log
ð
L
Þ
with respect to the trackparameters.
We have implemented several minimization
procedures.
The likelihood space for
AMANDA
events is often
characterized by several minima. Local likelihood
minima can arise due to symmetries in the
detector, especially in the azimuth angle, or due
to unexpected hit times caused by scattering. In the
example, shown in Fig. 7, the reconstruction
converged on a local minimum, because of non-
optimal starting values. Several techniques, which
are used to find the global minimum, are here
presented. In particular, the iterative reconstruc-
tion, Section 5.2.2, solves the problem and
converges to the global minimum. One generally
assumes that the global minimum corresponds to
the true solution, but this is not always correct due
to stochastic nature of light emission and detec-
tion. Such events cannot be reconstructed properly
and have to be rejected using quality parameters
(see Section 6.2).
ARTICLE IN PRESS
Hitcleaning Hitcleaning Selections
↓↓
↓
↓
↓
Data
⇒
first guess
⇒
Likelihood
⇒
Analysis
Selections Selections
Fig. 6. Schematic principle of the reconstruction chain.
J. Ahrens et al. / Nuclear Instruments and Methods in Physics Research A 524 (2004) 169–194
181
5.2.1. Minimization algorithms
The reconstruction frameworkallows us to use
and compare these numerical minimization algo-
rithms:
Simplex
[44],
Powell’s
[44],
Minuit
[45]
(using the
minimize
method), and
Simulated
annealing
[44]. The Simplex algorithm is the fastest
algorithm. Powell’s method and Minuit are
B
5
times slower than the Simplex algorithm. The
reconstruction results from Minuit and the Sim-
plex algorithm are nearly identical and almost as
good as the Powell results. Exceptions occur in less
than 1% of the cases, when these methods fail and
stop at the extreme zenith angles
y
¼
0
?
and 80
?
:
The Simulated annealing algorithm is less sensitive
to local minima than the other algorithms, but it is
much slower and requires fine-tuning.
5.2.2. Iterative reconstruction
The
iterative reconstruction
algorithm success-
fully copes with the problem of local minima and
extreme zenith angles by performing multiple
reconstructions of the same event. Each recon-
struction starts with a different initial track.
Therefore, the fast Simplex algorithm is sufficient.
The ability to find the global minimum depends
strongly on the quality of the initial track. A
systematic scan of the full parameter space for
initial seeds is not feasible. Instead the iterative
algorithm concentrates on the direction angles,
zenith and azimuth, and uses reasonable values for
the spatial coordinates. The following procedure
yields good results.
The result of a first minimization is saved as a
reference. Then both direction angles are ran-
domly selected. The trackpoint,
r
0
;
is transformed
to the point on the new track, which is closest to
the center of gravity of hits. The time,
t
0
;
of this
point is shifted to match the Cherenkov expecta-
tion (see Section 5.2.3). Then a new minimization
is started. If the minimum is less than the reference
minimum, it is saved as the new reference. This
procedure is iterated
n
times, and the best minima
found for zenith angles
above
and
below
the
horizon, are saved, and used to generate an
important selection parameter (see Section 6.2).
This algorithm substantially reduces the number
of false minima found, after a few iterations. For
n
¼
6 roughly 95% of the results are in the vicinity
of the asymptotic optimum for
n
N
:
For
n
C
20
more than 99% of the results are the global
minimum. Despite the fast convergence, the
iterative reconstruction
requires significant CPU
time, which limits its use to reduced data sets.
5.2.3. Lateral shift and time residual
The efficiency of finding the global minimum of
the likelihood function can be improved by
translating the arbitrary vertex and/or time origin
of the output trackfrom the first guess algorithm
before application of the full maximum likelihood
method.
Transformation of
r
0
:
In general this ‘‘vertex’’
point is arbitrary in the infinite trackapproxima-
tion used, and first guess methods may produce
positions distant from the detector. During the
likelihood minimization, numerical errors can be
avoided and the convergence improved by shifting
this point along the direction of the tracktowards
the point closest to the
center of gravity of hits
(see
Eq. (26)). The vertex time
t
0
is transformed
accordingly:
D
ð
t
0
Þ¼
D
ð
r
0
Þ
=
c
:
Transformation of t
0
:
The time
t
0
obtained from
first guess algorithms is not calculated from a full
Cherenkov model. The efficiency of the likelihood
reconstruction can be improved by shifting the
t
0
such that the time residuals, Eq. (5), fit better to a
ARTICLE IN PRESS
180
160
140
120
100
80
60
40
20
0
170
175
180
185
190
Parabola fit
experimental data
−
log (likelihood)
theta [
°
]
Fig. 7. An example of the likelihood space (one-dimensional
projection) for a specific
AMANDA
event. Shown is
?
log
ð
L
Þ
as
function of the zenith angle. Each point represents a fit, for
which the zenith angle was fixed and the other trackparameters
were allowed to vary in order to find the best minimum. A local
minimum which was found by a gradient likelihood minimiza-
tion is indicated by a fitted parabola. Improved methods that
avoid this are described in the text.
J. Ahrens et al. / Nuclear Instruments and Methods in Physics Research A 524 (2004) 169–194
182
Cherenkov model. In particular it is useful to
avoid negative
t
res
;
which would correspond to
causality violations. This can be achieved by
transforming
t
0
t
0
?
t
?
res
;
where
t
?
res
is the most
negative time residual.
5.2.4. Coordinates and restricted parameters
The trackcoordinates
a
;
which are used by the
likelihood, are independent of the coordinates
actually chosen for the minimization. Therefore,
the coordinate system can be chosen arbitrarily.
Any of the parameters in this coordinate system
can be kept fixed. During the minimization
parameterization
functions translate the coordi-
nates as necessary. The most commonly used
coordinates are
r
0
and the zenith and azimuth
angles
y
;
f
:
The freedom in the choice of coordinates can be
used to improve the numerical minimization, for
systematic studies, or to fix certain parameters
according to external knowledge. An example is
the reconstruction of coincident events with the
SPASE
surface arrays [8]. Here, we fix the location
of the trajectory to coincide with the core location
at the surface as measured by
SPASE
. Then, the
direction is determined with the
AMANDA
recon-
struction subject to this constraint.
Under certain circumstances the allowed range
of the reconstruction parameters is restricted. The
most important example here is to restrict the
reconstructed zenith angle to above or below the
horizon, to find the most likely up- or down-going
tracks, respectively. Comparing the quality of the
two solutions can be used for background rejec-
tion. Technically the constrained fit is accom-
plished by multiplying the likelihood by a prior,
which is zero outside the allowed parameter range.
5.3. Preprocessing and hit cleaning
The data must be filtered and calibrated before
reconstruction. Defective OMs are removed, and
the amplitudes and hit times are calibrated. A
hit
cleaning
procedure identifies and flags hits which
appear to be noise or electronic effects, such as
cross talkor after-pulsing. These hits are not used
in the reconstruction, but they are retained for
post-reconstruction analysis.
The hit cleaning procedure can be based on
simple and robust algorithms, because the PMTs
have low noise rates. Noise and after-pulse hits are
strongly suppressed by rejecting hits that are
isolated in time and space from other signals in
the detector. Typically a hit is considered to be
noise if there is no hit within a distance of 60–
100 m and a time of
7
300 to
7
600 ns
:
Cross talk
hits are identified by examining the amplitudes and
pulse widths of the individual pulses and by
analyzing the correlations of uncalibrated hit times
with hits of large amplitude in channel combina-
tions which are known to cross talk to each other.
The required cross talkcorrelation map was
determined independently in a dedicated calibra-
tion campaign.
5.4. Processing speeds
The first guess algorithms are sufficiently fast
that the execution time is dominated by file input/
output and the software framework. Typical fit
times are
E
20 ms per event on a 850 MHz
Pentium-III Linux PC. The processing speed of
the likelihood reconstructions can vary signifi-
cantly depending on the number of free para-
meters, the number of iterations, the minimization
algorithm, and the experimental parameters like
the number of hit OMs. These effects dominate the
differences in processing speeds due to different
reconstruction algorithms. The typical execution
time for a 16-fold iterative likelihood reconstruc-
tions using the simplex minimizer to reconstruct
the five free trackparameters is
C
250 ms per
event.
6. Background rejection
The performance of the reconstruction depends
strongly on the quality and background selection
criteria. The major classes of background events in
AMANDA
(see Section 6.1) are suppressed by the
quality parameters presented in Section 6.2.
Optimization strategies for the selection criteria
are summarized in Section 6.3. Finally, we
evaluate the reconstruction performance in
Section 7.
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J. Ahrens et al. / Nuclear Instruments and Methods in Physics Research A 524 (2004) 169–194
183
6.1. Background classes
Most background events from atmospheric
muons are well reconstructed and can be
rejected by selecting up-going reconstructed
events. However, there is a small fraction of mis-
reconstructed events, amounting to about 10
?
2
for
the unbiased and about 10
?
4
for the zenith-
weighted reconstruction. These events are rejected
by additional selection criteria described in Section
6.2. These background events are classified as
follows.
Nearly horizontal muons
: These events have true
incident angles close to the horizon. A small error
in the reconstruction causes them to appear as up-
going. These events are not severely mis-recon-
structed, but occur due to the finite angular
resolution.
Muon bundles
: The spatial separation between
multiple muons from a single air shower, a
muon
bundle
, is usually small enough that the event can
be described by a single bright muon track. If the
separation is too large, the reconstruction fails.
Cascades
: Bright stochastic energy losses (e.g.
bremsstrahlung) produce additional light, which
distorts the Cherenkov cone from the muon.
Cascades emit most of their light with the same
Cherenkov angle as the muon, but some light is
emitted at other angles. These secondary events
can cause the reconstruction to fail, especially
when the cascade(s) produce more light than the
muon itself. A special class of these events are
muons which pass outside the detector and release
a bright cascade, which can mimic an up-going hit
pattern.
Stopping muons
: Over the depth of the detector
the muon flux changes by a factor of
B
2
;
since
muons lose their energy and stop. These muons
can create an up-going hit pattern, especially when
the muon stops just before entering the detector
from the side.
Scattering layers
: The scattering of light in the
polar ice cap varies with depth. Light from bright
events, can mimic an up-going hit pattern, in
particular when it traverses layers of higher
scattering.
Corner clippers
: These are events where the
muon passes diagonally below the detector. The
light travel upwards through the detector mimick-
ing an up-going muon.
Uncorrelated coincident muons
: Due to the large
size of the
AMANDA
detector, the probability of
muons from two independent air showers forming
a single event is small on the trigger level but not
negligible. If an initial muon traverses the bottom
of the detector and a later muon traverses the top,
the combination can be reconstructed as an up-
going muon.
Electronic artifacts
: Noise, cross talkand other
transient electronic malfunctions are generally
small effects, but they can occasionally produce
hits, which distort the time pattern. Such effects
become important after a selection process of
several orders of magnitude.
6.2. Quality parameters
Background events, which pass a zenith angle
selection, need to be rejected by applying selection
criteria on quality parameters. These parameters
usually evaluate information, which is not opti-
mally exploited in the reconstruction. The detailed
choice of quality parameters is specific to each
analysis. Here, we summarize the most important
categories.
The
number of direct hits
,
N
dir
ð
t
1
:
t
2
Þ
;
is the
number of hits with small time residuals:
t
1
o
t
res
o
t
2
(see Eq. (5)). Un-scattered photons
provide the best information for the reconstruc-
tion, and a large number of
N
dir
indicates high
quality information in the event. Empirically
reasonable values are
t
1
C
?
15 ns and
t
2
between
¼þ
25 and
þ
150 ns
;
depending on the specific
analysis.
The
length of the event L
is obtained by
projecting each hit OM onto the reconstructed
trackand taking the distance between the two
outermost of these points.
L
can be considered as
the ‘‘lever arm’’ of the reconstruction. Larger
values corresponding to a more robust and precise
reconstruction of the track’s direction. This para-
meter is particularly powerful when calculated for
direct hits only, and is then referred to as
L
dir
ð
t
1
:
t
2
Þ
:
Length requirements are efficient
against corner clippers, stopping muons and
cascades.
ARTICLE IN PRESS
J. Ahrens et al. / Nuclear Instruments and Methods in Physics Research A 524 (2004) 169–194
184
The absolute value of the likelihood at the
maximum is a good parameter to evaluate the
quality of a reconstruction. Here, a useful ob-
servable is the
likelihood parameter
L
which is
defined as
L
??
log
ð
L
Þ
N
free
ð
27
Þ
where
N
free
is the degrees of freedom (e.g.
N
free
¼
N
hits
?
5 for a trackreconstruction). For Gaussian
probability distributions this expression corre-
sponds to the reduced chi-square.
L
can be used
as a selection parameter, smaller values corre-
sponding to higher quality. A selection of events
with good
L
P
hit
P
no
?
hit
values is efficient against
stopping muons.
Comparing
L
from different reconstructions is a
powerful technique. Cascade-like events will have
a better likelihood from a cascade reconstruction
than one from a trackreconstruction.
Another efficient rejection method is to compare
L
for the best up-going versus the best down-going
reconstruction of a single event. If the up-going
reconstruction is not significantly better than the
down-going reconstruction, the event is rejected.
These values can be obtained from the iterative
reconstruction method (Section 5.2.2) or by
restricting the parameter space. This method is
particularly powerful when the down-going recon-
struction uses a zenith weighted likelihood (Sec-
tion 3.1.4).
The reconstruction methods consider the
p.d.f. for each hit separately but ignore correla-
tions. Therefore, the reconstructions assign the
same likelihood to tracks where all hits cluster at
one end of the reconstructed trackand tracks
where the same number of hits are smoothly
distributed along the track. The latter hit
pattern indicates a successful trackreconstruction,
while the former hit pattern may be caused
by a background event. The
smoothness
parameter
S
was inspired by the Kolmogorov–Smirnov
test of the consistency of two distributions.
S
is a measure of the consistency of the observed
hit pattern with the hypothesis of constant light
emission by a muon. The simplest definition
of the smoothness
S
is
S
¼
S
max
j
;
where
S
max
j
is
that
S
j
;
which has the largest absolute value, and
S
j
is defined as
S
j
?
j
?
1
N
?
1
?
l
j
l
N
:
ð
28
Þ
l
j
is the distance along the trackbetween the points
of closest approach of the trackto the first and the
j
th hit module, with the hits taken in order of their
projected position on the track.
N
is the total
number of hits. Tracks with hits clustered at the
beginning or end of the trackhave
S
approaching
þ
1or
?
1
;
respectively. High-quality tracks with
S
close to zero, have hits equally spaced along the
track. A graphical representation of the smooth-
ness construction can be found inRef. [30].
Extensions of this smoothness parameter in-
clude the restriction of the calculation to direct hits
only or using the distribution of hit times
t
i
instead
of the distances
l
i
:
A particularly important extension is
S
P
hit
:
In
order to account for the granularity and asym-
metric geometry of the detector one can replace
the above formulation with one that models the hit
smoothness expectation for the actual geometry of
the assumed muon track. This can be accom-
plished by using the hit probabilities of all
N
OM
;
the number of operational OMs, (ordered along
the track) as weights:
S
P
hit
¼
max
ð
S
P
hit
j
Þ
with
S
P
hit
j
?
P
j
i
¼
1
L
i
P
N
OM
i
¼
1
L
i
?
P
j
i
¼
1
P
hit
;
i
P
N
OM
i
¼
1
P
hit
;
i
ð
29
Þ
L
i
¼
1
;
if the OM
i
was hit and 0 otherwise and
P
hit
;
i
is the probability for OM
i
to be hit given the
reconstructed track. The hit probabilities are
calculated according to the algorithm in Section
3.2.3. Smoothness selections are very efficient
against secondary cascades, stopping muons and
coincident muons from independent air showers.
Interesting
AMANDA
events are analyzed with
multiple reconstruction algorithms. An event is
most likely to have been reconstructed correctly, if
the different algorithms produce consistent results.
For two reconstructions with directions
e
1
and
e
2
;
the space angle between them is given by
C
¼
arccos
ð
e
1
?
e
2
Þ
;
which should be reasonably small
for successful reconstructions. This concept can be
extended to multiple reconstructions and their
angular deviations from the average direction. For
n
different reconstructed directions,
e
i
;
the average
ARTICLE IN PRESS
J. Ahrens et al. / Nuclear Instruments and Methods in Physics Research A 524 (2004) 169–194
185
reconstructed direction,
E
;
is given by
E
¼
P
n
i
e
i
=
j
P
n
i
e
i
j
:
We can define the parameter
C
w
¼
X
i
½
arccos
ð
e
i
?
E
Þ?
w
!
1
=
w
:
ð
30
Þ
C
1
describes the average space angle between the
individual reconstructions and
E
:
C
2
is a different
parameter, which treats the deviations between
E
and the
e
i
as ‘‘errors’’ and adds them quadrati-
cally. Small values of
C
1
or
C
2
indicate consistent
reconstruction results.
The
C
parameters are a mathematically correct
consistency checkonly when comparing the results
of uncorrelated reconstructions of the same
intrinsic resolutions. This is not the case when
comparing different
AMANDA
reconstructions. Irre-
spective of the validity of such an interpretation,
C
1
or
C
2
are very efficient selection criteria,
especially against almost horizontal muons and
wide muon bundles.
A few additional selection parameters are
closely related to first guess methods. The ratio
of the eigenvalues of the
tensor of inertia
(see
Section 4.4) are a measure of the sphericity of the
event topology, which is an efficient selection
parameter against cascade backgrounds. Tracks
reconstructed as down-going by the
dipole fit
(see
Section 4.3) that have a non-negligible
dipole
moment
,
M
DA
?j
~
MM
j
;
indicate coincident muons
from independent air showers. Larger values of the
line-fit speed
v
LF
(see Section 4.2) are an indication
for longer muon-like, smaller values for more
spherical cascade-like events.
Finally, two approaches evaluate the ‘‘intrinsic
resolution’’ or ‘‘stability’’ of the reconstruction of
each event. One approach quantifies the sharpness
of the minimum found by the minimizers in
?
log
ð
L
Þ
by fitting a paraboloid to it. The fitted
parameters can then be used to classify the
sharpness of the minimum. The other approach
splits an event into sub-events (for example,
containing odd- vs. even-numbered hits) and
reconstructs the sub-events. If the reconstructed
directions of the sub-events are different, then the
reconstruction of the full event has a larger
uncertainty.
6.3. Analysis strategies
Analyses that search for neutrino induced
muons must cope with a large background of
atmospheric muons. The optimal choice of recon-
struction and selection criteria varies strongly with
different expectations for the energy and angular
distribution of the signal events. The goal is to
optimize the signal efficiency over the background
or noise (square root of the background) based on
sets of signal and background data.
?
The selection criteria for background sensitive
variables may be adjusted individually such
that a specified fraction of signal events pass.
After these
first level criteria
are set, the
adjustment is repeated until the desired back-
ground rejection is reached. Each iteration
defines a ‘‘cut-level’’, which corresponds to
data sets of increasing purity. This simple
method is used to derive a defined set of
selection parameters for the performance Sec-
tion 7. However, less efficient criteria are mixed
with more efficient criteria, and correlations of
the variables are not taken into account.
Therefore, this method does not achieve the
optimum signal efficiency.
?
An improvement to this method has been
demonstrated in an
AMANDA
point source
analysis
[46,47]. Here, a selection criterion is
only applied to the most sensitive variable, and
the most sensitive variable is determined at each
cut level. An interesting aspect of this point
source search is that the experimental data
themselves can be used as a background
sample, which reduces systematic uncertainties
from the background simulation. The selection
criteria are not optimized with respect to signal
purity but with respect to an optimal signifi-
cance of a possible signal.
?
Another approach is to combine the selection
parameters into a single selection parameter,
called
event quality
. This can be done by
rescaling and normalizing each of the selection
parameters according to the cumulative dis-
tribution of the signal expectation. The
AMANDA
analyses of atmospheric neutrinos [30,48] used
this technique.
ARTICLE IN PRESS
J. Ahrens et al. / Nuclear Instruments and Methods in Physics Research A 524 (2004) 169–194
186
?
Additional approaches use discriminant analy-
sis [49] or neural nets [6,50,51] to optimize the
efficiency while taking into account the correla-
tions between selection criteria and their
individual selectivity. However, both methods
depend critically on a good agreement between
experiment and simulation. These methods
quantify the efficiency of each parameter by
including and excluding it from the optimiza-
tion procedure.
?
The ‘‘C
ut
E
val
’’ method finds the optimum
combination of selection parameters and cut
values by numerically maximizing a significance
function,
Q
:
An example is
Q
¼
S
=
ffiffiffiffi
B
p
;
where
S
is the number of signal events, and
B
is the
number of background events after selection.
The implementation proceeds in several
steps. First, the most efficient selection para-
meter,
C
1
;
is the parameter that individually
maximizes
Q
:
The next parameter,
C
2
;
is the
parameter that maximizes
Q
in conjunction
with
C
1
:
More parameters are successively
determined until the addition of a new para-
meter fails to improve
Q
:
This procedure takes
correlations between the selection criteria into
account. The final number of selection para-
meters is reduced to a minimum, while max-
imizing the efficiency. Next, the optimal
selection for this combination parameters is
computed as a function of a boundary condi-
tion (e.g. the maximum number of accepted
background events). This boundary condition
is also used to define a single quality parameter.
Such a formalized procedure has to be
carefully monitored, e.g. to handle potentially
un-simulated experimental effects. The C
ut
E-
val
procedure is monitored by defining differ-
ent, complementary optimization functions
Q
;
which allow real and simulated data to be
compared
[30,52–54]
7. Performance
This section describes the performance of the
reconstruction methods. It is based on illustrative
data selections, and the actual performance of a
dedicated analysis can be different. Unless noted
otherwise, the data shown is from Monte
Carlo simulations of atmospheric neutrinos for
AMANDA-II
.
7.1. First guess algorithms
Since the first guess algorithms are used as a
starting point for the full reconstruction, they
should provide a reasonable estimate of the track
coordinates. Also, these algorithms are used as the
basis of early level filtering, and therefore need to
be sufficiently accurate for that purpose, i.e. they
should at least reconstruct the events in the correct
hemisphere.
As an example,
Table 1
gives the passing
efficiencies with respect to the
AMANDA-II
trigger
for atmospheric neutrinos (signal) and atmo-
spheric muons (background) for the first guess
methods (see Section 4), after the selection of
events with calculated zenith angles larger 80
?
:
The
direct walk
algorithm gives the best background
suppression and the highest atmospheric neutrino
passing rate. Correspondingly, it also gives the
best initial tracks to the likelihood reconstructions.
7.2. Pointing accuracy of the track reconstruction
The angular accuracy of the reconstruction can
be expressed in terms of a point spread function,
which is given by the space angle deviation
C
between the true and the reconstructed direction of
a muon corrected for solid angle. The space angle
deviation is a combined result of two effects: a
systematic shift in the direction and a random
spread around this shift. In a point source analysis,
for example, it is possible to correct for systematic
ARTICLE IN PRESS
Table 1
The atmospheric muon and atmospheric neutrino detection
efficiencies for a selection at
y
X
80
?
for the first guess
algorithms
Reconstruction atm.
m
(%) atm.
n
(%)
Direct walk1.5% 93%
Line-fit 4.8% 85%
Dipole algorithm 16.8% 78%
J. Ahrens et al. / Nuclear Instruments and Methods in Physics Research A 524 (2004) 169–194
187
shifts and be limited by the point spread function
alone [47].
The zenith and space angular deviations are
shown in Figs. 8 and 9. They are obtained by the
reconstruction algorithms as used in
AMANDA-B10
.
The same event selection is used for all. As a
general observation, the distributions of deviations
for different reconstruction algorithms is surpris-
ingly similar after a particular selection. Larger
differences are usually seen in the selection
efficiencies. A similar behavior is observed for
AMANDA-II
.
The dependence of the space angle deviation for
the full
AMANDA-II
detector on the cut level
5
for
the LH reconstruction is shown in
Fig. 10. The
tighter the selection criteria, the better the angular
resolution. The same general trend is true for the
other reconstructions. Tight criteria select events
with unambiguous hit topologies, which are
reconstructed better. The results for cut level 6
are shown in Figs. 11–13 as function of the energy
and the zenith angle.
The angular resolution (see Fig. 11) has a weak
energy dependence. The energy of the muon is
taken at the point of its closest approach to the
detector center. Best results are achieved for
energies of 100 GeV–10 TeV
:
At energies
o
100 GeV
;
the muons have paths shorter than
the full detector, which limits the angular
resolution. At energies
>
10 TeV
;
more light is
emitted due to individual stochastic energy loss
processes along the muon track. Here, the hit
pattern is not correctly described by the underlying
reconstruction assumption of a bare muon track
(see Section 6.1).
The space angular resolution depends on the
incident muon zenith angle (see
Fig. 12). Again
ARTICLE IN PRESS
Fig. 8. The zenith angle deviations for various reconstructions
of
AMANDA-B10
. The result of an atmospheric neutrino
simulation after the selection criteria of (Ahrens et al.)
[30]
is
shown. The fits are a
linefit
(LF), an iterated
upandel
fit (LH),
an iterated zenith-weighted
upandel
fit and a MPE fit.
Fig. 9. The distribution of space angle deviations for various
reconstructions of
AMANDA-B10
. The result of an atmospheric
neutrino simulation after the selection criteria of (Ahrens et al.)
[30]
is shown. The fits are a
linefit
(LF), an iterated
upandel
fit
(LH), an iterated zenith-weighted
upandel
fit and a MPE fit.
5
The cut levels defined here are typical and intended as
demonstrating example. We use typical selection parameters
from Section 6.2: the reconstructed zenith angle,
y
DW
>
80
?
;
y
LH
>
80
?
;
N
ch
;
N
LH
dir
ð?
15
:
25
Þ
;
L
LH
dir
ð?
15
:
75
Þ
;
L
LH
;
S
LH
and
C
1
ð
DW
;
LH
;
MPE
Þ
:
Our goal here is to illustrate the analysis,
and we do not optimize with respect to efficiency and angular
resolution. Instead each individual criterion is enforced in such
a way that 95% of the events from the previous level would
pass, and correlations between the parameters are ignored.
Specific physics analyses will use selection criteria of higher
efficiency and will achieve better angular resolutions than the
C
2
?
;
shown here.
J. Ahrens et al. / Nuclear Instruments and Methods in Physics Research A 524 (2004) 169–194
188
this is shown only for the LH reconstruction, the
other reconstructions are similar. Up-going muons
with cos
y
m
C
?
0
:
7 are best reconstructed, and
horizontal muons are the worst, because of the
geometry of the
AMANDA-II
detector. Nearly
vertical events with cos
y
m
C
?
1 have a poorer
angular resolution, because they illuminate
fewer strings, which can cause ambiguities in the
azimuth.
Systematic shifts also degrade the angular resolu-
tion.
AMANDA
observes a small zenith-dependent shift
ARTICLE IN PRESS
log
10
(E
µ
/GeV)
space angle deviation
[°]
Mean
Median
1.5
2
2.5
3
3.5
4
4.5
5
0
2
4
6
Fig. 11. The dependence of the space angle deviation of the LH
fit on the muon energy for
AMANDA-II
. Shown are mean (stars)
and median (circles) for simulated atmospheric neutrinos.
Cut level
space angle deviation
[°]
Mean
Median
2
3
4
5
6
7
8
9
10
0246
Fig. 10. The dependence of the space angle deviation of the LH
reconstruction in
AMANDA-II
on the event selection (cut levels).
cos (
Θ
µ
)
space angle deviation
[°]
Mean
Median
1
1.5
2
2.5
3
3.5
4
4.5
5
1 0.75 0.5 0.25 0
Fig. 12. The space angle deviations of the LH fit as a function
of the cosine of the incident zenith angle (for
AMANDA-II
).
Shown are the mean (stars) and median (circles) for simulated
atmospheric neutrinos.
cos (
Θ
µ
)
Mean
Median
2
1.5
1
0.5
0
0.5
1
1.5
2
1 0.5 0
Θ
µ
Θ
LH
Fig. 13. The zenith angle shift of the reconstruction versus the
cosine of the incident angle. Shown are mean (stars) and
median (circles) for simulated atmospheric neutrinos.
J. Ahrens et al. / Nuclear Instruments and Methods in Physics Research A 524 (2004) 169–194
189
of the reconstructed zenith angle and no systema-
tic shift in azimuth. This is shown in Fig. 13 for
simulated atmospheric neutrinos in
AMANDA-II
.
The size of this shift depends on the zenith angle
itself, and it is determined by the geometry of
AMANDA
, which has a larger size in vertical than in
horizontal directions. From a comparison with
AMANDA-B10
data
[46,55], we observe that these
shifts become smaller with a larger horizontal
detector size. These shifts are confirmed by
analyzing
AMANDA
events coincident with
SPASE
(see
below).
These angular deviations have been obtained
from Monte Carlo simulations. They can be
experimentally verified by analyzing coincident
events between
AMANDA
and
SPASE
. An analysis of
data from the 10 string
AMANDA-B10
detector,
shown in
Fig. 14, confirms the estimate of
C
3
?
obtained from Monte Carlo studies for
AMANDA-
B10
. Unfolding the estimated
SPASE
resolution of
C
1
?
confirms the estimated
AMANDA-B10
resolu-
tion of
C
3
?
near the
SPASE-AMANDA
coincidence
direction [8–10].
A simulation-independent estimate can be ob-
tained by splitting the hits of individual events in
two parts and reconstructing each sub-event
separately. The difference in the two results gives
an estimate of the total angular resolution. Such
analyses are being performed at present and results
will be published separately.
7.3. Energy reconstruction
The energy resolution of the three methods,
described in Section 3.2.4, is shown in Fig. 15 as
function of the muon energy at its closest point
to the
AMANDA-B10
center. The resolution for
AMANDA-B10
in
D
log
10
E
is
C
0
:
4
;
for the interest-
ing energy range of a few TeV to 1 PeV
:
Below
C
600 GeV the energy resolution is limited,
because the amount of light emitted by a muon
is only weakly dependent on its energy. Above
1 TeV the resolution improves because radiative
energy losses become dominant. Above 100 TeV
the resolution degrades, because energy loss
fluctuations dominate.
Although these methods are quite different,
their performances are similar. The full
E
reco
and
P
hit
methods achieve similar resolutions up to
1 PeV
:
The
P
hit
method becomes worse above this
energy, because in
AMANDA-B10
almost all of the
OMs are hit, and the method saturates. In
contrast, the Neural Net method shows a slightly
poorer resolution up to 1 PeV but is better above.
Its resolution is relatively constant over several
decades of energy. This is an advantage when
reconstructing an original energy spectrum with an
unfolding procedure as in Ref. [36].
The
AMANDA-II
detector contains more than
twice as many OMs as
AMANDA-B10
, and the
ARTICLE IN PRESS
0
Space angle (degrees)
arbitrary units
20
40
60
80
100
120
140
5
0 101520253
0
Fig. 14. Distribution of the space angle deviations between air
shower directions assigned by
SPASE-2
and muon directions
assigned by
AMANDA-B10
for coincident events measured in
1997. The figure is not corrected for the systematic shift.
log
10
(E
gen
/GeV)
σ
(log
10
(E
rec
/ E
gen
))
P
hit
method
Full E
reco
method
Neural Net method
0
0.2
0.4
0.6
0.8
1
1.2
1.4
2345678
Fig. 15. Comparison of the resolution of three different energy
reconstruction approaches for
AMANDA-B10
.
E
gen
is the gener-
ated energy (MC) and
E
rec
the reconstructed energy.
J. Ahrens et al. / Nuclear Instruments and Methods in Physics Research A 524 (2004) 169–194
190
energy resolution is better, especially at larger
energies,
s
ð
D
log
10
E
Þ
C
0
:
3
:
The neural net recon-
struction results for
AMANDA-II
are shown in Fig.
16. Finally, the recently installed transient wave-
form recorders (TWR) allow better amplitude
measurements, which should significantly improve
the results of the energy reconstructions, in
particular, the
full E
reco
method [56].
As discussed in Section 1, the cascade channel
can achieve substantially better resolutions, be-
cause the full energy is deposited inside or close of
the detector. Energy resolutions in
D
log
10
E
of
p
0
:
2 and
p
0
:
15 can be achieved by
AMANDA-B10
and
AMANDA-II
. respectively [16].
7.4. Systematic uncertainties
Several parameters of the detector are calibrated
and therefore only known with limited accuracy.
These parameters include the time offsets, the OM
positions and the absolute OM sensitivities. We
have estimated the effects of these uncertainties on
the resolution of
AMANDA
reconstructions
[55].As
an example, Fig. 17 shows the effect of an
additional contribution to the time calibration
uncertainty for the 10 string
AMANDA-B10
detector.
The zenith angular resolutions for simulated
atmospheric neutrino events only degrade when
the additional timing uncertainties exceed 10 ns
:
Additional tests with similar results were done
with non-random systematic shifts such as a
depth-dependent shift or a string-dependent shift.
Therefore, the angular resolution is insensitive to
the uncertainties in the time calibration. The
geometry of the detector is known to better than
30 cm horizontally and to better than 1 m
vertically, which corresponds to timing uncertain-
ties of
t
1or 3
:
5ns
;
respectively. Therefore, the
geometry calibration is also sufficiently accurate.
Similarly, the effect of uncertainties on other
parameters, like the absolute PMT efficiency, has
been investigated. No indication was found that
the remaining calibration uncertainties seriously
affect the angular resolution or the systematic
zenith angle offset. The combined calibration
uncertainties are expected to affect the accuracy
of the reconstruction by less than 5
%
in the zenith
angle resolution and to less than 0
:
5
?
in the
absolute pointing offset.
ARTICLE IN PRESS
arbitrary units
log10 (Energy/GeV)
1 TeV
10 TeV
100 TeV
1 PeV
700
600
500
400
300
200
100
0
12 345 67
Fig. 16. Energy reconstruction for simulated muons of
different fixed energy in
AMANDA-II
, using the neural net
method.
Random timing error
[
ns
]
RMS (
Θ
µ
Θ
LH
)
2
2.5
3
3.5
4
4.5
5
1
10
Fig. 17. The zenith angle deviations (RMS) as function of an
additional uncertainty in the
t
0
time calibration. Data is shown
for simulated atmospheric neutrino events in
AMANDA-B10
with
the selection of (Ahrens et al.)
[30]. The transit time of the
PMTs has been shifted without correcting for in the reconstruc-
tion. The shift is a fixed value for each PMT, obtained from a
random Gaussian distribution.
J. Ahrens et al. / Nuclear Instruments and Methods in Physics Research A 524 (2004) 169–194
191
8. Discussion and Outlook
We have developed methods to reconstruct and
identify muons induced by neutrinos
[30], inspite
of the challenges of the natural environment and
large backgrounds. These methods allow us to
establish
AMANDA
as a working neutrino telescope.
The reconstruction techniques described in this
paper are still subject to improvement in several
aspects.
The likelihood description
: The likelihood func-
tions for trackreconstruction are based on the
assumption of exactly one infinitely long muon
trackper event. Extensions of this model to
encompass
starting muon tracks
(including the
description of the hadronic vertex),
stopping
muons
,
muon bundles
of non-negligible width, and
multiple independent muons
will be important,
particularly in the context of larger detectors such
as Ice Cube. Initial efforts fitting multiple muons
with the direct walkalgorithm have been useful in
rejecting coincident down-going muons, and work
toward reconstructing muon bundles has begun in
the context of events coincident with
SPASE
air
showers.
The p.d.f. calculation
: The likelihood function is
based on parametrizations of probability density
functions (p.d.f.). The p.d.f. is obtained from
Monte Carlo simulations, and its accuracy is
limited by the accuracy of the simulation. Better
simulations lead directly to a better p.d.f. and
hence better reconstructions.
The p.d.f. parametrizations
: The p.d.f. is para-
metrized by functions (e.g. the
Pandel functions
)
which only approximate the full p.d.f. More
accurate parametrization functions will result in
better reconstructions. For example, the scattering
coefficient shows a significant depth dependence
(see Section 2). The current reconstruction is based
on an average p.d.f. assuming depth-independent
ice properties. While the trackreconstruction is
relatively insensitive to the accuracy of the
parametrization, we expect a depth-dependent
p.d.f. to have better energy reconstruction.
Complementary information
: The current recon-
struction algorithms do not include all available
information in an event. In particular, correlations
between detected PMT signals are ignored. For
this reason dedicated selection parameters have
been designed to exploit this information. They are
used to discriminate between well reconstructed
and poorly reconstructed events and improve the
quality of the data sample. Future workwill try to
improve these parameters and expand the present
likelihood description.
Transient waveform recorders
: At the beginning
of the year 2003, the detector readout has been
upgraded with transient waveform recorders [56].
We expect a substantial improvement of the
multiple-photon detection and the dynamic range
in particular for high muon energies.
The construction of a much larger detector, the
IceCube
detector, will start in the year 2004. It will
consist of 4800 PMT deployed on 80 vertical
strings and will surround the
AMANDA
detector [57].
The performance of
IceCube
has been studied
with realistic Monte Carlo simulations and similar
analysis techniques as described in this paper [58].
The result is a substantially improved performance
in terms of sensitivity and reconstruction accuracy.
A direction accuracy of about 0
:
7
?
(median) for
energies above 1 TeV is achieved. Similar to
AMANDA
, we expect a further improvement by
exploiting the full information, avaliable from
the recorded wave-forms, in the reconstruction.
Acknowledgements
This research was supported by the following
agencies: Deutsche Forschungsgemeinschaft
(DFG); German Ministry for Education and
Research; Knut and Alice Wallenberg Founda-
tion, Sweden; Swedish Research Council; Swedish
Natural Science Research Council; Fund for
Scientific Research (FNRS-FWO), Flanders In-
stitute to encourage scientific and technological
research in industry (IWT), and Belgian Federal
Office for Scientific, Technical and Cultural affairs
(OSTC), Belgium. UC-Irvine AENEAS Super-
computer Facility; University of Wisconsin
Alumni Research Foundation; U.S. National
Science Foundation, Office of Polar Programs;
U.S. National Science Foundation, Physics
Division; U.S. Department of Energy; D.F.
Cowen acknowledges the support of the NSF
ARTICLE IN PRESS
J. Ahrens et al. / Nuclear Instruments and Methods in Physics Research A 524 (2004) 169–194
192
CAREER program. I. Taboada acknowledges the
support of FVPI.
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