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Sphericity Lee Pondrom May 9, 2011

Sphericity Lee Pondrom May 9, 2011. References for sphericity and thrust Original application from Spear G. Hanson et al., PRL 35. 1609 (1975). Useful

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Page 1: Sphericity Lee Pondrom May 9, 2011. References for sphericity and thrust Original application from Spear G. Hanson et al., PRL 35. 1609 (1975). Useful

Sphericity

Lee PondromMay 9, 2011

Page 2: Sphericity Lee Pondrom May 9, 2011. References for sphericity and thrust Original application from Spear G. Hanson et al., PRL 35. 1609 (1975). Useful

References for sphericity and thrust

• Original application from Spear

G. Hanson et al., PRL 35. 1609 (1975).Useful lecture slides by Steve Mrennain a description of Pythia:

http://cepa.fnal.gov/psm/simulation/mcgen/lund/pythia_manual/pythia6.3/pythia6301/node213.html

Page 3: Sphericity Lee Pondrom May 9, 2011. References for sphericity and thrust Original application from Spear G. Hanson et al., PRL 35. 1609 (1975). Useful

Definitions

• Sαβ = Σi pαipβ

i/Σipi² . • Where the sum is over all particles in the

event, and α,β refer to the coordinate axes x,y,z. Gail Hanson uses a definition which interchanges the eigenvalues, namely:

• T = (1 – S)Σipi².• This is the form originally proposed by

Bjorken (PRD 1, 1416(1970)). We will use Mrenna’s definition.

Page 4: Sphericity Lee Pondrom May 9, 2011. References for sphericity and thrust Original application from Spear G. Hanson et al., PRL 35. 1609 (1975). Useful

Eigenvalues of S

• Diagonalize S• λ1 • S’ = RSR-1 = λ2 , • λ3 • and order them λ1>λ2>λ3, so λ1

• is the ‘jet axis’ . A two body final state would have λ1 = 1, and λ3 = λ2 = 0, which is as jetty as you can get. A spherical event would have λ1 = λ2 = λ3 = 1/3. The sphericity is defined as Sp = 3(λ2 + λ3 )/2, 0<Sp<1.

Page 5: Sphericity Lee Pondrom May 9, 2011. References for sphericity and thrust Original application from Spear G. Hanson et al., PRL 35. 1609 (1975). Useful

Some formulas

• The matrix S is symmetric, so we have to calculate six components: S11, S12, S13, S22, S23, and S33. The trace is an invariant, S11 + S22 + S33 = 1. The diagonalization procedure gives a cubic equation: λ3 – λ2 + q λ + r = 0, where q and r are functions of the components of S.

Page 6: Sphericity Lee Pondrom May 9, 2011. References for sphericity and thrust Original application from Spear G. Hanson et al., PRL 35. 1609 (1975). Useful

More formulas

• q=(S11S22 + S11S33 + S22S33 – (S13)² - (S23)² - (S12)²), and

• r=-S11S22S33 – 2S12S13S23 + (S13)²S22 + (S 23)²S11 + (S12)²S33.The cubic equation may be solved with

the substitution λ = x + 1/3. This eliminates the squared term: x3 + ax + b = 0.

Page 7: Sphericity Lee Pondrom May 9, 2011. References for sphericity and thrust Original application from Spear G. Hanson et al., PRL 35. 1609 (1975). Useful

Cubic equation

• x = λ – 1/3; x3 + ax + b = 0.• a = (3q -1)/3; and b = (-2 +9q

+27r)/27.• Define K = b²/4 + a3/27.• If K>0 there are one real and two

conjugate imaginary roots.• If K=0 there are three real roots, at

least two are equal.• If K<0 there are three real unequal

roots

Page 8: Sphericity Lee Pondrom May 9, 2011. References for sphericity and thrust Original application from Spear G. Hanson et al., PRL 35. 1609 (1975). Useful

Solutions to the cubic equation

• K<0 is the usual case for sphericity

• Then xn = 2 (-a/3)1/2cos((φ + 2πn)/3), for n=0,1,2.

• cosφ = (27b2/(-4a3))1/2 , + if b<0.

Page 9: Sphericity Lee Pondrom May 9, 2011. References for sphericity and thrust Original application from Spear G. Hanson et al., PRL 35. 1609 (1975). Useful

More about the cubic equation

• It can be written in terms of the trace and determinant of the matrix S

• λ3–Tr(S)λ2-.5(Tr(S²)–Tr(S)²)λ–det|S|=0

• Here Tr(S)=1, and r=det|S|.

• If det|S|=0, S is singular, and one root λ3=0. The other two roots are

• λ±=(1±(1-4q).5)/2, where q=-.5(Tr(S²)-Tr(S)²)

Page 10: Sphericity Lee Pondrom May 9, 2011. References for sphericity and thrust Original application from Spear G. Hanson et al., PRL 35. 1609 (1975). Useful

Eigenvectors

• The cosine of the polar angle of λ1 was calculated from

• Sψ = λ1ψ, with components of ψ (a,b,c) satisfying a² + b² + c² =1, and the ratios

• a/c=(S12S23-S13(S22-λ1))/denom

• b/c=(S12S13-S23(S11-λ1))/denom

• denom=(S11-λ1)(S22-λ1) – (S12)²

Page 11: Sphericity Lee Pondrom May 9, 2011. References for sphericity and thrust Original application from Spear G. Hanson et al., PRL 35. 1609 (1975). Useful

Transverse eigenvector

• To calculate the azimuthal angle φ the thrust was used in the transverse plane.

• Thrust = ∑i|n∙pi|/∑i|pi|, where n and p are transverse vectors, and n is determined so that Thrust is maximized. ½<Thrust<1.

Page 12: Sphericity Lee Pondrom May 9, 2011. References for sphericity and thrust Original application from Spear G. Hanson et al., PRL 35. 1609 (1975). Useful

Simple example

• Consider a three body decay M->3, and define x1=2E1/M, 0<x1<1. x1+x2+x3=2.

• Phase space

0 x1 1

1 x2 0

Allowed

Page 13: Sphericity Lee Pondrom May 9, 2011. References for sphericity and thrust Original application from Spear G. Hanson et al., PRL 35. 1609 (1975). Useful

Generate the events

• Pick x1 and x2 and check that the point is inside the allowed triangle.

• Calculate x3 and the angles 12 13 in the decay plane.

• Orient the plane at random relative to the master xyz coordinates with a cartesian rotation (α,β,).

• Calculate 9 momentum components.

Page 14: Sphericity Lee Pondrom May 9, 2011. References for sphericity and thrust Original application from Spear G. Hanson et al., PRL 35. 1609 (1975). Useful

Analyze the events

• The three momentum vectors are coplanar, which means that r=0, and λ3=0.

• The two other roots are

• λ = (1(1-4q)1/2)/2, with λ+ = λ1.

• The direction cosines of λ1 give the thrust direction, and λ2 gives the transverse momentum in the decay plane.

Page 15: Sphericity Lee Pondrom May 9, 2011. References for sphericity and thrust Original application from Spear G. Hanson et al., PRL 35. 1609 (1975). Useful

The results for 1000 events generated

Page 16: Sphericity Lee Pondrom May 9, 2011. References for sphericity and thrust Original application from Spear G. Hanson et al., PRL 35. 1609 (1975). Useful

Next try it with jet20 data

• Use calorimeter towers as energy vectors

• Calculate S for the event, with a tower threshold of 1 GeV.

• Two problems:

• 1. cal towers are in detector coordinates (fixable).

• 2. Events are in the center of mass only on average (also fixable).

Page 17: Sphericity Lee Pondrom May 9, 2011. References for sphericity and thrust Original application from Spear G. Hanson et al., PRL 35. 1609 (1975). Useful

10000 jet20 events tower eta distribution

• Left hand plot is before any cuts. Note the ring of fire.

• Right hand plot has tower ET>1 GeV and tower |η|<2.

Before cutsBefore cuts

Before cutsBefore cuts

Before cutsBefore cutstechnical computing 4/8/2011

Page 18: Sphericity Lee Pondrom May 9, 2011. References for sphericity and thrust Original application from Spear G. Hanson et al., PRL 35. 1609 (1975). Useful

Cal towers jet 20 φ and ET

Page 19: Sphericity Lee Pondrom May 9, 2011. References for sphericity and thrust Original application from Spear G. Hanson et al., PRL 35. 1609 (1975). Useful

Cal towers sphericity and λ1

Page 20: Sphericity Lee Pondrom May 9, 2011. References for sphericity and thrust Original application from Spear G. Hanson et al., PRL 35. 1609 (1975). Useful

λ1 η φ

Page 21: Sphericity Lee Pondrom May 9, 2011. References for sphericity and thrust Original application from Spear G. Hanson et al., PRL 35. 1609 (1975). Useful

Jet data from jet20 fileET and η

Page 22: Sphericity Lee Pondrom May 9, 2011. References for sphericity and thrust Original application from Spear G. Hanson et al., PRL 35. 1609 (1975). Useful

Jet data φ and Zvertex

Page 23: Sphericity Lee Pondrom May 9, 2011. References for sphericity and thrust Original application from Spear G. Hanson et al., PRL 35. 1609 (1975). Useful

Met variables

Page 24: Sphericity Lee Pondrom May 9, 2011. References for sphericity and thrust Original application from Spear G. Hanson et al., PRL 35. 1609 (1975). Useful

sumET and metsig

Page 25: Sphericity Lee Pondrom May 9, 2011. References for sphericity and thrust Original application from Spear G. Hanson et al., PRL 35. 1609 (1975). Useful

Met variables

• Look normal – no cuts applied.

Page 26: Sphericity Lee Pondrom May 9, 2011. References for sphericity and thrust Original application from Spear G. Hanson et al., PRL 35. 1609 (1975). Useful

Jet1 compared to λ1

Δ η Δφ

Page 27: Sphericity Lee Pondrom May 9, 2011. References for sphericity and thrust Original application from Spear G. Hanson et al., PRL 35. 1609 (1975). Useful

Delta R=(Δη²+Δφ²)1/2

Page 28: Sphericity Lee Pondrom May 9, 2011. References for sphericity and thrust Original application from Spear G. Hanson et al., PRL 35. 1609 (1975). Useful

Look at the second jet in the event

Page 29: Sphericity Lee Pondrom May 9, 2011. References for sphericity and thrust Original application from Spear G. Hanson et al., PRL 35. 1609 (1975). Useful

Φ resolution for jets and thrust

Page 30: Sphericity Lee Pondrom May 9, 2011. References for sphericity and thrust Original application from Spear G. Hanson et al., PRL 35. 1609 (1975). Useful

Transform tower η to the dijet center of mass

• Define ηcm= (ηjet1 + ηjet2)/2

• Then tower ηcm = tower η – ηcm

• Also correct tower η to the event vertex• For CHA use r=154 cm to the iron face,

and tanθ = tanθ0/(1-zvtanθ0/r)• For PHA use d = 217 cm from the origin to

the iron face, and • tanθ=tanθ0/(1-zv/d). Not much difference.

Page 31: Sphericity Lee Pondrom May 9, 2011. References for sphericity and thrust Original application from Spear G. Hanson et al., PRL 35. 1609 (1975). Useful

Comparison of ηcm and tower ηsphericity λ1 η distribution

Page 32: Sphericity Lee Pondrom May 9, 2011. References for sphericity and thrust Original application from Spear G. Hanson et al., PRL 35. 1609 (1975). Useful

Δη λ1- jet1 ΔR

Page 33: Sphericity Lee Pondrom May 9, 2011. References for sphericity and thrust Original application from Spear G. Hanson et al., PRL 35. 1609 (1975). Useful

Jet triggers

• L1 L2 L3

• ST5 (100) CL20 (50) Jet20

• ST5 (100) CL40 (1) Jet50

• ST10(8) CL60 (1) Jet70

• ST20(1) CL90 (1) Jet100

• Prescales in parenthesis, from Physics_5_05 trigger table.

Page 34: Sphericity Lee Pondrom May 9, 2011. References for sphericity and thrust Original application from Spear G. Hanson et al., PRL 35. 1609 (1975). Useful

Check the lorentz transformation by comparing jets and towers

Page 35: Sphericity Lee Pondrom May 9, 2011. References for sphericity and thrust Original application from Spear G. Hanson et al., PRL 35. 1609 (1975). Useful

Definitions for the previous slide

• labeta = (jet1η +jet2η)/2 ignores jet3

• y* = .5*log((1+β*)/(1-β*))

• β* = ∑i pzi / ∑i Ei summed over all towers with ET > 1 GeV.

Page 36: Sphericity Lee Pondrom May 9, 2011. References for sphericity and thrust Original application from Spear G. Hanson et al., PRL 35. 1609 (1975). Useful

What about jet3 in the jet20 data?

Page 37: Sphericity Lee Pondrom May 9, 2011. References for sphericity and thrust Original application from Spear G. Hanson et al., PRL 35. 1609 (1975). Useful

Compare transverse energy balance, 3 jets and sum towers

Page 38: Sphericity Lee Pondrom May 9, 2011. References for sphericity and thrust Original application from Spear G. Hanson et al., PRL 35. 1609 (1975). Useful

Transverse energy balance is not perfect, and is about the same for

towers and jets.• Longitudinal tower

sum energy is sharpened by the lorentz transformation

Page 39: Sphericity Lee Pondrom May 9, 2011. References for sphericity and thrust Original application from Spear G. Hanson et al., PRL 35. 1609 (1975). Useful

Nothing really improves things

• About 90% of the events with jet1ET>15 GeV have a third ‘jet’, which has an average ET ≈ 7 GeV, and cuts off at 3 GeV!

• Tower sums do not balance in the transverse plane any better than the 3 jets do.

• Longitudinally (η1+η2)/2 sharpens up the tower sum pz, but it is far from perfect.

Page 40: Sphericity Lee Pondrom May 9, 2011. References for sphericity and thrust Original application from Spear G. Hanson et al., PRL 35. 1609 (1975). Useful

Lorentz transformation to the event center of mass

• Using the towers, define a total momentum vector ptot = ∑ipxi x + ∑ipyi y + ∑ipzi z, where (x,y,z) are unit vectors

• And a total energy Etot= ∑I towEi

• Then β* = ptot/Etot , and L = R-1LzR, where R is a space rotation placing the z axis along ptot , and Lz is a Lorentz transformation along the new z axis.

Page 41: Sphericity Lee Pondrom May 9, 2011. References for sphericity and thrust Original application from Spear G. Hanson et al., PRL 35. 1609 (1975). Useful

Total momentum in the event center of mass should vanish, and

it does.

Page 42: Sphericity Lee Pondrom May 9, 2011. References for sphericity and thrust Original application from Spear G. Hanson et al., PRL 35. 1609 (1975). Useful

And the other two components

Page 43: Sphericity Lee Pondrom May 9, 2011. References for sphericity and thrust Original application from Spear G. Hanson et al., PRL 35. 1609 (1975). Useful

So the Lorentz transformation to the event center of mass works

Page 44: Sphericity Lee Pondrom May 9, 2011. References for sphericity and thrust Original application from Spear G. Hanson et al., PRL 35. 1609 (1975). Useful

Event c of m and longitudinal Lorentz transformation are close

Page 45: Sphericity Lee Pondrom May 9, 2011. References for sphericity and thrust Original application from Spear G. Hanson et al., PRL 35. 1609 (1975). Useful

Compare to jet1 in the event

Page 46: Sphericity Lee Pondrom May 9, 2011. References for sphericity and thrust Original application from Spear G. Hanson et al., PRL 35. 1609 (1975). Useful

Two vertex events

• Analysis so far has been Jet20 triggers gjt1ah (1->4) Aug 04->Sep 05 low luminosity

• Now run on Jet20 in a later set of runs gjt1bk (14->17) Oct 07->Apr 08.

• 396 nsec bunch crossing and σinel=60 mb• <L>E32 <n> Pr(0) Pr(1) Pr(>=2) >=2/1data• .5 1.2 .3 .36 .34 .15• 2.0 4.8 .008 .039 .95 .34• <n> is much less than estimated from <L>

Page 47: Sphericity Lee Pondrom May 9, 2011. References for sphericity and thrust Original application from Spear G. Hanson et al., PRL 35. 1609 (1975). Useful

Tower occupancy gjt1bk –cut at ntower=560:63%1v,19%2v.

Page 48: Sphericity Lee Pondrom May 9, 2011. References for sphericity and thrust Original application from Spear G. Hanson et al., PRL 35. 1609 (1975). Useful

Ntowers with ET>1 GeV

Page 49: Sphericity Lee Pondrom May 9, 2011. References for sphericity and thrust Original application from Spear G. Hanson et al., PRL 35. 1609 (1975). Useful

Events with extra vertices

• They have lots of extra tower hits:

• 1 vertex <Ntowers> = 518,

• >=2 vertices <Ntowers> = 636.

• However, a cut on tower ET>1 GeV virtually wipes out the minbias background. 1Vertex <Ntowers>=12.3;

• >=2 vertices <Ntowers>=13.4.

• So the sphericity analysis, which requires towerET>1 GeV is not affected by extra vertices.

Page 50: Sphericity Lee Pondrom May 9, 2011. References for sphericity and thrust Original application from Spear G. Hanson et al., PRL 35. 1609 (1975). Useful

Δvertex gjt1bk

Page 51: Sphericity Lee Pondrom May 9, 2011. References for sphericity and thrust Original application from Spear G. Hanson et al., PRL 35. 1609 (1975). Useful

sphericity

Page 52: Sphericity Lee Pondrom May 9, 2011. References for sphericity and thrust Original application from Spear G. Hanson et al., PRL 35. 1609 (1975). Useful

Tower sum energy in cm

Page 53: Sphericity Lee Pondrom May 9, 2011. References for sphericity and thrust Original application from Spear G. Hanson et al., PRL 35. 1609 (1975). Useful

Thrust axis cm η