Beam Dynamics –2
2021.05.06
K.Kubo
Transfer matrix summary
• Drift space (free space)
• Quadrupole field thin lens
• Dipole field – sector
– with edge effect:
• Determinant =1
1 𝐿 0 1
cosh 𝐾 𝑙 1
𝐾 sinh 𝐾 𝑙 𝐾 sinh 𝐾 𝑙 cosh 𝐾 𝑙 cos 𝐾 𝑙 1
𝐾 sin 𝐾 𝑙
−𝐾 sin 𝐾 𝑙 cos 𝐾 𝑙
, 1 0
±𝑘 1
cos 𝜃 𝜌 sin 𝜃
− 1
𝜌 sin 𝜃 cos 𝜃 , 1 𝜌𝜃 0 1
thin lens × sector × thin lens
Motion described by transfer matrix
• Transverse linear motion can be described by 4x4 Transfer Matrix. 2x2 Matrix without coupling
• Transfer matrix of
– drift(free) space – dipole magnet
– quadrupole magnet
All expressed by same form of quadrupole field
• Transfer matrix of any beam line can be calculated by
multiplying matrix of (short) components
𝑠 0 𝑠 1 𝑠 2 …
… 𝑠 𝑖
𝑠 𝑁
… 𝑠 𝑁−1 𝑀 0→1 𝑀 1→2
𝑀 2→3
𝑠 𝑖+1 …
𝑀 𝑖→𝑖+1 𝑀 𝑁−1→𝑁
𝑀 0→𝑁 = 𝑀 𝑁−1→𝑁 … 𝑀 𝑖→𝑖+1 𝑀 𝑖−1→𝑖 … 𝑀 1→2 𝑀 0→1
Dividing beam line into small pieces, (using computer)) transfer matrix can be accurately calculated.
May be enough for describing motions in given beam line.
But, not enough for designing beam line. (?)
More intuitive(?
直観的に分かりやすい) method is desirable.
Treat motions as oscillations
Transverse motion in circular
accelerator
Closed orbit
(閉軌道)• After one turn, return to the same position and angle:
Closed Orbit
– Particles on this orbit are circulating the same orbit – Without errors, this should be the design orbit
• Closed orbit depends on particle energy
Design orbit
Closed orbit
• From here, for a while, x, y, etc. denote deviation from closed orbit
• ( or, closed orbit = design orbit )
• Particles oscillate around the closed orbit
Closed orbit
Actual orbit
Particles oscillate around the closed orbit
Linear motion with 1 degree of freedom
0 )
(
'' + K s x = x
1 degree of freedom
• Ignore x-y coupling. (No skew quadrupole field)
• Consider motions in only x or y direction.
Linear motion
• Linear motion around closed orbit can be expressed by a differential equation
• K is strength of quadrupole field at location s.
• In a circular accelerator, K is periodic
• where L is circumference of the accelerator.
) ( )
( L s K s
K + =
Linear motion with 1 degree of freedom
0 )
(
'' + K s x = x
1 degree of freedom
• Ignore x-y coupling. (No skew quadrupole field)
• Consider motions in only x or y direction.
Linear motion
• Linear motion around closed orbit can be expressed by a differential equation
• K is strength of quadrupole field at location s.
• In a circular accelerator, K is periodic
• where L is circumference of the accelerator.
) ( )
( L s K s
K + =
Transfer Matrix of all “linear”
components (drift space, dipole field,
quadrupole field) have the same form as
quadrupole field)
If K is constant, the equation can be solved easily
Generally, K depends on s,
solution can be expressed as
Linear motion with 1 degree of freedom
0 )
(
'' + K s x = x
Generally, for a periodic function , differential equation
) ( )
( L s K s
K + =
) )
( cos(
) ( )
( s = a s s +
0x beta-function
Hill’s equation has this form of solution. There are two cases:
, , a are all real. stable oscillation
, , a are imaginary. divergent.
Such accelerators do not work has solution with a form
“Hill’s equation”
with periodic function
: Depend on s, common for all particles
: Constant, different for different particles
) cos(
0 +
= a x
0 )
(
'' + K s x = x
+ − +
= cos( ) ' sin( )
2
' '
0
0 a
x
+
+
−
+
− −
= ' ' '' sin( )
) cos(
' 4
' 2
'' ''
3 2 0 02
a
x
0 '
4 ' 2
''
23
2
− + =
−
K ' ' '' 0
= +
Motion is not solved yet.
①
②
③ Substituting ② and ③ into ① ,
and require coefficients of sine and cosine to be zero
0 '
4 ' 2
''
23
2
− + =
−
K
0 '' ' '
= +
( ) ' ' 0 '' 1
' '
=
=
+
' = const ( ) = 1
0 4 1
' 2
''
2 2= +
−
−
K
(this constant can be set as 1 without losing generality.
Because of another constant a,
can be multiplied by any constant.) (1)
(2)
From (2)
(1) becomes
In principle, can be solved if K is known.
(usually numerically solved)
(cannot generally be solved analytically)
Betatron oscillation
) )
( cos(
) ( )
( s = a s s + 0 x
( sin( ( ) ) ( ) cos( ( ) ) )
) ) (
(
' 0 0
+ + +
−
= s s s
s s a
x
ds d
2
− 1 ds
d / /
1 =
phase n
oscillatio
:
Oscillation around closed orbit,
with s-dependent amplitude and phase advance
𝛽 : beta-function, represents s-dependence of amplitude
Beta-function
If
second-order differential equation with two boundary conditions
→ No ambiguity Ambiguous without periodicity
(linac, transport line)
≠ 0
In a region of 𝐾 = 0
𝛽 𝑠 = 1 + 𝛼 2 (0)
𝛽(0) 𝑠 2 − 2𝛼 0 𝑠 + 𝛽 0
𝛼 ≡ − 1 2
𝑑𝛽 𝑑𝑠
In a drift space, beta-function is a 2
ndorder function of s.
(Downward-convex parabola)
𝛽𝛽 ′′
2 − 𝛽 ′2
4 − 1 = 0 → 𝛽𝛽 ′′
2 − 𝛽 ′2 4
′
= 𝛽𝛽 ′′′
2 = 0 → 𝛽 ′′′ = 0
Transfer-matrix can be written by betatron oscillation parameters,
M(s 1 → s 2 ) : expressed by
(s 1 ), (s 1 ), (s 1 ), (s 2 ), (s 2 ), (s 2 )
Some manipulations of betatron oscillation equations
) )
( cos(
) ( )
( s = a s s + 0 x
( sin( ( ) ) ( ) cos( ( ) ) )
) ) (
(
' 0 0
+ + +
−
= s s s
s s a
x
( )
sin ) ( /
1 )
( ' cos
) ( /
sin ) )
( sin(
cos ) )
( cos(
) )
( cos(
) )
( cos(
) (
1 1 1
1 1
2 1
1 2
0 1
2 0
1 2
0 1
2 0
2 2
2
s x s
x s
x
s a
s a
s a
s a
s x
−
−
−
=
+
− +
=
+ +
= +
=
( = ( s
2) − ( s
1) )
Relation of x, x’ at s
1and s
2: Phase advance between s
1and s
2Transfer-matrix written by betatron oscillation parameters
𝑥 𝑠 2 = 𝛽 2
𝛽 1 𝑥 𝑠 1 cos 𝜓 − 𝛽 2 − 𝛽 1 𝑥 ′ 𝑠 1 − 𝛼 1 1
𝛽 1 𝑥 𝑠 1 sin 𝜓
= 𝛽
2𝛽
1cos 𝜓 + 𝛼 1 𝛽
2𝛽
1sin 𝜓 𝑥 𝑠 1 + 𝛽 1 𝛽 2 sin 𝜓 𝑥′(𝑠 1 )
( )
( ) ( ) ( )
− − +
− +
+
=
sin cos cos
sin 1
sin sin
cos )
, (
2 2
1 1
2
1 2
1 2
1 2 1
1 2
1 2
s s M
( = ( s
2) − ( s
1) )
Transfer matrix from s1 to s2
𝑥 ′ (𝑠 2 ) = ⋯
Transfer-matrix written by betatron oscillation parameters
( )
( ) ( ) ( )
− − +
− +
+
=
sin cos cos
sin 1
sin sin
cos )
, (
2 2
1 1
2
1 2
1 2
1 2 1
1 2
1 2
s s M
( = ( s
2) − ( s
1) )
Inversely, change of the parameters can be given by transfer matrix (formula will be given later)
1 , 1 , 1 → 2 , 2 , 2
Determinant of Transfer-matrix is 1
( )
( 1 ) sin ( ) cos ( cos sin ) 1
sin sin
cos det
2 2
1 1
2
1 2
1 2
1 2 1
1 2
=
− − +
− +
+
Determinant of Transfer-matrix is 1 for linear motion
Dividing the beam line into N short sections.
“Tune” in circular accelerator
Important parameter of circular accelerator Phase advance in one turn
( L + s ) − ( s ) = = 2
Does not depend on s.
( This can be shown from is periodic function )
y x
, are called “tunes”
ds d / /
1 =
s 1
s 2
is periodic:
(same at the same position at any turns)
Phase change in one turn does
not depend on position.
One-turn, multi-turn Transfer-matrix
( )
( ) ( )
+ −
−
+
=
+
sin sin cos
1
sin sin
cos )
,
( L s s
2M
( )
( )
( ) ( )
+ −
−
+
= +
=
+ 1 sin( ) cos( ) sin( )
) sin(
) sin(
) cos(
) , (
) ,
(
2
n n n
n n
n s
s L M s
s nL
M
n1 turn
n turns
phase advance becomes n times
( 𝜑 = 2𝜋𝜈)
Stability Condition
( )
( ) ( )
+ −
−
+
=
+
sin sin cos
1
sin sin
cos )
,
( L s s
2M 1-turn transfer-matrix
2 cos
2 )
( =
Tr M
is real → stable
2 ) cosh(
2 cos
2 )
( = =
Tr M i
is (pure) imaginary → unstable
Absolute of Trace can be used for checking stability.
cos and sin include
exponentially divergent term
cos and sin are oscillating
Look trance of the matrix (= 2 cos 𝜑)
( )
( ) ( )
+ −
−
+
=
+
sin sin cos
1
sin sin
cos )
,
( L s s
2M
, , Should be either All real or
All pure imaginary
All components are real. (transformation of physical values.)
→ Trace 𝑀 = 𝑀
11+ 𝑀
22= 2 cos 𝜑 = 𝑟𝑒𝑎𝑙
→ 𝜑 is either real or pure imaginary
𝛼 sin 𝜑, 𝛽 sin 𝜑 should be real (𝑀
11− 𝑀
22, 𝑀
12are real)
→ if 𝜑 is real, sin 𝜑 real → 𝛼, 𝛽 real.
if 𝜑 is pure imaginary, sin 𝜑 ∶ pure imaginary → 𝛼, 𝛽: pureimaginary.
Are the parameters real or imaginary?
( )
( )
( ) ( )
+ −
−
+
= +
=
+ 1 sin( ) cos( ) sin( )
) sin(
) sin(
) cos(
) , (
) ,
(
2
n n n
n n
n s
s L M s
s nL
M
nn turns
Divergent (becomes infinitely large for infinitely large n ) if 𝜑 is imaginary.
2 ) cosh(
2 cos
2 )
( = =
Tr M i
𝑇𝑟𝑎𝑐𝑒(𝑀) can be used for checking stability
x a
1/2x'
a(1+
2/)
1/2a/
x'=-(/)x
Betatron oscillation In phase space, (x-x’)
a(1+
2/
1/2)
At a certain location, x-x’
of one particle at any turns are all on the same ellipse.
At a certain location, x-x’
of any particles with same a are all on the same
ellipse
cos a
x =
( )
sin cos
' = − a +
x Same amplitude
Constant a, change
Courant-Snyder Invariance
2 2
2 2 2
2
1 2 ' '
1 '
a x
xx x
x x
x = + + + =
+
+
From betatron oscillation formula, the following is ocnstant
( s independent, determined by initial condition )
Invariance of each particle
Consider many particles in a beam
Emittance
2 2
2 x ' xx '
x x −
Invariant in linear motion
: Average of particles
ds x dx ds x
xx dx ds
x dx x
ds x x dx ds
d '
' '
' 2 '
2 '
) 2
(
2=
2+
2− +
x s ds K
x d ds
dx ds
x dx ' ( )
,
'
22
= −
=
=
inserting , this becomes zero.
Conservation of Emitance can be also shown from that the determinant of transfer-matrix is 1. (next next page)
2
2
'
, ' '
, ' '
' ,
' K x
ds x dx x
ds x xx dx
ds K x dx ds xx
x dx = = − = = −
Meaning of Emittance ?
If particles are distributed uniformly in an ellipse, Emittance ~ Area of ellipse in phase space (x, x’)
x=ac
x’ = a/c x’ = ab/c
x’
x
Meaning of Emittance ?
For general distribution
Emittance = Area of ellipse of 1-sigma in phase space/
𝑥
2𝑥
′2𝜀 𝑥
2𝜀
𝑥′
2Emittance is invariant, shown from Beam Matrix form
2 2
2 x ' xx '
x x −
( ' )
det ' '
'
det 2 '
2
2 x x
x x x
xx
xx x
x
=
=
) , ' (
' ) '
, ' (
'
'
1 2 )
( 2 2
1 2 )
( 2 2
1 2
s s x M
xx
xx s x
s x M
xx
xx
x
Ts s
=
Change of beam matrix from s1 to s2 can be expressed by transfermatrix
) det det
det ,
det (det
, 1 det
B A
AB A
A M
T = =
=
Determinant unchanged because determinant of transfer-matrix is 1
→ Emittance is invariant
Emittance - oscillation parameters
2 0 0
2 0
2 2
0 2 2
2 sin cos sin cos
= a a − a
Betatron oscillation
Emittance can be expressed as
a 、
0are different for different particles (initial condition).
Average <> should be taken for these parameters.
It is easy to show emittance is unchanged by adding common constant to
0.
𝑥 = 𝑎 𝛽 cos(𝜙 + 𝜙 0 ) 𝑥′ = − 𝑎
𝛽 sin(𝜙 + 𝜙 0 ) + 𝛼 cos(𝜙 + 𝜙 0 )
2 2
2 x ' xx '
x x −
Emittance, beam size, matching
In special case,
0distributes uniformly from 0 to 2, ( no
correlation between a and
0and average can be taken independently ) , Same beam size at the same beta-function.
) )
( ( cos )
( )
( )
( 2 2 2 0
x s x s = s a s + Beam size can be defined as
Generally, beam size may be different at different turns at the same location in a circular accelerator.
) ( 2
/ ) ( )
( s a
2s s
x
= =
This condition is called “matched”.
Beam parameters in matched condition
Bea msize =
emittance = a
2/ 2
= x 2
−
= ' xx
𝑥′ 2 = 𝜀 1 + 𝛼 2
𝛽 = 𝜀𝛾
𝑥
2= 𝑎
2/2 𝛽 𝑥𝑥′ = − 𝑎
2/2 𝛼 𝑥′
2= 𝑎
2/2 1 + 𝛼
2𝛽 = 𝑎
2/2 𝛾
Average over particles Average of one particle for many turns (no relation with matching)
“Matching” means:
Particle distribution and beam line design are matched.
Parameters Twiss
called are
, ,
Note on “matched beam”
For the same emittance beam, matched beam gives the minimum required aperture.
beam size:
If not matched, beam size at a certain location changes turn by turn.
The maximum beam size at s is larger than (s ) )
(s
Change of Twiss parameters
( )
−
= −
=
2 2
' '
' '
' xx x
xx x x
x x x
) , ( )
,
(
2 11 1
1 1
1 2 2
2
2
2
M s s M
Ts s
−
= −
−
−
− +
, 1
22 , 1
ds
d
M : transfer matrix
𝑥
𝑥′ 𝑥 𝑥′ = 𝑥 2 𝑥𝑥′
𝑥𝑥′ 𝑥′ 2
𝑥 2 2 𝑥 2 𝑥 2 ′
𝑥 2 𝑥 2 ′ 𝑥′ 2 2 = 𝑥 2
𝑥 2 ′ 𝑥 2 𝑥 2 ′
= 𝑀 𝑥 1
𝑥 1 ′ 𝑥 1 𝑥 1 ′ 𝑀 𝑇 = 𝑀 𝑥 1 2 𝑥 1 𝑥 1 ′
𝑥 1 𝑥 1 ′ 𝑥′ 1 2 𝑀 𝑇
Because
Betatron Oscillation Summary
) )
( cos(
) ( )
( s = a s s + 0 x
( sin( ( ) ) ( ) cos( ( ) ) )
) ) (
(
' 0 0
+ + +
−
= s s s
s s a
x
ds d
2
− 1
= ds
d /
= ( , ( L + s ) = , ( s ) )
• Tune: Phase advance in one turn divided by 2
• Stability condition:
• Courant-Snyder invariance :
• emittance :
• matching :
Particle distribution and beam line design are matched
( )
22