2.1. time-dependent hamiltonian - university of...
TRANSCRIPT
2-1
2.1. TIME-DEPENDENT HAMILTONIAN
Mixing of eigenstates by a time-dependent potential
For many time-dependent problems, most notably in spectroscopy, we often can partition the
time-dependent Hamiltonian into a time-independent part that we can describe exactly and a
time-dependent part
H = H
0+V t( ) (2.1)
Here H
0 is time-independent and
V t( ) is a time-dependent potential, often an external field.
Nitzan, Sec. 2.3., offers a nice explanation of the circumstances that allow us to use this
approach. It arises from partitioning the system into internal degrees of freedom in H0 and
external degrees of freedom acting on H0. If you have reason to believe that the external
Hamiltonian can be treated classically, then eq. (2.1) follows in a straightforward manner. Then
there is a straightforward approach to describing the time-evolving wavefunction for the system
in terms of the eigenstates and energy eigenvalues ofH0
. We know
H
0n = E
nn . (2.2)
The state of the system can be expressed as a superposition of these eigenstates:
! t( ) = cn
t( ) n
n
" (2.3)
The TDSE can be used to find an equation of motion for the expansion coefficients
c
kt( ) = k ! t( ) (2.4)
Starting with
! "
!t=#i
!H " (2.5)
! ck
t( )!t
= "i
!k H # t( ) (2.6)
Andrei Tokmakoff, MIT Department of Chemistry, 2/13/2007
2-2
inserting
n n
n
! = 1
= !i
!k H n
n
" cn
t( ) (2.7)
substituting eq. (2.1) we have:
! ck
t( )!t
= "i
!k H
0+V t( )( ) n
n
# cn
t( )
= "i
!E
n$
kn+V
knt( )%
&'(
n
# cn
t( ) (2.8)
or,
!ck
t( )!t
+i
!E
kc
kt( ) = "
i
!V
knt( )c
nt( )
n
# . (2.9)
If we make a substitution
c
mt( ) = e
! iEm
t !b
mt( ) , (2.10)
which defines a slightly different expansion coefficient, we can simplify considerably. Notice
that b
kt( )
2
= ck
t( )2
. Also, b
k0( ) = c
k0( ) . In practice what we are doing is pulling out the
“trivial” part of the time-evolution, the time-evolving phase factor for state m. The reasons will
become clear later when we discuss the interaction picture. It is easy to calculate bkt( ) and then
add in the extra oscillatory term at the end. Now eq. (2.9) becomes
e! iE
kt !
"bk
"t= !
i
!V
knt( ) e
! iEnt !
bn
t( )n
# (2.11)
or
i!!b
k
!t= V
knt( ) e
" i#nk
tb
nt( )
n
$ (2.12)
This equation is an exact solution. It is a set of coupled differential equations that describe how
probability amplitude moves through eigenstates due to a time-dependent potential. Except in
simple cases, these equations can’t be solved analytically, but it’s often straightforward to
integrate numerically.
2-3
Resonant Driving of Two-level System
As an example of the use of these equations, let’s describe what happens when you drive a two-
level system with an oscillating potential.
V t( ) =V cos!t =Vf t( ) (2.13)
Note: This is what you expect for an electromagnetic field interacting with charged particles, i.e.
dipole transitions. In a simple sense, the electric field is
E t( ) = E
0cos!t (2.14)
For a particle with charge q in a field E , the force on the particle is
F = q E (2.15)
which is the gradient of the potential
F
x= !
"V
"x= qE
x# V = !qE
xx (2.16)
qx is just the x component of the dipole momentµ . So matrix elements in V look like:
k |V (t) | ! = !qEx
k | x | ! cos"t (2.17)
More generally,
V = !E "µ . (2.18)
We’ll look at this a bit more carefully later.
So,
V t( ) =V cos!t = "E0#µ cos!t
Vk!
t( ) =Vk!
cos!t = "E0#µ
k!cos!t
. (2.19)
We will now couple our two states k and
! with the
oscillating field. Let’s ask if the system starts in ! what is the
probability of finding it in k at time t ?
2-4
The system of differential equations that describe this situation are:
i!!
!tb
kt( ) = b
nt( )V
knt( ) e
" i#nk
t
n
$
= bn
t( )Vkn
e" i#
nkt%
1
2e" i# t
+ e+ i# t( )
n
$
(2.20)
Or more explicitly
i! "bk= 1
2b#V
k#e
i !k#"!( )t
+ ei !
k#+!( )t#
$%&'(+ 1
2b
kV
kke
i! t+ e
" i! t#$
&'
i! "b#= 1
2b#V##
ei! t
+ e" i! t#
$&' +
1
2b
kV#k
ei !#k"!( )t
+ ei !#k+!( )t#
$%&'(
or
e" i !
k#+!( )t
+ e" i !
k#"!( )t#
$%&'(
(2.21)
Two of these terms can be dropped since (for our case) the diagonal matrix elements V
ii= 0 . We
also make the secular approximation (rotating wave approximation) in which the nonresonant
terms are dropped. When !
k!"! , terms like e± i! t or e
i !k!+!( )t oscillate very rapidly (relative
to V
k!
!1
) and so don’t contribute much to change of cn
. (Remember that !
k! is positive). So we
have:
!bk=!i
2"b#V
k#e
i "k#!"( )t (2.22)
!b"=!i
2#b
kV"k
e! i "
k"!"( )t (2.23)
Note that the coefficients are oscillating out of phase with one another.
Now if we differentiate eq. (2.22):
!!bk=!i
2"
!b#V
k#e
i "k#!"( )t
+ i "k#!"( )b
#V
k#e
i "k#!"( )t#
$%&'(
(2.24)
Rewrite eq. (2.22):
2-5
b!=
2i"
Vk!
#bk
e! i "
k!!"( )t (2.25)
and substitute (2.25) and (2.23) into (2.24), we get linear second order equation for b
k.
!!bk! i "
k"!"( ) !b
k+
Vk"
2
4#2
bk= 0 (2.26)
This is just the second order differential equation for a damped harmonic oscillator:
a!!x + b !x + cx = 0 (2.27)
x = e! b 2a( )t
Acosµt + Bsinµt( )
µ =1
2a4ac ! b
2"#
$%
1
2
(2.28)
With a little more work, and remembering the initial conditions b
k0( ) = 0 and
b!
0( ) = 1 , we find
Pk= b
kt( )
2
=V
k!
2
Vk!
2
+ "2!
k!"!( )
2sin
2#
rt (2.29)
Where the Rabi Frequency
!R=
1
2!V
k"
2
+ !2 "
k"#"( )
2$%&
'()
1
2
(2.30)
Also, P!= 1! b
k
2
(2.31)
The amplitude oscillates back and forth between the two states at a frequency dictated by the
coupling between them. [ Note a result we will return to later: Electric fields couple quantum
states, creating coherences! ]
An important observation is the importance of resonance between the driving potential
and the energy splitting between states. To get transfer of probability density you need the
driving field to be at the same frequency as the energy splitting. On resonance, you always drive
probability amplitude entirely from one state to another.
2-6
The efficiency of driving between ! and k states drops off with detuning. Here plotting the
maximum value of P
k! as a function of frequency:
Readings
This lecture draws from
1. C. Cohen-Tannoudji, B. Diu, and F. Lalöe, Quantum Mechanics, Vol. 2. (Wiley-
Interscience, Paris, 1977)
2. J. J. Sakurai, Modern Quantum Mechanics. (Addison-Wesley, Reading, MA, 1994).
2-7
2.2. QUANTUM DYNAMICS
The motion of a particle is described by a complex wavefunction ! r ,t( ) that gives the
probability amplitude of finding a particle at point r at time t . If we know ! r ,t
0( ) , how does
it change with time?
! r ,t
0( ) ?" #" ! r ,t( )
t > t
0 (2.32)
We will use our intuition here (largely based on correspondence to classical mechanics). We are
seeking an equation of motion for quantum systems that is equivalent to Newton’s (or more
accurately Hamilton’s) equations for classical systems.
We start by assuming causality: ! t
0( ) precedes and determines
! t( ) . So will be
deriving a deterministic equation of motion for ! r ,t( ) . Also, we assume time is a continuous
parameter:
limt!t
0
" t( ) = " t0
( ) (2.33)
Define an operator that gives time-evolution of system.
! t( ) =U t,t
0( ) ! t0( ) (2.34)
This “time-displacement operator” or “propagator” is similar to the “space-displacement
operator”
! r( ) = e
ik (r" r0
)! r
0( ) (2.35)
which moves a wavefunction in space.
Andrei Tokmakoff, MIT Department of Chemistry, 2/13/2007
2-8
We also say that U does not depend on the particular state of the system ! . This is
necessary for conservation of probability, i.e. to retain normalization for the system. If
! t
0( ) = a
1"
1t0
( ) + a2"
2t0
( ) (2.36)
then
! t( ) =U t,t0( ) ! t
0( )
=U t,t0( )a1
"1
t0( ) +U t,t
0( )a2"
2t0( )
= a1
t( ) "1+ a
2t( ) "2
(2.37)
This is a reflection of the importance of linearity in quantum systems. While a
it( ) typically not
equal to a
i0( ) ,
an
t( )n
!2
= an
t0
( )n
!2
(2.38)
Properties of U(t,t0)
1) Unitary. Note that for eq. (2.38) to hold and for probability density to be conserved, U must
be unitary
P = ! t( ) ! t( ) = ! t
0( ) U†U ! t
0( ) (2.39)
which holds only if U †=U
!1 . In fact, this is the reason that equates unitary operators with
probability conservation.
2) Time continuity:
U t,t( ) = 1 . (2.40)
3) Composition property. If we take the system to be deterministic, then it stands to reason
that we should get the same wavefunction whether we evolve to a target time in one step
t0! t
2( ) or multiple steps
t0! t
1! t
2( ) :
2-9
U t
2,t
0( ) =U t2,t
1( )U t1,t
0( ) (2.41)
Note, since U acts to the right, order matters:
! t2( ) =U t
2,t
1( )U t1,t
0( ) ! t0( )
=U t2,t
1( ) ! t1( )
(2.42)
Equation (2.41) is already very suggestive of an exponential form. Furthermore, since time
is continuous and the operator is linear it also suggests what we will see that the time
propagator is only dependent on a time interval
U t
1,t
0( ) =U t1! t
0( ) (2.43)
and
U t
2! t
0( ) =U t
2! t
1( )U t
1! t
0( ) (2.43
4) Time-reversal. The inverse of the time-propagator is the time reversal operator. From eq.
(2.41):
U t,t
0( )U t0,t( ) = 1 (2.32)
!U
"1t,t
0( ) =U t0,t( ) . (2.33)
Finding an equation of motion for U
Let’s find an equation of motion that describes the time-evolution operator using the change of
the system for an infinitesimal time-step, !t : U t
0+ !t,t
0( )
lim! t"0
U t0+ !t,t
0( )= 1 (2.34)
We expect that for small !t , the difference between U t0,t0( ) and
U t
0+ !t,t
0( ) will be linear in
!t (This is based on analogy to how we think of deterministic motion in classical systems)
2-10
U t
0+ !t,t
0( ) =U t0,t
0( ) " i# t0( )!t (2.35)
We take ! to be a time-dependent Hermetian operator. We’ll see later why the second term
must be imaginary. So, now we can write a differential equation for U. We know that
U t + !t,t
0( ) =U t + !t,t( )U t,t0( ) . (2.36)
Knowing the change of U during the period !t allows us to write a differential equation for the
time-development of U t,t
0( ) . The equation of motion for U is
d U t,t0( )
dt= lim
!t"0
U t + !t,t0( ) #U t,t
0( )!t
= lim!t"0
U t + !t,t( ) #1$%
&'U t,t
0( )!t
(2.37)
Where I have substituted eqn. (2.35) in the second step. So we have:
!U t,t0( )
!t= "i#U t,t
0( ) (2.38)
You can now see that the operator needed a complex argument, because otherwise probability
density would not be conserved (it would rise or decay). Rather it oscillates through different
states of the system.
We note that ! has units of frequency. Since (1) quantum mechanics says E = !! and
(2) in classical mechanics the Hamiltonian generates time-evolution, we write
! =H
! (2.39)
Where ! can be a function of time. Then
i!
!
!tU t,t
0( ) = HU t,t0( ) (2.40)
Multiplying from right by ! t
0( ) gives the TDSE
2-11
i!!
!t" = H " (2.41)
We are also interested in the equation of motion for U † which describes the time-evolution of the
conjugate wavefunctions. Following the same approach and recognizing that U
†t,t
0( ) acts to
the left:
! t( ) = ! t
0( ) U†
t,t0( ) , (2.42)
we get
!i!
"
"tU
†t,t
0( ) =U†
t,t0( ) H (2.43)
Evaluating U(t,t0): Time-independent Hamiltonian
Direct integration of eqn. (2.40) suggests that U can be expressed as:
U t,t0( ) = exp !
i
!H t ! t
0( )"
#$
%
&' (2.44)
Since H is an operator, we will define this operator through the expansion:
exp !iH
!t ! t
0( )"
#$
%
&' = 1+
!iH
!t ! t
0( ) +!i
!
()*
+,-
2H t ! t
0( )"# %&2
2+… (2.45)
Note H commutes at all t . You can confirm the expansion satisfies the equation of motion
forU .
To evaluate U for the time-independent Hamiltonian, we expand in a set of eigenkets:
H n = En
n n
n
! n = 1 (2.46)
So we have
2-12
U t,t0( ) = exp !iH t ! t
0( ) / !"#
$% n n
n
&
= n exp !iEn
t ! t0( ) / !"
#$%
n
& n
(2.47)
and
! t( ) =U t,t0( ) ! t
0( )
= n n ! t0( )
cn t0( )! "# $#
exp"i
%E
nt " t
0( )#
$%
&
'(
n
)
= n cn
t( )n
)
(2.48)
Expectation values of operators are given by
A t( ) = ! t( ) A! t( )
= ! t0( )U
†t,t
0( ) AU t,t0( )! t
0( ) (2.49)
For an initial state
! t0
( ) = cn
n
" n , we showed in eq. 1.48 that
A = cm
*m m e
+i!m
t"t0( )m A n e
"i!n
t"t0( )n n
n,m
# cn
= cm
*c
nA
mne"i!
nmt"t0( )
n,m
#
= cm
*t( )c
nt( ) A
mn
n,m
#
(2.50)
which is Tr(ρ(t)A). The correlation amplitude
! " t( ) was given in eq. 1.45.
2-13
Evaluating the time-evolution operator: Time-dependent Hamiltonian
At first glance it may seem straightforward to deal with. If H is a function of time, then the
formal integration of i!!U !t = HU gives
U t,t0( ) = exp
!i
!H "t( )d "t
t0
t
#$
%&
'
() (2.51)
We would define this exponential as an expansion in a series, and substitute into the equation of
motion to confirm it:
U t,t0
( ) = 1!i
!H "t( )d "t
t0
t
# +1
2!
!i
!
$%&
'()
2
d "tt0
t
# d ""tt0
t
# H "t( )H ""t( ) +… (2.52)
Then if we know the eigenstates of H, we could use eq. (2.46) to express U as
U t,t0( ) = n exp
!i
!E
j"t( )d "t
t0
t
#$
%&
'
()
n
* n (2.53)
However, this is dangerous; we are not treating H as an operator. We are assuming that the
Hamiltonians at different times commute!
H !t( ), H !!t( )"#
$% = 0 . It is only the case for special
Hamiltonians with a high degree of symmetry, in which the eigenstates have the same symmetry
at all times. This holds for instance in the case of a degenerate system, i.e., spin ½ system, with
a time-dependent coupling. Generally speaking this is not the case.
Now, let’s proceed a bit more carefully assuming that the Hamiltonian at different times
does not commute. Integrate
!
!tU t,t
0( ) ="i
!H t( )U t,t
0( ) (2.54)
To give: U t,t
0( ) = 1!i
!d" H "( )U " ,t
0( )t0
t
# (2.55)
This is the solution; however, it’s not very practical since U t,t0( ) is a function of itself. But we
can solve by iteratively substituting U into itself. First Step:
2-14
U t,t0( ) = 1!
i
!d"
t0
t
# H "( ) 1!i
!d $"
t0
"
# H $"( )U $" ,t0( )
%
&'
(
)*
= 1+!i
!
+,-
./0
d"t0
t
# H "( ) +!i
!
+,-
./0
2
d" d $" H "( )H $"( )U $" ,t0( )
t0
"
#t0
t
# (2.56)
Note in the last term of this equation, the integration variable !" preceeds! . Pictorally, the area
of integration is
Next Step:
U t,t0( ) = 1+
!i
!
"#$
%&'
d(t0
t
) H (( )
+!i
!
"#$
%&'
2
d(t0
t
) d *(t0
(
) H (( )H *(( )
+!i
!
"#$
%&'
3
d(t0
t
) d *(t0
(
) d **(t0
*(
) H (( )H *(( )H **(( )U **( ,t0( )
(2.57)
From this expansion, you should be aware that there is a time-ordering to the interactions. For
the third term, !!" acts before !" , which acts before! : t0! ""# ! "# ! # ! t .
Imagine you are starting in state !
0= ! and you are working toward a target
state ! = k . The possible paths and associated time variables are:
2-15
The expression for U describes all possible paths between initial and final state. Each of these
paths interfere in ways dictated by the acquired phase of our eigenstates under the time-
dependent Hamiltonian. The solution for U obtained from this iterative substitution is known as
the (positive) time-ordered exponential
U t,t0( ) ! exp
+
"i
!d#
t0
t
$ H #( )%
&'
(
)*
! T exp"i
!d#
t0
t
$ H #( )%
&'
(
)*
= 1+"i
!
+,-
./0
n
n=1
1
2 d#n
d#n
t0
#
$ … d#1
t0
t
$t0
t
$ H #n
( )H #n"1( )…H #
1( )
(2.58)
( T is known as the Tyson time-ordering operator.) In this expression the time-ordering is:
t0!"
1!"
2!"
3...."
n! t
t0! … ##" ! #" ! "
(2.59)
So, this expression tells you about how a quantum system evolves over a given time interval, and
it allows for any possible trajectory from an initial state to a final state through any number of
intermediate states. Each term in the expansion accounts for more possible transitions between
different intermediate quantum states during this trajectory.
Compare the time-ordered exponential with the traditional expansion of an exponential:
1+1
n!
!i
!
"#$
%&'
n
d(n… d(
1H (
n( )H (
n!1( )…H (
1( )
t0
t
)t0
t
)n=1
*
+ (2.60)
2-16
Here the time-variables assume all values, and therefore all orderings for H !i( ) are calculated.
The areas are normalized by the n! factor. (There are n! time-orderings of the !n times.)
We are also interested in the Hermetian conjugate ofU t,t0( ) , which has the equation of
motion in eq. (2.43)
!
!tU
†t,t
0( ) =+i
!U
†t,t
0( )H t( ) (2.61)
If we repeat the method above, remembering that U
†t,t
0( ) acts to the left:
! t( ) = ! t
0( ) U†
t,t0( ) (2.62)
then from
U
†t,t
0( ) =U†
t0,t
0( ) +i
!d!
t0
t
" U†
t,!( )H !( ) (2.63)
we obtain a negative-time-ordered exponential:
U†
t,t0( ) = exp!
i
!d"
t0
t
# H "( )$
%&
'
()
= 1+i
!
*+,
-./
n
d"n
d"n!1
… d"1
t0
"2# H "
1( )H "2( )…H "
n( )
t0
"n#
t0
t
#n=1
0
1 (2.64)
Here the H !i( ) act to the left.
Readings
This lecture draws from the following:
1. Merzbacher, E. Quantum Mechanics, 3rd ed. (Wiley, New York, 1998), Ch. 14.
2. Mukamel, S. Principles of Nonlinear Optical Spectroscopy (Oxford University Press, New
York, 1995), Ch. 2.
3. Sakurai, J. J. Modern Quantum Mechanics, Revised Edition (Addison-Wesley, Reading, MA,
1994), Ch. 2.
2-17
2.3 SCHRÖDINGER AND HEISENBERG REPRESENTATIONS
The mathematical formulation of the dynamics of a quantum system is not unique. So far we
have described the dynamics by propagating the wavefunction, which encodes probability
densities. This is known as the Schrödinger representation of quantum mechanics. Ultimately,
since we can’t measure a wavefunction, we are interested in observables (probability amplitudes
associated with Hermetian operators). Looking at a time-evolving expectation value suggests an
alternate interpretation of the quantum observable:
A t( ) = ! t( ) A ! t( ) = ! 0( ) U†AU ! 0( )
= ! 0( ) U†( ) A U ! 0( )( )
= ! 0( ) U†AU( )! 0( )
(2.65)
The last two expressions here suggest alternate transformation that can describe the dynamics.
These have different physical interpretations:
1) Transform the eigenvectors: ! t( ) "U ! . Leave operators unchanged.
2) Transform the operators: A t( )!U
†AU . Leave eigenvectors unchanged.
(1) Schrödinger Picture: Everything we have done so far. Operators are stationary.
Eigenvectors evolve under U t,t
0( ) .
(2) Heisenberg Picture: Use unitary property of U to transform operators so they evolve
in time. The wavefunction is stationary. This is a physically appealing picture, because
particles move – there is a time-dependence to position and momentum.
Let’s look at time-evolution in these two pictures:
Schrödinger Picture
We have talked about the time-development of ! , which is governed by
i!!
!t" = H " (2.66)
Andrei Tokmakoff, MIT Department of Chemistry, 2/22/2007
2-18
in differential form, or alternatively ! t( ) =U t,t
0( ) ! t0( ) in an integral form. In the
Schrödinger picture, for operators typically
!A
!t= 0 . What about observables? For expectation
values of operators
A(t) = ! t( ) A! t( ) :
i!!!t
A(t) = i! " A!"!t
+!"!t
A" + "!A
!t"
#
$
%%
&
'
((
= " A H " ) " H A"
= " A, H#$ &' "
= A, H#$ &'
(2.67)
Alternatively, written for the density matrix:
i!!!t
A(t) = i!!!t
Tr A"( )
= i!Tr A!!t
"#$%
&'(
= Tr A H ,")* +,( )= Tr A, H)* +,"( )
(2.68)
If A is independent of time (as we expect in the Schrödinger picture) and if it commutes withH ,
it is referred to as a constant of motion.
Heisenberg Picture
From eq. (2.65) we can distinguish the Schrödinger picture from Heisenberg operators:
A(t) = ! t( ) A! t( )
S
= ! t0( )U
†AU ! t
0( )S
= ! A t( )!H
(2.69)
where the operator is defined as
AH
t( ) =U†
t,t0( ) A
SU t,t
0( )A
Ht0( ) = A
S
(2.70)
2-19
Also, since the wavefunction should be time-independent ! "
H!t = 0 , we can relate the
Schrödinger and Heisenberg wavefunctions as
!
St( ) =U t,t
0( ) !H
(2.71)
So, !
H=U
†t,t
0( ) !S
t( ) = !S
t0( ) (2.72)
In either picture the eigenvalues are preserved:
A !i S
= ai!
i S
U†AUU
† !i S
= aiU
† !i S
AH!
i H= a
i!
i H
(2.73)
The time-evolution of the operators in the Heisenberg picture is:
!AH
!t=
!!t
U†A
SU( ) =
!U†
!tA
SU +U
†A
S
!U
!t+U
†!A
S
!tU
=i
!U
†H A
SU "
i
!U
†A
SH U +
!A
!t
#
$%&
'(H
=i
!H
HA
H"
i
!A
HH
H
="i
!A, H)* +,H
(2.74)
The result: i!
!
!tA
H= A, H"#
$%H
(2.75)
is known as the Heisenberg equation of motion. Here I have written H
H=U
†H U . Generally
speaking, for a time-independent Hamiltonian U = e
! iHt /! , U and H commute, and H
H= H . For
a time-dependent Hamiltonian, U and H need not commute.
Particle in a potential
2-20
Often we want to describe the equations of motion for particles with an arbitrary potential:
H =
p2
2m+V (x) (2.76)
For which the Heisenberg equation gives:
!p = !
"V
"x. (2.77)
!x =
p
m (2.78)
Here, I’ve made use of
xn, p!
"#$ = i!nx
n%1 (2.79)
x, pn!
"#$ = i!np
n%1 (2.80)
These equations indicate that the position and momentum operators follow equations of motion
identical to the classical variables in Hamilton’s equations. These do not involve factors of ! .
Note here that if we integrate eq. (2.78) over a time period t we find:
x t( ) =p t
m+ x 0( ) (2.81)
implying that the expectation value for the position of the particle follows the classical motion.
These equations also hold for the expectation values for the position and momentum operators
(Ehrenfest’s Theorem) and indicate the nature of the classical correspondence. In correspondence
to Newton’s equation, we see
m!
2x
!t2
= " #V (2.82)
2-21
THE INTERACTION PICTURE
The interaction picture is a hybrid representation that is useful in solving problems with time-
dependent Hamiltonians in which we can partition the Hamiltonian as
H t( ) = H
0+V t( ) (2.83)
H0
is a Hamiltonian for the degrees of freedom we are interested in, which we treat exactly, and
can be (although for us generally won’t be) a function of time. V t( ) is a time-dependent potential
which can be complicated. In the interaction picture we will treat each part of the Hamiltonian in
a different representation. We will use the eigenstates of H0
as a basis set to describe the
dynamics induced byV t( ) , assuming that V t( ) is small enough that eigenstates of H0
are a
useful basis to describe H. If H0
is not a function of time, then there is simple time-dependence
to this part of the Hamiltonian, that we may be able to account for easily.
Setting V to zero, we can see that the time evolution of the exact part of the Hamiltonian
H0
is described by
!
!tU
0t,t
0( ) ="i
!H
0t( )U0
t,t0( ) (2.84)
where, most generally,
U0
t,t0( ) = exp
+
i
!d! H
0t( )
t0
t
"#
$%
&
'( (2.85)
but for a time-independentH0
U
0t,t
0( ) = e! iH
0t! t
0( ) ! (2.86)
We define a wavefunction in the interaction picture !
I through:
!
St( ) "U
0t,t
0( ) !I
t( ) (2.87)
or !
I=U
0
† !S
(2.88)
Effectively the interaction representation defines wavefunctions in such a way that the phase
accumulated under e! iH
0t ! is removed. For small V, these are typically high frequency
oscillations relative to the slower amplitude changes in coherences induced by V.
2-22
We are after an equation of motion that describes the time-evolution of the interaction
picture wave-functions. We begin by substituting eq. (2.87) into the TDSE:
i!!
!t"
S= H "
S (2.89)
!
!tU
0t,t
0( ) "I=#i
!H t( )U
0t,t
0( ) "I
!U0
!t"
I+U
0
! "I
!t=#i
!H
0+V t( )( )U
0t,t
0`( ) "I
#i
!H
0U
0"
I+U
0
! "I
!t=#i
!H
0+V t( )( )U
0"
I
(2.90)
! i!" #
I
"t=V
I#
I (2.91)
where V
It( ) =U
0
†t,t
0( )V t( ) U0
t,t0( ) (2.92)
!
Isatisfies the Schrödinger equation with a new Hamiltonian: the interaction picture
Hamiltonian, V
It( ) , which is the U
0 unitary transformation ofV t( ) . Note: Matrix elements in
V
I= k V
Il = e
! i"lk
tV
kl where k and l are eigenstates of H0.
We can now define a time-evolution operator in the interaction picture:
!
It( ) =U
It,t
0( ) !I
t0( ) (2.93)
where
UI
t,t0( ) = exp
+
!i
!d"
t0
t
# VI"( )
$
%&
'
() . (2.94)
Now we see that
!S
t( ) =U0
t,t0( ) !
It( )
=U0
t,t0( )U
It,t
0( ) !I
t0( )
=U0
t,t0( )U
It,t
0( ) !S
t0( )
(2.95)
2-23
! U t,t
0( ) =U0
t,t0( )U
It,t
0( ) (2.96)
Using the time ordered exponential in eq. (2.94), U can be written as
U t,t0( ) =U
0t,t
0( ) +
!i
!
"#$
%&'n=1
(
)n
d*n
d*n!1
… d*1U
0t,*
n( )V *
n( )U0
*n,*
n!1( )…t0
*2+
t0
*n+
t0
t
+U
0*
2,*
1( )V *1( )U0
*1,t
0( )
(2.97)
where we have used the composition property ofU t,t0( ) . The same positive time-ordering
applies. Note that the interactions V(τi) are not in the interaction representation here. Rather we
used the definition in eq. (2.92) and collected terms.
For transitions between two eigenstates of H0 ( l and k):
The system evolves in eigenstates of H0 during the different
time periods, with the time-dependent interactions V driving the
transitions between these states. The time-ordered exponential
accounts for all possible intermediate pathways.
Also, the time evolution of conjugate wavefunction in
the interaction picture is expressed as
U†
t,t0( ) =U
I
†t,t
0( )U0
†t,t
0( ) = exp!
+i
!d"
t0
t
# VI"( )
$
%&
'
() exp
!
+i
!d"
t0
t
# H0"( )
$
%&
'
() (2.98)
or U
0
†= e
iH t! t0( ) ! when
H
0 is independent of time.
The expectation value of an operator is:
A t( ) = ! t( ) A! t( )
= ! t0( )U
†t,t
0( ) AU t,t0( )! t
0( )
= ! t0( )U
I
†U
0
†AU
0U
I! t
0( )
= !I
t( ) AI!
It( )
(2.99)
2-24
where A
I!U
0
†A
SU
0 (2.100)
Differentiating AI gives:
!
!tA
I=
i
!H
0, A
I"#
$% (2.101)
also,
!
!t"
I=#i
!V
It( ) "
I (2.102)
Notice that the interaction representation is a partition between the Schrödinger and Heisenberg
representations. Wavefunctions evolve under V
I, while operators evolve under H0.
For H0= 0,V t( ) = H !
"A
"t= 0;
""t
#S
=$i
!H #
SSchrödinger
For H0= H ,V t( ) = 0 !
"A
"t=
i
!H , A%& '(;
"#"t
= 0 Heisenberg
(2.103)
2-25
The relationship between UI(t,t0) and bn(t)
For problems in which we partition a time-dependent Hamiltonian,
H = H
0+V t( ) (2.104)
H0
is the time-independent exact zero-order Hamiltonian and V t( ) is a time-dependent
potential. We know the eigenkets and eigenvalues ofH0
:
H
0n = E
nn (2.105)
and we can describe the state of the system as a superposition of these eigenstates:
! t( ) = cn
t( ) n
n
" (2.106)
The expansion coefficients ckt( ) are given by
c
kt( ) = k ! t( ) = k U t,t
0( )! t0( ) (2.107)
Alternatively we can express the expansion coefficients in terms of the interaction picture
wavefunctions
b
kt( ) = k !
It( ) = k U
I! t
0( ) (2.108)
(This notation follows Cohen-Tannoudji.) Notice
ck
t( ) = k U0U
I! t
0( )
= e" i#
kt
k UI! t
0( )
= e" i#
kt
bk
t( )
(2.109)
This is the same identity we used earlier to derive the coupled differential equations that describe
the change in the time-evolving amplitude of the eigenstates:
i!!b
k
!t= V
knt( ) e
" i#nk
tb
nt( )
n
$ (2.110)
So, b
k is the expansion coefficient of the interaction picture wavefunctions. Remember
b
kt( )
2
= ck
t( )2
and b
k0( ) = c
k0( ) . If necessary we can calculate
b
kt( ) and then add in the
extra oscillatory term at the end.
2-26
2.4 PERTURBATION THEORY
Given a Hamiltonian H t( ) = H
0+V t( ) where we know the eigenkets for
H
0: H
0n = E
nn , we
can calculate the evolution of the wavefunction that results from V t( ) :
!I
t( ) = bn
t( ) n
n
" (2.111)
• using the coupled differential equations for the amplitudes of n . For a complex time-
dependence or a system with many states to be considered, solving these equations isn’t
practical. Alternatively, we can choose to work directly with U
It,t
0( ) , calculate b
kt( ) as:
b
k= k U
It,t
0( )! t0( ) (2.112)
where
UI
t,t0( ) = exp
+
!i
!V
I"( )d"
t0
t
#$
%&
'
() (2.113)
Now we can truncate the expansion after a few terms. This is perturbation theory, where the
dynamics under H0
are treated exactly, but the influence of V t( ) on b
n is truncated. This
works well for small changes in amplitude of the quantum states with small coupling matrix
elements relative to the energy splittings involved ( b
kt( ) ! b
k0( ) ; V ! E
k" E
n) As we’ll see,
the results we obtain from perturbation theory are widely used for spectroscopy, condensed
phase dynamics, and relaxation.
Transition Probability
Let’s take the specific case where we have a system prepared in ! , and we want to know the
probability of observing the system in k at time t , due to
V t( ) .
P
kt( ) = b
kt( )
2
bk
t( ) = k UI
t,t0( ) ! (2.114)
Andrei Tokmakoff, MIT Department of Chemistry, 3/14/2007
2-27
bk
t( ) = k exp+!
i
!d"
t0
t
# VI"( )
$
%&
'
() " (2.115)
bk
t( ) = k ! !i
"d"
t0
t
# k VI"( ) !
+!i
"
$%&
'()
2
d"2
d"1
t0
"2#
t0
t
# k VI"
2( )V
I"
1( ) ! +…
(2.116)
using
k VI
t( ) ! = k U0
† V t( )U0! = e! i"
!k tV
k!t( ) (2.117)
So,
bk
t( ) = !k!"
i
"d#
1e" i$
!k#
1Vk!
#1
( )t0
t
% “first order” (2.118)
+!i
!
"#$
%&'
2
m
( d)2
d)1e! i*
mk)
2 Vkm
)2
( ) e! i*
"m)
1
t0
)2+
t0
t
+ Vm"
)1
( ) +… (2.119)
“second order”
The first-order term allows only direct transitions between ! and
k , as allowed by the matrix
element in V, whereas the second-order term accounts for transitions occuring through all
possible intermediate states m . For perturbation theory, the time ordered integral is truncated at
the appropriate order. Including only the first integral is first-order perturbation theory. The
order of perturbation theory that one would extend a calculation should be evaluated initially by
which allowed pathways between ! and
k you need to account for and which ones are
allowed by the matrix elements.
For first order perturbation theory, the expression in eq. (2.118) is the solution to the
differential equation that you get for direct coupling between ! and
k :
!
!tb
k="i
!e" i#
"ktV
k"t( ) b
"0( ) (2.120)
2-28
This indicates that the solution doesn’t allow for the feedback between ! and
k that accounts
for changing populations. This is the reason we say that validity dictates b
kt( ) ! b
k0( ) .
If !
0 is not an eigenstate, we only need to express it as a superposition of eigenstates,
!0= b
n0( ) n
n
" and
bk
t( ) = bn
0( ) k UI
n
n
! . (2.121)
Now there may be interference effects between the pathways initiating from different states:
Pk
t( ) = ck
t( )2
= bk
t( )2
= k bn
t( ) n
n
!2
(2.122)
Also note that if the system is initially prepared in a state ! , and a time-dependent
perturbation is turned on and then turned off over the time interval t = !" to+! , then the
complex amplitude in the target state k is just the Fourier transform of V(t) evaluated at the
energy gap !!k
.
bk
t( ) = !i
!d" e
! i#"k"V
k""( )
!$
+$
% (2.123)
If the Fourier transform is defined as
!V !( ) " !F V t( )#$
%& =
1
2'dt V
()
+)
* t( )exp i!t( ) , (2.124)
then P
k!= "V !
k!( )
2
. (2.125)
2-29
Example: First-order Perturbation Theory
Vibrational excitation on compression of harmonic oscillator. Let’s subject a harmonic oscillator
to a Gaussian compression pulse, which increases its force constant.
First write the Hamiltonian:
H t( ) = T +V t( ) =
p2
2m+
1
2k t( )x2 (2.126)
Now partition it according to H = H
0+V t( ) :
k t( ) = k
0+ !k t( )
k
0= m!
2
!k t( ) = !k0exp "
t " t0( )
2
2# 2
$
%&&
'
())
(2.127)
H =p2
2m+
1
2k
0x2
H0
! "## $##
+1
2!k
0x2 exp "
t " t0( )
2
2# 2
$
%&&
'
())
V (t)! "#### $####
(2.128)
H
0n = E
nn
H0= !! a
†a +
1
2
"#$
%&'
En= !! n +
1
2
"#$
%&'
(2.129)
2-30
If the system is in 0 at
t0= !" , what is the probability of finding it in
n at t = ! ?
For n ! 0 :
bn
t( ) =!i
2!d" V
n0"( )
t0
t
# ei$
n0" (2.130)
Using !
n0= E
n" E
0( ) ! = n# :
bn
t( ) =!i
2!"k
0n x
20 d#
!$
+$
% ein&#
e!# 2
2' 2
(2.131)
So,
bn
t( ) =!i
2!"k
02#$ n x
20 e
!n2$ 2%2 /2 (2.132)
Here we used:
What about the matrix element?
x
2=!
2m!a + a
†( )2
=!
2m!aa + a
†a + aa
†+ a
†a
†( ) (2.133)
First-order perturbation theory won’t allow transitions ton = 1 , only n = 0 andn = 2 .
Generally this wouldn’t be realistic, because you would certainly expect excitation to v=1
would dominate over excitation to v=2. A real system would also be anharmonic, in which case,
the leading term in the expansion of the potential V(x), that is linear in x, would not vanish as it
does for a harmonic oscillator, and this would lead to matrix elements that raise and lower the
excitation by one quantum.
However for the present case,
2 x2
0 = 2!
2m! (2.134)
So,
b2=!i " #k
0$
2m%e!2$ 2%2
(2.135)
2-31
and
P2= b
2
2
=!"k
0
2# 2
2m2$2
e%4# 2$2
= # 2$2!2
"k0
2
k0
2
&
'(
)
*+ e
%4# 2$2
(2.136)
From the exponential argument, significant transfer of amplitude occurs when the compression
pulse is short compared to the vibrational period.
! <<1
" (2.137)
Validity: First order perturbation theory doesn’t allow for bn to change much from its initial
value. For P
2<< 1
! 2"2#2
$k0
2
k0
2
%
&'
(
)* << 1 (2.138)
Generally, the perturbation δk(t) must be small compared to k0, i.e. H
0>> V , but it should also
work well for the impulsive shock limit (σΩ<<1).
2-32
FIRST-ORDER PERTURBATION THEORY
A number of important relationships in quantum mechanics that describe rate processes come
from 1st order perturbation theory. For that, there are a couple of model problems that we want
to work through:
Constant Perturbation (Step-Function Perturbation)
! "#( ) = ! . A constant perturbation of amplitude V is applied to
t0. What is
P
k?
V t( ) = ! t " t0
( )V
=0 t < 0
V t # 0
$%&
To first order, we have:
k U0
†V U
0! =V e
i!k!
t" t0( )
bk= !
k!"
i
"d#
t0
t
$ ei%
k!# "t
0( )V
k!#( ) (2.139)
Here Vk!
is independent of time. Now, assuming k ! ! and setting t0 = 0 we have
bk= !
i
!V
k"d"
0
t
# ei$
k"" (2.140)
= !V
k!
Ek! E
!
exp i"k!
t( ) !1#$
%& (2.141)
= !2iV
k!e
i"k!
t / 2
Ek! E
!
sin "k!
t / 2( ) (2.142)
Where I used e
i!"1= 2i e
i! 2sin ! 2( ) . Now
2-33
Pk= b
k
2
=4 V
k!
2
Ek! E
!
2sin
2 1
2"
k!t (2.143)
Writing this as we did in Lecture 1:
Pk=
V2
!2
sin2!t / !( ) (2.144)
where ! = E
k" E
!( ) 2 . Compare this with the exact result we have for the two-level problem:
Pk=
V2
V2+ !
2sin
2!
2+V
2t / !( ) (2.145)
Clearly the perturbation theory result works for V << Δ.
We can also write the first-order result as
Pk=
V2t
2
!2
sinc2!t / 2!( ) (2.146)
where sinc x( ) = sin x( ) x . Since
limx!0
sinc x( ) = 1,
lim!"0
Pk=V
2t
2!
2 (2.147)
The probability of transfer from ! to
k as a function of the energy level splitting
E
k! E
!( ) :
Since the energy spread of states to which transfer is efficient scales approximately
as E
k! E
!< 2"" t , this observation is sometimes referred to as an uncertainty relation
Area scales linearly with time.
2-34
with !E " !t # 2$! . However, remember that this is really just an observation of the principles
of Fourier transforms, that frequency can only be determined by the length of the time period
over which you observe oscillations. Since time is not an operator, it is not a true uncertainly
relation like !p " !x # 2$! .
Now turning to the time-dependence:
The quadratic growth for Δ=0 is certainly unrealistic (at least for long times), but the expression
shouldn’t hold for what is a “strong coupling” case Δ=0. However, let’s continue looking at this
behavior. In the long time limit, the sinc2(x) function narrows rapidly with time giving a delta
function:
limt!"
sin2
ax 2( )ax
2=#
2$ x( ) (2.148)
limt!"
Pk
t( ) =2# V
k!
2
"$ E
k% E
!( ) t (2.149)
The delta function enforces energy conservation, saying that the energies of the initial and target
state must be the same in the long time limit.
What is interesting in eq. (2.149) is that we see a probability growing linearly in time.
This suggests a transfer rate that is independent of time, as expected for simple first order
kinetics:
2-35
wk
t( ) =!P
kt( )
!t=
2" Vk!
2
"# E
k$ E
!( ) (2.150)
This is one statement of Fermi’s Golden Rule −the state-to-state form− which describes
relaxation rates from first order perturbation theory. We will show that this rate properly
describes long time exponential relaxation rates that you would expect from the solution
to dP dt = !wP .
2-36
Slowly Applied (Adiabatic) Perturbation
Our perturbation was applied suddenly at t > t0 (step function)
V t( ) = ! t " t
0( )V t( )
This leads to unphysical consequences—you generally can’t turn on a perturbation fast enough
to appear instantaneous. Since first-order P.T. says that the transition amplitude is related to the
Fourier Transform of the perturbation, this leads to additional Fourier components in the spectral
dependence of the perturbation—even for a monochromatic perturbation!
So, let’s apply a perturbation slowly . . .
V t( ) =V e
!t
here η is a small positive number. !"1 is the
effective turn-on time of the perturbation.
The system is prepared in state ! at t = !" . FindP
kt( ) .
bk= k U
I! =
!i
"d" e
i#k!"
!$
t
% k V ! e&"
bk=!iV
k!
"
exp &t + i#k!
t'( )*& + i#
k!
=Vk!
exp &t + i Ek! E
!( )t / "'( )*
Ek! E
!+ i&"
Pk= b
k
2
=V
k!
2
"2
exp 2&t'( )*&2
+#k!
2=
Vk!
2
exp 2&t'( )*
Ek! E
!( )
2
+ &"( )2
This is a Lorentzian lineshape in !
k! with width
2!! .
2-37
Gradually Applied Perturbation Step Response Perturbation
The gradually turned on perturbation has a width dependent on the turn-on rate, and is
independent of time. (The amplitude grows exponentially in time.) Notice, there are no nodes
inPk.
Now, let’s calculate the transition rate:
wkl=!P
k
!t=
Vk!
2
"2
2"e2"t
"2+#
k!
2
Look at the adiabatic limit; !"0 . Setting e2!t
" 1 and using
lim
!" 0
!
!2+#
k!
2= $% #
k!( )
wk!=
2!
"2
Vk!
2
" #k!
( ) =2!
"V
k!
2
" Ek$ E
!( )
We get Fermi’s Golden Rule—independent of how perturbation is introduced!
2-38
Harmonic Perturbation
Interaction of a system with an oscillating perturbation
turned on at time t0= 0 . This describes how a light
field (monochromatic) induces transitions in a system
through dipole interactions. Again, we are looking to
calculate the transition probability between states !
and k:
V t( ) =V cos!t = "µE
0cos!t (2.151)
Vk!
t( ) =Vk!
cos!t
=V
k!
2e
i! t+ e
" i! t#$
%&
(2.152)
To first order, we have:
bk= k !
It( ) =
"i
!d#
t0
t
$ Vk"
#( ) ei%
k"#
="iV
k"
2!d#
0
t
$ ei %
k"+%( )# " e
i %k""%( )#&
'()
="V
k"
2!
ei %
k"+%( )t "1
%k"+%
+e
i %k""%( )t "1
%k""%
&
'**
(
)++
setting t0! 0 (2.153)
Now, using e
i!"1= 2i e
i! 2sin ! 2( ) as before:
bk=!iV
k!
"
ei "
k!!"( )t / 2
sin "k!!"( )t / 2#
$%&
"k!!"
+e
i "k!+"( )t / 2
sin "k!+"( )t / 2#
$%&
"k!+"
#
$
''
%
&
((
(2.154)
Notice that these terms are only significant when ! "!
k!. As we learned before, resonance is
required to gain significant transfer of amplitude.
2-39
First Term Second Term
max at : ! = +!
k!
! = "!
k!
Ek> E
!
Ek< E
!
Ek= E
!+ "!
Ek= E
!! ""
Absorption Stimulated Emission
(resonant term) (anti-resonant term)
For the case where only absorption contributes, Ek> E
!, we have:
Pk!= b
k
2
=V
k!
2
"2 !
k!"!( )
2sin
2 1
2!
k!"!( )t#
$%&
orE
0
2 µk!
2
" !k!"!( )
2sin
2 1
2!
k!"!( )t#
$%&
(2.155)
We can compare this with the exact expression:
Pk!= b
k
2
=V
k!
2
"2 !
k!"!( )
2
+ Vk!
2sin
21
2"V
k!
2
+ !k!"!( )
2
t#
$%
&
'( (2.156)
which points out that this is valid for couplings V
k! that are small relative to the
detuning !" = "
k!#"( ) . The maximum probability for transfer is on resonance
!
k!=!
2-40
Limitations of this formula:
By expanding
sin x = x !x3
3!+… , we see that on resonance
!" ="
k!# " $ 0
lim
!" # 0P
kt( ) =
Vk!
2
4"2
t2 (2.157)
This clearly will not describe long-time behavior. This is a result of 1st order perturbation theory
not treating the depletion of ! . However, it will hold for smallP
k, so we require
t <<2!
Vk"
(2.158)
At the same time, we can’t observe the system on too short a time scale. We need the field to
make several oscillations for it to be a harmonic perturbation.
t >1
!"
1
!k!
(2.159)
These relationships imply that
V
k!<< "!
k!(2.160)
2-41
Adiabatic Harmonic Perturbation
What happens if we slowly turn on the harmonic interaction?
V t( ) =V e!t
cos"t
bk=#i
!d$
#%
t
& Vk"
ei"
k"$ +!$ e
i"$ + e# i"$
2
'
()
*
+,
=V
k"
2!e!t
ei "
k"+"( )t
# "k"+"( )+ i!
+e
i "k"#"( )t
# "k"#"( ) + i!
'
())
*
+,,
Again, we have a resonant and anti-resonant term, which are now broadened by! . If we only
consider absorption:
Pk= b
k
2
=V
k!
2
4"2
e2!t
1
"k!#"( )
2
+ !2
which is the Lorentzian lineshape centered at !
k!=! with width!" = 2# . Again, we can
calculate the adiabatic limit, setting!" 0 . We will calculate the rate of
transitions !
k!= "P
k/ "t . But let’s restrict ourselves to long enough times that the harmonic
perturbation has cycled a few times (this allows us to neglect cross terms) ! resonances sharpen.
wk!=
!
2"2
Vk!
2
" #k!$#( ) + " #
k!+#( )%
&'(
2-42
2.5 FERMI’S GOLDEN RULE
The transition rate and probability of observing the system in a state k after applying a
perturbation to ! from the constant first-order perturbation doesn’t allow for the feedback
between quantum states, so it turns out to be most useful in cases where we are interested just the
rate of leaving a state. This question shows up commonly when we calculate the transition
probability not to an individual eigenstate, but a distribution of eigenstates. Often the set of
eigenstates form a continuum of accepting states, for instance, vibrational relaxation or
ionization.
Transfer to a set of continuum (or bath) states forms the basis for a describing irreversible
relaxation. You can think of the material Hamiltonian for our problem being partitioned into two
portions, H = H
S+ H
B+V
SBt( ) , where you are interested in the loss of amplitude in the
H
S
states as it leaks into H
B. Qualitatively, you expect deterministic, oscillatory feedback between
discrete quantum states. However, the amplitude of one discrete state coupled to a continuum
will decay due to destructive interferences between the oscillating frequencies for each member
of the continuum.
So, using the same ideas as before, let’s calculate the transition probability from ! to a
distribution of final states: P
k.
P
k= b
k
2
Probability of observing amplitude in discrete eigenstate of H
0
! E
k( ) : Density of states—units in
1 E
k, describes distribution of final
states—all eigenstates of H
0
If we start in a state ! , the total transition probability is a sum of probabilities
Pk= P
k
k
! . (2.161)
We are just interested in the rate of leaving ! and occupying any state
k or for a continuous
distribution:
Andrei Tokmakoff, MIT Department of Chemistry, 3/1/2007
2-43
Pk = dE
k! E
k( ) P
k" (2.162)
For a constant perturbation:
Pk = dEk! E
k( ) 4 V
k!
2 sin2
Ek" E
!( )t / 2"( )
Ek" E
!
2# (2.163)
Now, let’s make two assumptions to evaluate this expression:
1) ! E
k( ) varies slowly with frequency and there is a
continuum of final states. (By slow what we are saying is that the observation point t is relatively long).
2) The matrix element
V
k! is invariant across the final
states.
These assumptions allow those variables to be factored out of integral
Pk= ! V
k!
2
dEk
4sin
2E
k" E
!( )t / 2"
Ek" E
!( )
2"#
+#
$ (2.164)
Here, we have chosen the limits !"# + " since ! E
k( ) is broad relative to
P
k. Using the
identity
d!"#
+#
$sin
2a!
!2= a% (2.165)
with a = t / ! we have
Pk=
2!
!" V
k"
2
t (2.166)
The total transition probability is linearly proportional to time. For relaxation processes, we will
be concerned with the transition rate, w
k!:
2-44
wk!=!Pk!
!t
wk!=
2"
"# V
k!
2
(2.167)
Remember that P
k is centered sharply at
E
k= E
!. So although ρ is a constant, we usually write
eq. (2.167) in terms of ! E
k= E
!( ) or more commonly in terms of
! E
k" E
!( ) :
wk!=
2!
"" E
k= E
!( ) V
k!
2
(2.168)
wk!=
2!
"V
k!
2
" Ek# E
!( )
w
k!= dE
k! E
k( ) w
k!" (2.169)
This expression is known as Fermi’s Golden Rule. Note the rates are independent of time. As
we will see going forward, this first-order perturbation theory expression involving the matrix
element squared and the density of states is very common in the calculation of chemical rate
processes.
Range of validity
For discrete states we saw that the first order expression held for V
k!<< "!
k!, and for
times such that P
k never varies from initial values.
P
k= w
k!t ! t
0( )
t <<1
wk!
(2.170)
However, transition probability must also be sharp compared to ! E
k( ) , which implies
t >> ! / !E
k (2.171)
So, this expression is useful where
2-45
!E >> wk!"
!"k>> w
k!
. (2.172)
Andrei Tokmakoff, MIT Department of Chemistry, 2/22/2007