The Effect of Angular Distributions on Anisotropy Measurements

Bernhard Lang

Department of Physical Chemistry, University of Geneva,
30, quai Ernest Ansermet, CH-1211 Geneva 4, Switzerland
bernhard.lang@unige.ch
Version 1.03,
14th February 2008

Abstract

The fluorescence anisotropy is calculated for a system in which the angle between absorption and emission dipole is not fixed but is given by a distribution around a central value and may have an additional degree of freedom in form of a rotation on an axis perpendicular to the excitation dipole. First, a so-called parallel transition is considered, where the two dipoles have the same direction. Then, the general expression for a fixed, non-zero angle is derived. Finally, an integration over a range of values yields the desired result. 1

Introduction

The anisotropy to be expected from a molecule where excitation and emission (or probe-) dipole are not parallel can be calculated by the well-known formula

        2
R = 3-cosα-−-1
         5
(1)

where α is the angle between the two dipoles. In a situation where these dipoles are localised on two different moieties of a molecule or complex which are not rigidly linked, this formula cannot be used any more. To extend it to such a scenario we’ll first derive the above formula and insert afterwards the additional degree of freedom at the appropriate step.

1 Emission from a Parallel Transition

Let us first consider a molecule with a so-called parallel transition, i.e. an excitation-emission cycle in which the transition dipoles for excitation and emission are parallel to each other. These dipoles shall be characterised by their moduli μ21 and μ32 and the two angles ϕ and ψ, where ϕ describes the angle between the dipole and the z-axis, whereas ψ denotes the angle between the projection of the dipole onto the x-y plane and the x-axis (c.f. figure 1).


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Figure 1: Transition dipole moment ⃗μ21 in lab coordinate system.

We chose the excitation source to be polarised parallel to the z-axis. The emission from the dipole ⃗μ32 is detected along the x-axis, using polarisations in two directions, parallel to the z-axis and parallel to the y-axis, respectively. The probability of detecting a photon in one of the two directions when exciting a molecule oriented in space according to ϕ and ψ is proportional to the product of the probability of exciting the molecule, the probability of detecting a photon emitted by an excited molecule and by the detection efficiency. The constant of proportionality is determined by the absorption cross section and the quantum efficiency of the photo cycle in the molecule, and by the solid angle of detection. The z- and y-components of the electric field emitted by an excited molecule at angles ϕ and ψ are given by

Ez(ϕ,ψ) = Ez(ϕ) = E cosϕ (2)
Ey(ϕ,ψ) = E sinϕsinψ. (3)
Accordingly, the probabilities of detecting a photon with the corresponding polarisation are
Pdet,z(ϕ) Iz(ϕ) = E02 cos2ϕ (4)
Pdet,y(ϕ,ψ) Iy(ϕ,ψ) = E02 sin2ϕcos2ψ, (5)
being the projections of the the total “intensity-vector” onto the z- and y-axis, respectively. Similarly, the probability of exciting a molecule with dipole ⃗μ21 oriented according to ϕ and ψ is given by
Pex(ϕ,ψ) = Pex(ϕ) ∝ cos2ϕ.
(6)

The total probability to detect a photon coming from a single molecule and being polarised parallel to the z- or y-axis is therefore the product of the corresponding probabilities

Pz(ϕ) = Pex(ϕ)Pdet,z(ϕ) cos4ϕ (7)
Py(ϕ,ψ) = Pex(ϕ)Pdet,y(ϕ,ψ) cos2ϕsin2ϕcos2ψ. (8)
The overall probability is therefore given by the average over all molecules in the sample, i.e. a homogeneous distribution of absorption-emission dipoles. The number of molecules dn to be found in the solid angle [ϕ,ϕ + dϕ] × [ψ,ψ + dψ] is proportional to
dn = sin ϕdϕdψ.
(9)

The origin of the factor sinϕ can be explained as follows. Integrating dϕdψ over ψ from 0 to 2π at ϕ close to 90  yields a much larger value than at ϕ close to zero. The values of these integrals are represented by the corresponding part of the surface of a sphere. A stripe around the equator of with Δϕ will have a much larger surface than a one close to the pole of the same width. The ratio between the surfaces is given by sinϕ. We have therefore

Pz = 02π 0π∕2P z(ϕ)sinϕdϕdψ (10)
2π 0π∕2 cos4ϕsinϕdϕ (11)
= 2π1   5  ||
5 cos ϕ||0π∕2 (12)
= 2π
---
 5, (13)
where we made use of
 α∫1                             |α
   cosn αsinαdα = − --1--cos(n+1)α|| 1.
                   n + 1        |α0
α0
(14)

The probability of detecting a photon polarised in y-direction is similarly given by

Py = 02π 0π∕2P y(ϕ,ψ)sinϕdϕdψ (15)
02π 0π∕2 cos2ϕsin2ϕcos2ψdϕdψ (16)
= π 0π∕2 cos2ϕ(        )
 1 − cos2ϕsinϕdϕ (17)
= π[               ]
 1cos3ϕ − 1cos5ϕ
 3        50π∕2 = 2-
15π. (18)
For the anisotropy of the detected light we have thus
R∥ = Pz-−-Py-= 1∕5-−-1∕15 = 2
     Pz + 2Py  1∕5 + 2∕15   5
(19)

since the constants of proportionality do not depend on the polarisation and are, therefore, the same for parallel and perpendicular detection.

2 Emission from a Non-Parallel Transition

2.1 Euler’s Method

We assume now that the two transition dipoles ⃗μ21 and ⃗μ32 are separated by an angle α. The problem becomes a little more complicated as we also have to take into account now the orientation of the plane spanned by ⃗μ21 and ⃗μ32. In other words, given a certain orientation of ⃗μ21 as in the previous section and fixing α, we may still rotate the molecule around ⃗μ21. Excitation source and emission detection are fixed within the lab coordinate system {ˆni} = {ˆx,ŷ,} = {ˆn1,ˆn2,ˆn3}, whereas the orientation of the transition dipoles is more easily described in a molecule-internal coordinate system {êi} = {ê1,ê2,ê3}. The idea of the calculation is similar to the parallel transition, however, we first have to express the molecule-internal coordinate system in terms of the laboratory coordinate system. In general, the transformation of a rectangular and right handed coordinate system into another can be performed by two rotations. However, as the two corresponding axes are in general not parallel to one of the axes of the coordinate systems, a calculation using these two rotations is rather complicated. Euler’s method simplifies the description at the cost of introducing an additional rotational transformation.


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Figure 2: Transformation of two rectangular and right handed coordinate systems using Euler’s method.

Figure 2 illustrates the threefold angular transformation. The two circles indicate the planes spanned by ˆn1 and ˆn2, and by ê1 and ê2, respectively. In a first step, the laboratory system {ˆni} is rotated around the ˆn3 axis by an angle ϕ such that the new vector ˆn1 is identical with the intersection line of the two circles. We have nˆ3 = ˆn3, and the ˆn1-ˆn2 circle is conserved during this rotation. The second step consists of a rotation around the new vector ˆn1 by θ such that ˆn3′′ becomes equal to ê3. This rotation tilts also the ˆn1-ˆn2 plane into the ê1-ê2 plane. Finally, the obtained system is turned around ê3 = nˆ3′′ by ψ such that {ˆni′′′}≡{êi}.

Mathematically, the first step is described by the three following equations

ˆn1 = cosϕˆn 1 + sinϕˆn2 (20)
ˆn2 = sinϕˆn 1 + cosϕˆn2 (21)
ˆn3 = ˆn 3 (22)
or
(     )        (     )
   ˆn′1             ˆn1
(  ˆn′2 ) = R1(ϕ)(  ˆn2 )
   ˆn′3             ˆn3
(23)

with

        (  cosϕ   sin ϕ  0 )
R1 (ϕ ) = ( − sinϕ cosϕ  0 ) .
             0     0    1
(24)

Similarly we have

nˆ1′′ = ˆn 1 (25)
nˆ2′′ = cosθˆn 2 + sinθˆn 3 (26)
nˆ3′′ = sinθˆn 2 + cosθnˆ 3 (27)
or
       (  1    0      0  )
R2(θ) = ( 0   cosθ   sin θ )
          0  − sinθ  cosθ
(28)

and

ê1 = cosψˆn1′′ + sinψˆn 2′′ (29)
ê2 = sinψˆn1′′ + cosψˆn 2′′ (30)
ê3 = ˆn3′′ (31)
or
R3 (ψ) = R1 (ψ ).
(32)

Combining the rotations together we get

ˆei = R1 (ψ )R2(θ)R1 (ϕ)nˆi = D(ψ,θ,ϕ)ˆni.
(33)

The transformation matrix is given by the matrix multiplication of the three individual transformation matrices

D(ψ,θ,ϕ) = (34)
(                 )
   cosψ   sinψ  0
( − sinψ  cosψ  0 )
     0      0   1(                 )
   1    0      0
(  0   cosθ  sinθ )
   0  − sinθ  cosθ(                 )
    cosϕ   sinϕ  0
(  − sinϕ  cosϕ  0 )
     0      0   1
= (   cosψ   sinψ   0 )
(  − sinψ   cos ψ  0 )
     0      0    1(    cosϕ        sin ϕ      0   )
(  − cosθ sinϕ  cosθcosϕ   sin θ )
    sinθ sinϕ   − sin θcosϕ  cosθ (35)
= (                                                                 )
    cosψcosϕ − sinψ cosθsin ϕ    cosψ cosϕ+ sinψ cos θcosϕ  sinψ cosθ
(  − sinψ cosϕ − cosψ cosθsin ϕ − sinψ sinϕ + cosψcosθ cosϕ  cosψ sin θ )
            sinθ sinϕ                  − sin θcosϕ            cos θ. (36)
Using D(ψ,θ,ϕ) we can now express {êi} by {ˆni} as
     ∑3
ˆei =    djiˆnj
     j=1
(37)

with

dij(ψ,θ,ϕ) = [D(ψ,θ,ϕ)]ij.
(38)

Let us assume that ⃗μ21 is parallel to ê3

⃗μ21 = μ21ˆe3
(39)

and that ⃗μ32 lies in the plane spanned by ê1 and ê3

⃗μ32 = μ(1)ˆe1 + μ(3)ˆe3 = μ32sinαˆe1 +μ32cosα ˆe3
      32      32
(40)

where α denotes the angle between ⃗μ21 and ⃗μ32. This choice has been made such that using Euler’s transformation will not only yield an expression of the molecule’s orientation in the laboratory coordinate system, but will also yield a direct parametrisation of the most important angles. θ represents the angle between the z-axis (the direction of the polarisation of the excitation light) and the excitation dipole μ21. ψ indicates the rotation of the molecule around μ21, the added degree of freedom in the problem. And ϕ, finally, parametrises the rotation of μ21 around the z-axis.

Expressed in the laboratory coordinate system the excitation dipole reads

                 3
                ∑
⃗μ21 = μ21ˆe3 = μ21i=1 di3(ψ,θ,ϕ)ˆni.
(41)

The emission dipole moment is given by

         ∑3
⃗μ32 = μ32   [di1(ψ,θ,ϕ)sinα + di3(ψ,θ,ϕ)cosα]ˆni.
         i=1
(42)

The intensity of the emitted light with polarisation in z-direction is again the square of the projection of ⃗μ32 onto , i.e. the square of the z-component of (42)

Iz(ψ,θ,ϕ) = E02[d 31(ψ,θ,ϕ)sinα + d33(ψ,θ,ϕ)cosα]2 (43)
= E02(sinθ sinϕsinα + cosθ cosα)2 (44)
For a detection polarised parallel to the y-axis we get
Iy(ψ,θ,ϕ) = E02[d 21(ψ,θ,ϕ)sinα + d23(ψ,θ,ϕ)cosα]2 (45)
= E02[(sinψ cosϕ cosψ cosθ sinϕ)sinα + cosψ sinθ cosα]2. (46)
Incorporating the probability of absorption as a function of the molecule’s orientation we have to multiply (44) and (46) by cos2ϕ and get
Pz(ψ,θ,ϕ,α) cos2θ(sinθ sinϕsinα + cosθ cosα)2 (47)
Py(ψ,θ,ϕ,α) cos2θ[(sinψ cosϕ cosψ cosθ sinϕ)sinα + cosψ sinθ cosα]2. (48)
Similar to (10) we have now to integrate over all molecules in the sample, i.e. to integrate over all directions in space properly weighted
       ∫2π π∫∕2∫2π
Pz(α) ∝       cos2θsinθ(sinθ sinϕ sinα + cosθcosα)2dϕdθdψ.
       0  0 0
(49)

The integration over ψ yields a constant factor 2π, and due to the factor sinϕ, the cross term of the bracket vanishes when integrating over ϕ from 0 to 2π. We have therefore

           π∫∕2
P (α) = 2π2   (cos2θ sin3θsin2α+ 2 cos4θ sinθ cos2α) dθ.
 z
           0
(50)

Using sin2θ = 1 cos2θ we get

Pz(α) = 2π2 0π∕2 sinθ[    (              )           ]
cos4θ 2 cos2α − sin2α  + cos2θ sin2αdθ (51)
= 2π2[                                    ]
 1 (2cos2α− sin2α)cos5θ+ 1 sin2α cos3θ
 5                       30π∕2 (52)
= 4
5π2 cos2α + 4-
15π2 sin2α (53)
= 4-
15π2(2cos2α + 1). (54)
For the detection along the y axis we get
       ∫2ππ∫∕22∫π
Py(α) ∝        cos2θ sinθ [(− sinψ cosϕ− cosψ cosθsin ϕ)sinα + cosψ sinθcosα ]2dϕdθdψ.
        0 0  0
(55)

The integration over ϕ is again easily performed, as ϕ occurs only in the first term of the square bracket. Therefore, the cross terms vanish when integrating over ϕ from 0 to 2π. We have thus

Py(α) = π 02π 0π∕2 cos2θsinθ[sin2ψ sin2α + cos2 ψcos2θsin2α (56)
+                 ]
2cos2 ψsin2 θcos2 αdθdψ
= π2 0π∕2 cos2θsinθ(                              )
sin2α + cos2θ sin2α + 2sin2θ cos2αdθ (57)
= π2[                                                      ]
 − 1 sin2α cos3θ− 1 sin2α cos5θ − 2cos2α cos3θ + 2cos2α cos5θ
  3             5             3             50π∕2 (58)
= 4-
15π2(sin2α + 1). (59)
The final expression for the anisotropy is therefore
R(α) = Pz(α)−-Py(α)-= -2cos2α-+-1−-sin2α-−-1-=  3cos2-α−-1.
       Pz(α )+ 2Py(α)  2 cos2α + 1+ 2 sin2α + 2       5
(60)

For α = 0 we get again R = 0.4 as already found in (19) in the previous section. For a perpendicular transition, i.e. α = 90, we get R = 0.2. For a complete arbitrary orientation of the two dipoles—which should yield an isotropic signal—we have to integrate over α, taking into account that varying α is possible by turning ⃗μ32 in two independent directions within the molecule-internal coordinate system. This is reflected in an additional factor sinα (c.f. (9) and the subsequent phrase)

       π∫∕2                            |π∕2
R    =    3cos2α-− 1-sin αdα = cos3α−-1-|| = 0
  arb.         5                  5    |0
       0
(61)

as expected.

2.2 Plane-Perpendicular Transition

In some molecules the emission can occur from two degenerated states with transition dipoles perpendicular to each other. (60) can be used directly with α = 90 when the plane spanned by these two dipoles is perpendicular to the transition dipole which corresponds to the excitation. The integration over ψ in the above derivation, being there an average over all molecules in the sample, can also be interpreted as the integration over all possible emission directions within the same molecule. We get R = 0.2 in this case.

On the other hand, an integration over α from 0 to 90 will yield the anisotropy for the case where the plane spanned by the two emission dipoles contains the excitation dipole. However, performing the calculation of Pz and Py we do not need to care about normalisation due to averaging over solid angles as the normalisation is the same for both polarisations and will thus vanish when calculating R.

        π∕2              π∕2
        ∫            4  2∫  (    2    )      4  3
Pperp.z =   Pz(α)dα = 15π     2cos α+ 1 dα = 15 π
        0                0
(62)

and

        π∫∕2          4   π∫∕2(        )     3
Pperp.y =   Py (α )dα = 15π2    sin2α + 1 dα = 15π3
        0                0
(63)

We have thus

R ∥⊥ = 4-−-3= 0.1.
      4 + 6
(64)

3 Distribution of Directions

3.1 Distribution of the angle α

A distribution of directions wα can be introduced using (60)

            π∫∕23cos2α − 1
R (α0,wα)) =   ----------w(α)sinαdα.
             0     5
(65)

Figure 3 shows the anisotropy R of a distribution of angles around α for a couple of equidistant angles between zero an 90 . Note the logarithmic scale for the width of the Gaussian distribution.


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Figure 3: Anisotropy of a distribution of angles centered at different angles.

3.2 Additional degree of freedom between transition dipoles

Let us assume that the probed dipole is not rigidly attached to the excitation dipole but may freely rotate around an axis perpendicular to the excitation dipole. This situation could correspond to a weakly bound complex of two planar molecules in a sandwich-like geometry where the mutual orientation is random with respect to the normal direction of the “sandwich plane”. Let us start from the geometry where the angle between the dipoles is minimal and let us call this minimal angle α0. Turning the probe dipole around the vector which is perpendicular to ⃗μ12 and lies in the plane spawned by ⃗μ12 and ⃗μ23(0) generates the set of contributing molecules, where ⃗μ23(0) is the probe dipole which corresponds to the minimal angle α0. An integration over the turning angle δ yields the desired result. However, as (60) is not linear neither in Py(α) nor in Pz(α), we have to perform the integration in these two expressions using (51) and (56) and to calculate R(α0) by the usual expression.

From fig. 1 and using (40) we obtain

⃗μ23(γ) = μ23ˆe1 + μ323(sin γˆe2 + cosγˆe3).
(66)

The relation between α and γ is given by the scalar product

cosα(γ,α0) = ⃗μ12 ⋅⃗μ23(γ)-= cosα0cosγ
               μ12μ23
(67)

where we have used again (40). For the detection probability with polarisation parallel to the z-axis we obtain therefore using (51)

Pz(α0) = 0π∕2P z(α(γ,α0)) (68)
=  4
15π2 0π∕2{    2                    }
 2cos [arccos(cosα0 cosγ )]+ 1 (69)
=  4
--
15π2 0π∕2{                }
 2cos2α0cos2γ)+ 1 (70)
= -2
15π3(         )
 cos2α0 + 1. (71)
As upper integration limit π∕2 is sufficient as the direction of the transition dipole may be inverted without changing the underlying physics and, thus, the second quadrant does not yield new contributions. From (56) and using
  2             2
sin α + 1 = 2 − cos α
(72)

we get similarly for detection with polarisation parallel to the y-axis

Py(α0) = 0π∕2(              )
 2− cos2α0cos2γ (73)
= -2
15π3(           )
 2 − 1cos2α0
     2. (74)
We have thus
           2           1   2         2
R (α0 ) = cos-α0 +-1-− 2-+-2 cos-α0-= 3cos-α0-− 2-.
         cos2 α0 + 1+ 4 + cos2α0       10
(75)

Considering the two extreme cases α0 = 0 and α0 = π∕2 yields the known values of R = 0.1 and R = 0.2, respectively, as to be expected. In between, no new maximum is to be observed. In other words, in the situation described here, the maximum positive anisotropy to be obtained is R = 0.1.

A Anisotropy from multiple contributions

Assume that the detected signal is composed out of several different contributions which are of different absolute intensity and anisotropy. The anisotropy rn for the nth contribution as an isolated signal is given by the usual definition

     I  − I
rn = -∥n---⊥n-.
     I∥n + 2I⊥n
(76)

It is important to notice that the total anisotropy is not the sum or average of the individual anisotropies but the anisotropy of the sum of the signals

       ∑   (        )
rtotal = ∑-n(I∥,n −-I⊥,n-).
         n I∥,n +2I⊥,n
(77)

In consequence, the total anisotropy is a nonlinear quantity with respect to the individual contributions. Let us inspect how this total anisotropy looks like. We start from the usual definition of the anisotropy

r = I∥ −-I⊥-= I∥ −-I⊥
    I∥ + 2I⊥   3Im
(78)

with Im being the signal at magic angle

Im = (I∥ + 2I⊥)∕3
(79)

or equivalently

I∥ = 3Im − 2I⊥
(80)

and

I⊥ = 3Im − 1I∥.
     2     2
(81)

Inserting (80), respectively (81) into (78) we have

I∥ = Im(2r+ 1)
(82)

and

I⊥ = Im (1− r)
(83)

as can easily be verified by inserting (82) and (83) into (78). Inserting (82) and (83) into (77) we get

       -∑n-Imn[(2rn-+1)-− (1-− rn)] ∑n-Imnrn-
rtotal = ∑ Imn [(2rn + 1)+ 2(1− rn)] = ∑ Imn  .
         n                            n
(84)

The obtained formula resembles the one which determines the position of the center of masses in an ensemble of particles. Hence, for positive magic angle signals Im the total anisotropy lies always in between the anisotropy values of the individual contributions and closest to the anisotropy value of the contribution with the largest absolute signal at magic angle.

Special attention has to be payed in case of contributions which may have opposite signs as for instance data obtained from a transient absorption measurement in spectral regions with overlap of induced absorption and emission or bleach signals. When two contributions with opposite sign cancel each other, i.e. the corresponding magic angle signal crosses the zero line, the denominator of (84) vanishes and rtotal diverges. In the vicinity of such a zero-crossing point any value between −∞ and + can be obtained for rtotal depending on the detailed experimental conditions like signal-to-noise ratio and removal of background offset signals. But even without a zero-crossing nearly arbitrary values may be obtained for rtotal in case of two contributions with large anisotropy of the same sign but signal of opposite sign and similar amplitude. As soon as nImn n|Imn| one has to be prepared for “surprises”. In consequence, when trying to extract from the measured anisotropy the anisotropy of an individual contribution to the signal can be difficult. It is given by the expression

    (     ∑        ∑       )                  ∑
rn = (rtotal  Imk −    Imkrk) ∕Imn = rtotal +-1--   Imk(rtotal− rk).
           k       k⁄=n                    Imn k⁄=n
(85)

If all but one anisotropy values rk,rn and all intensities Imk have been determined, the missing rn can be calculated. To estimate the uncertainty in rn we need to calculate the derivations with respect to all parameters

-∂rn--
∂rtotal = 1 + (Itotal Imn)∕Imn = Itotal∕Imn (86)
 ∂rn
∂I---
  mk = (rtotal rk)∕Imn (87)
∂r
--n-
∂rk = Imk∕Imn (88)
-∂rn-
∂Imn = -12--
Imn knImk(rtotal rk). (89)
The error in the determination of the contribution of Imn scales with one over the square of Imn. Hence, for small contributions, the error in rn will be large. All other errors scale with one over Imn with the same consequence as before. In other words, the smaller a contribution n in terms of its absolute signal, the more difficult is it to obtain its individual anisotropy rn.

Another word of caution should be added. Also when dealing with composed signals, in general the total anisotropy of a sample decays eventually to zero, respectively to some residual value. Depending on the underlying kinetics the decay may or may not be monotonic. When the decay is monotonic, it might be tempting to describe the obtained curve by an exponential function or a sum of such. However, if the underlying contributions do not share the same kinetics, the obtained exponential terms will have nothing to do with the signals or anisotropies of the individual components because the dependence of the total anisotropy on the individual anisotropies of the different contributions is nonlinear. A proper decomposition has always to refer to (84).