trunk/mattDisertation/Introduction.tex


\chapter{\label{chapt:intro}INTRODUCTION AND THEORETICAL BACKGROUND}


The techniques used in the course of this research fall under the two
main classes of molecular simulation: Molecular Dynamics and Monte
Carlo. Molecular Dynamics simulations are carried out by integrating
the equations of motion for a given system of particles, allowing the
researcher to gain insight into the time dependent evolution of a
system. Transport phenomena are readily studied with this simulation
technique, making Molecular Dynamics the main simulation technique
used in this research. Other aspects of the research fall in the
Monte Carlo class of simulations. In Monte Carlo, the configuration
space available to the collection of particles is sampled
stochastically, or randomly. Each configuration is chosen with a given
probability based on the Boltzmann distribution. These types
of simulations are best used to probe properties of a system that are
dependent only on the state of the system. Structural information
about a system is most readily obtained through these types of
methods.

Although the two techniques employed seem dissimilar, they are both
linked by the over-arching principles of Statistical
Mechanics. Statistical Mechanics governs the behavior of
both classes of simulations and dictates what each method can and
cannot do. When investigating a system, one must first analyze what
thermodynamic properties of the system are being probed, then choose
which method best suits that objective.

\section{\label{introSec:statThermo}Statistical Mechanics}

The following section serves as a brief introduction to some of the
Statistical Mechanics concepts presented in this dissertation.  What
follows is a brief derivation of Boltzmann weighted statistics and an
explanation of how one can use the information to calculate an
observable for a system.  This section then concludes with a brief
discussion of the ergodic hypothesis and its relevance to this
research.

\subsection{\label{introSec:boltzman}Boltzmann weighted statistics}

Consider a system, $\gamma$, with total energy $E_{\gamma}$.  Let
$\Omega(E_{\gamma})$ represent the number of degenerate ways
$\boldsymbol{\Gamma}\{r_1,r_2,\ldots r_n,p_1,p_2,\ldots p_n\}$, the
collection of positions and conjugate momenta of system $\gamma$, can
be configured to give $E_{\gamma}$. Further, if $\gamma$ is a subset
of a larger system, $\boldsymbol{\Lambda}\{E_1,E_2,\ldots
E_{\gamma},\ldots E_n\}$, the total degeneracy of the system can be
expressed as
\begin{equation}
\Omega(\boldsymbol{\Lambda}) = \Omega(E_1) \times \Omega(E_2) \times \ldots
        \Omega(E_{\gamma}) \times \ldots \Omega(E_n).
\label{introEq:SM0.1}
\end{equation}
This multiplicative combination of degeneracies is illustrated in
Fig.~\ref{introFig:degenProd}.

\begin{figure}
\centering
\includegraphics[width=\linewidth]{omegaFig.eps}
\caption[An explanation of the combination of degeneracies]{Systems A and B both have three energy levels and two indistinguishable particles. When the total energy is 2, there are two ways for each system to disperse the energy. However, for system C, the superset of A and B, the total degeneracy is the product of the degeneracy of each system. In this case $\Omega(\text{C})$ is 4.}
\label{introFig:degenProd}
\end{figure}

Next, consider the specific case of $\gamma$ in contact with a
bath. Exchange of energy is allowed between the bath and the system,
subject to the constraint that the total energy
($E_{\text{bath}}+E_{\gamma}$) remain constant. $\Omega(E)$, where $E$
is the total energy of both systems, can be represented as
\begin{equation}
\Omega(E) = \Omega(E_{\gamma}) \times \Omega(E - E_{\gamma}).
\label{introEq:SM1}
\end{equation}
Or additively as,
\begin{equation}
\ln \Omega(E) = \ln \Omega(E_{\gamma}) + \ln \Omega(E - E_{\gamma}).
\label{introEq:SM2}
\end{equation}

The solution to Eq.~\ref{introEq:SM2} maximizes the number of
degenerate configurations in $E$. \cite{Frenkel1996} 
This gives
\begin{equation}
\frac{\partial \ln \Omega(E)}{\partial E_{\gamma}} = 0 =
        \frac{\partial \ln \Omega(E_{\gamma})}{\partial E_{\gamma}}
         + 
        \frac{\partial \ln \Omega(E_{\text{bath}})}{\partial E_{\text{bath}}}
        \frac{\partial E_{\text{bath}}}{\partial E_{\gamma}},
\label{introEq:SM3}
\end{equation}
where $E_{\text{bath}}$ is $E-E_{\gamma}$, and
$\frac{\partial E_{\text{bath}}}{\partial E_{\gamma}}$ is
$-1$. Eq.~\ref{introEq:SM3} becomes
\begin{equation}
\frac{\partial \ln \Omega(E_{\gamma})}{\partial E_{\gamma}} = 
\frac{\partial \ln \Omega(E_{\text{bath}})}{\partial E_{\text{bath}}}.
\label{introEq:SM4}
\end{equation}

At this point, one can draw a relationship between the maximization of
degeneracy in Eq.~\ref{introEq:SM3} and the second law of
thermodynamics.  Namely, that for a closed system, entropy will
increase for an irreversible process.\cite{chandler:1987} Here the
process is the partitioning of energy among the two systems.  This
allows the following definition of entropy:
\begin{equation}
S = k_B \ln \Omega(E),
\label{introEq:SM5}
\end{equation}
where $k_B$ is the Boltzmann constant.  Having defined entropy, one can
also define the temperature of the system using the Maxwell relation,
\begin{equation}
\frac{1}{T} = \biggl ( \frac{\partial S}{\partial E} \biggr )_{N,V}.
\label{introEq:SM6}
\end{equation}
The temperature in the system $\gamma$ is then
\begin{equation}
\beta( E_{\gamma} ) = \frac{1}{k_B T} = 
        \frac{\partial \ln \Omega(E_{\gamma})}{\partial E_{\gamma}}.
\label{introEq:SM7}
\end{equation}
Applying this to Eq.~\ref{introEq:SM4} gives the following
\begin{equation}
\beta( E_{\gamma} ) = \beta( E_{\text{bath}} ).
\label{introEq:SM8}
\end{equation}
Eq.~\ref{introEq:SM8} shows that the partitioning of energy between
the two systems is actually a process of thermal
equilibration.\cite{Frenkel1996}

An application of these results is to formulate the expectation value
of an observable, $A$, in the canonical ensemble. In the canonical
ensemble, the number of particles, $N$, the volume, $V$, and the
temperature, $T$, are all held constant while the energy, $E$, is
allowed to fluctuate. Returning to the previous example, the bath
system is now an infinitely large thermal bath, whose exchange of
energy with the system $\gamma$ holds the temperature constant.  The
partitioning of energy between the bath and the system is then related
to the total energy of both systems and the fluctuations in
$E_{\gamma}$:
\begin{equation}
\Omega( E_{\gamma} ) = \Omega( E - E_{\gamma} ).
\label{introEq:SM9}
\end{equation}
As for the expectation value, it can be defined
\begin{equation}
\langle A \rangle = 
        \int\limits_{\boldsymbol{\Gamma}} d\boldsymbol{\Gamma} 
        P_{\gamma} A(\boldsymbol{\Gamma}),
\label{introEq:SM10}
\end{equation}
where $\int\limits_{\boldsymbol{\Gamma}} d\boldsymbol{\Gamma}$ denotes
an integration over all accessible points in phase space, $P_{\gamma}$
is the probability of being in a given phase state and
$A(\boldsymbol{\Gamma})$ is an observable that is a function of the
phase state.

Because entropy seeks to maximize the number of degenerate states at a
given energy, the probability of being in a particular state in
$\gamma$ will be directly proportional to the number of allowable
states the coupled system is able to assume. Namely,
\begin{equation}
P_{\gamma} \propto \Omega( E_{\text{bath}} ) = 
        e^{\ln \Omega( E - E_{\gamma})}.
\label{introEq:SM11}
\end{equation}
Because $E_{\gamma} \ll E$, $\ln \Omega$ can be expanded in a Taylor series:
\begin{equation}
\ln \Omega ( E - E_{\gamma}) = 
        \ln \Omega (E) -
        E_{\gamma}  \frac{\partial \ln \Omega }{\partial E}
        + \ldots.
\label{introEq:SM12}
\end{equation}
Higher order terms are omitted as $E$ is an infinite thermal
bath. Further, using Eq.~\ref{introEq:SM7}, Eq.~\ref{introEq:SM11} can
be rewritten:
\begin{equation}
P_{\gamma} \propto e^{-\beta E_{\gamma}},
\label{introEq:SM13}
\end{equation}
where $\ln \Omega(E)$ has been factored out of the proportionality as a
constant.  Normalizing the probability ($\int\limits_{\boldsymbol{\Gamma}}
d\boldsymbol{\Gamma} P_{\gamma} = 1$) gives 
\begin{equation}
P_{\gamma} = \frac{e^{-\beta E_{\gamma}}}
{\int\limits_{\boldsymbol{\Gamma}} d\boldsymbol{\Gamma} e^{-\beta E_{\gamma}}}.
\label{introEq:SM14}
\end{equation}
This result is the standard Boltzmann statistical distribution.
Applying it to Eq.~\ref{introEq:SM10} one can obtain the following relation for ensemble averages:
\begin{equation}
\langle A \rangle = 
\frac{\int\limits_{\boldsymbol{\Gamma}} d\boldsymbol{\Gamma} 
        A( \boldsymbol{\Gamma} ) e^{-\beta E_{\gamma}}}
{\int\limits_{\boldsymbol{\Gamma}} d\boldsymbol{\Gamma} e^{-\beta E_{\gamma}}}.
\label{introEq:SM15}
\end{equation}

\subsection{\label{introSec:ergodic}The Ergodic Hypothesis}

In the case of a Molecular Dynamics simulation, rather than
calculating an ensemble average integral over phase space as in
Eq.~\ref{introEq:SM15}, it becomes easier to caclulate the time
average of an observable. Namely,
\begin{equation}
\langle A \rangle_t = \frac{1}{\tau} 
        \int_0^{\tau} A[\boldsymbol{\Gamma}(t)]\,dt,
\label{introEq:SM16}
\end{equation}
where the value of an observable is averaged over the length of time,
$\tau$, that the simulation is run. This type of measurement mirrors
the experimental measurement of an observable. In an experiment, the
instrument analyzing the system must average its observation over the
finite time of the measurement. What is required then, is a principle
to relate the time average to the ensemble average. This is the
ergodic hypothesis.

Ergodicity is the assumption that given an infinite amount of time, a
system will visit every available point in phase
space.\cite{Frenkel1996} For most systems, this is a valid assumption,
except in cases where the system may be trapped in a local feature
(\emph{e.g.}~glasses). When valid, ergodicity allows the unification
of a time averaged observation and an ensemble averaged one. If an
observation is averaged over a sufficiently long time, the system is
assumed to visit all energetically accessible points in phase space,
giving a properly weighted statistical average. This allows the
researcher freedom of choice when deciding how best to measure a given
observable.  When an ensemble averaged approach seems most logical,
the Monte Carlo techniques described in Sec.~\ref{introSec:monteCarlo}
can be utilized.  Conversely, if a problem lends itself to a time
averaging approach, the Molecular Dynamics techniques in
Sec.~\ref{introSec:MD} can be employed.

\section{\label{introSec:monteCarlo}Monte Carlo Simulations}

The Monte Carlo method was developed by Metropolis and Ulam for their
work in fissionable material.\cite{metropolis:1949} The method is so
named, because it uses random numbers extensively.\cite{allen87:csl}
The Monte Carlo method allows for the solution of integrals through
the stochastic sampling of the values within the integral. In the
simplest case, the evaluation of an integral would follow a brute
force method of sampling.\cite{Frenkel1996} Consider the following
single dimensional integral:
\begin{equation}
I = \int_a^b f(x)dx.
\label{eq:MCex1}
\end{equation}
The equation can be recast as:
\begin{equation}
I = \int^b_a \frac{f(x)}{\rho(x)} \rho(x) dx,
\label{introEq:Importance1}
\end{equation}
where $\rho(x)$ is an arbitrary probability distribution in $x$.  If
one conducts $\tau$ trials selecting a random number, $\zeta_\tau$,
from the distribution $\rho(x)$ on the interval $[a,b]$, then
Eq.~\ref{introEq:Importance1} becomes
\begin{equation}
I= \lim_{\tau \rightarrow \infty}\biggl \langle \frac{f(x)}{\rho(x)} \biggr \rangle_{\text{trials}[a,b]}.
\label{introEq:Importance2}
\end{equation}
If $\rho(x)$ is uniformly distributed over the interval $[a,b]$,
\begin{equation}
\rho(x) = \frac{1}{b-a},
\label{introEq:importance2b}
\end{equation}
then the integral can be rewritten as 
\begin{equation}
I = (b-a)\lim_{\tau \rightarrow \infty}
        \langle f(x) \rangle_{\text{trials}[a,b]}.
\label{eq:MCex2}
\end{equation}

However, in Statistical Mechanics, one is typically interested in
integrals of the form:
\begin{equation}
\langle A \rangle = \frac{\int d^N \mathbf{r}~A(\mathbf{r}^N)% 
        e^{-\beta V(\mathbf{r}^N)}}%
        {\int d^N \mathbf{r}~e^{-\beta V(\mathbf{r}^N)}},
\label{eq:mcEnsAvg}
\end{equation}
where $\mathbf{r}^N$ stands for the coordinates of all $N$ particles
and $A$ is some observable that is only dependent on position. This is
the ensemble average of $A$ as presented in
Sec.~\ref{introSec:statThermo}, except here $A$ is independent of
momentum. Therefore the momenta contribution of the integral can be
factored out, leaving the configurational integral. Application of the
brute force method to this system would yield highly inefficient
results. Due to the Boltzmann weighting of this integral, most random
configurations will have a near zero contribution to the ensemble
average. This is where importance sampling comes into
play.\cite{allen87:csl}

Importance sampling is a method where the distribution, from which the
random configurations are chosen, is selected in such a way as to
efficiently sample the integral in question.  Looking at
Eq.~\ref{eq:mcEnsAvg}, and realizing
\begin {equation}
\rho_{kT}(\mathbf{r}^N) = 
        \frac{e^{-\beta V(\mathbf{r}^N)}}
        {\int d^N \mathbf{r}~e^{-\beta V(\mathbf{r}^N)}},
\label{introEq:MCboltzman}
\end{equation}
where $\rho_{kT}$ is the Boltzmann distribution.  The ensemble average
can be rewritten as
\begin{equation}
\langle A \rangle = \int d^N \mathbf{r}~A(\mathbf{r}^N) 
        \rho_{kT}(\mathbf{r}^N).
\label{introEq:Importance3}
\end{equation}
Applying Eq.~\ref{introEq:Importance1} one obtains
\begin{equation}
\langle A \rangle = \biggl \langle
        \frac{ A \rho_{kT}(\mathbf{r}^N) }
        {\rho(\mathbf{r}^N)} \biggr \rangle_{\text{trials}}.
\label{introEq:Importance4}
\end{equation}
By selecting $\rho(\mathbf{r}^N)$ to be $\rho_{kT}(\mathbf{r}^N)$
Eq.~\ref{introEq:Importance4} becomes
\begin{equation}
\langle A \rangle = \langle A(\mathbf{r}^N) \rangle_{kT}.
\label{introEq:Importance5}
\end{equation}
The difficulty is selecting points $\mathbf{r}^N$ such that they are
sampled from the distribution $\rho_{kT}(\mathbf{r}^N)$.  A solution
was proposed by Metropolis \emph{et al}.\cite{metropolis:1953} which involved
the use of a Markov chain whose limiting distribution was
$\rho_{kT}(\mathbf{r}^N)$.

\subsection{\label{introSec:markovChains}Markov Chains}

A Markov chain is a chain of states satisfying the following
conditions:\cite{leach01:mm}
\begin{enumerate}
\item The outcome of each trial depends only on the outcome of the previous trial.
\item Each trial belongs to a finite set of outcomes called the state space.
\end{enumerate}
If given two configurations, $\mathbf{r}^N_m$ and $\mathbf{r}^N_n$,
$\rho_m$ and $\rho_n$ are the probabilities of being in state
$\mathbf{r}^N_m$ and $\mathbf{r}^N_n$ respectively.  Further, the two
states are linked by a transition probability, $\pi_{mn}$, which is the
probability of going from state $m$ to state $n$.

\newcommand{\accMe}{\operatorname{acc}}

The transition probability is given by the following:
\begin{equation}
\pi_{mn} = \alpha_{mn} \times \accMe(m \rightarrow n),
\label{introEq:MCpi}
\end{equation}
where $\alpha_{mn}$ is the probability of attempting the move $m
\rightarrow n$, and $\accMe$ is the probability of accepting the move
$m \rightarrow n$.  Defining a probability vector,
$\boldsymbol{\rho}$, such that
\begin{equation}
\boldsymbol{\rho} = \{\rho_1, \rho_2, \ldots \rho_m, \rho_n, 
        \ldots \rho_N \},
\label{introEq:MCrhoVector}
\end{equation}
a transition matrix $\boldsymbol{\Pi}$ can be defined,
whose elements are $\pi_{mn}$, for each given transition.  The
limiting distribution of the Markov chain can then be found by
applying the transition matrix an infinite number of times to the
distribution vector,
\begin{equation}
\boldsymbol{\rho}_{\text{limit}} = 
        \lim_{N \rightarrow \infty} \boldsymbol{\rho}_{\text{initial}}
        \boldsymbol{\Pi}^N.
\label{introEq:MCmarkovLimit}
\end{equation}
The limiting distribution of the chain is independent of the starting
distribution, and successive applications of the transition matrix
will only yield the limiting distribution again,
\begin{equation}
\boldsymbol{\rho}_{\text{limit}} = \boldsymbol{\rho}_{\text{limit}}
        \boldsymbol{\Pi}.
\label{introEq:MCmarkovEquil}
\end{equation}

\subsection{\label{introSec:metropolisMethod}The Metropolis Method}

In the Metropolis method\cite{metropolis:1953}
Eq.~\ref{introEq:MCmarkovEquil} is solved such that
$\boldsymbol{\rho}_{\text{limit}}$ matches the Boltzmann distribution
of states.  The method accomplishes this by imposing the strong
condition of microscopic reversibility on the equilibrium
distribution.  This means that at equilibrium, the probability of going
from $m$ to $n$ is the same as going from $n$ to $m$,
\begin{equation}
\rho_m\pi_{mn} = \rho_n\pi_{nm}.
\label{introEq:MCmicroReverse}
\end{equation}
Further, $\boldsymbol{\alpha}$ is chosen to be a symmetric matrix in
the Metropolis method.  Using Eq.~\ref{introEq:MCpi},
Eq.~\ref{introEq:MCmicroReverse} becomes
\begin{equation}
\frac{\accMe(m \rightarrow n)}{\accMe(n \rightarrow m)} =
        \frac{\rho_n}{\rho_m}.
\label{introEq:MCmicro2}
\end{equation}
For a Boltzmann limiting distribution,
\begin{equation}
\frac{\rho_n}{\rho_m} = e^{-\beta[\mathcal{U}(n) - \mathcal{U}(m)]}
        = e^{-\beta \Delta \mathcal{U}}.
\label{introEq:MCmicro3}
\end{equation}
This allows for the following set of acceptance rules be defined:
\begin{equation}
\accMe( m \rightarrow n ) = 
        \begin{cases}
        1& \text{if $\Delta \mathcal{U} \leq 0$,} \\
        e^{-\beta \Delta \mathcal{U}}& \text{if $\Delta \mathcal{U} > 0$.}
        \end{cases}
\label{introEq:accRules}
\end{equation}

Using the acceptance criteria from Eq.~\ref{introEq:accRules} the
Metropolis method proceeds as follows
\begin{enumerate}
\item Generate an initial configuration $\mathbf{r}^N$ which has some finite probability in $\rho_{kT}$.
\item Modify $\mathbf{r}^N$, to generate configuration $\mathbf{r^{\prime}}^N$.
\item If the new configuration lowers the energy of the system, accept the move ($\mathbf{r}^N$ becomes $\mathbf{r^{\prime}}^N$).  Otherwise accept with probability $e^{-\beta \Delta \mathcal{U}}$.
\item Accumulate the average for the configurational observable of interest.
\item Repeat from step 2 until the average converges.
\end{enumerate}
One important note is that the average is accumulated whether the move
is accepted or not, this ensures proper weighting of the average.
Using Eq.~\ref{introEq:Importance4} it becomes clear that the
accumulated averages are the ensemble averages, as this method ensures
that the limiting distribution is the Boltzmann distribution.

\section{\label{introSec:MD}Molecular Dynamics Simulations}

The main simulation tool used in this research is Molecular Dynamics.
Molecular Dynamics is the numerical integration of the equations of
motion for a system in order to obtain information about the dynamic
changes in the positions and momentum of the constituent particles.
This allows the calculation of not only configurational observables,
but momentum dependent ones as well: diffusion constants, relaxation
events, folding/unfolding events, etc. With the time dependent
information gained from a Molecular Dynamics simulation, one can also
calculate time correlation functions of the form\cite{Hansen86}
\begin{equation}
\langle A(t)\,A(0)\rangle = \lim_{\tau\rightarrow\infty} \frac{1}{\tau}
        \int_0^{\tau} A(t+t^{\prime})\,A(t^{\prime})\,dt^{\prime}.
\label{introEq:timeCorr}
\end{equation}
These correlations can be used to measure fundamental time constants
of a system, such as diffusion constants from the velocity
autocorrelation or dipole relaxation times from the dipole
autocorrelation.  Due to the principle of ergodicity,
Sec.~\ref{introSec:ergodic}, the average of static observables over
the length of the simulation are taken to be the ensemble averages for
the system.

The choice of when to use molecular dynamics over Monte Carlo
techniques, is normally decided by the observables in which the
researcher is interested.  If the observables depend on time in any
fashion, then the only choice is molecular dynamics in some form.
However, when the observable is dependent only on the configuration,
then for most small systems, Monte Carlo techniques will be more
efficient.  The focus of research in the second half of this
dissertation is centered on the dynamic properties of phospholipid
bilayers, making molecular dynamics key in the simulation of those
properties.

\subsection{\label{introSec:mdAlgorithm}Molecular Dynamics Algorithms}

To illustrate how the molecular dynamics technique is applied, the
following sections will describe the sequence involved in a
simulation.  Sec.~\ref{introSec:mdInit} deals with the initialization
of a simulation.  Sec.~\ref{introSec:mdForce} discusses issues
involved with the calculation of the forces.
Sec.~\ref{introSec:mdIntegrate} concludes the algorithm discussion
with the integration of the equations of motion.\cite{Frenkel1996}

\subsection{\label{introSec:mdInit}Initialization}

When selecting the initial configuration for the simulation it is
important to consider what dynamics one is hoping to observe.
Ch.~\ref{chapt:lipid} deals with the formation and equilibrium dynamics of
phospholipid membranes.  Therefore in these simulations initial
positions were selected that in some cases dispersed the lipids in
water, and in other cases structured the lipids into preformed
bilayers.  Important considerations at this stage of the simulation are:
\begin{itemize}
\item There are no overlapping molecules or atoms.
\item Velocities are chosen in such a way as to give the system zero total momentum and angular momentum.
\item It is also sometimes desirable to select the velocities to correctly sample the ensemble at a particular target temperature.
\end{itemize}

The first point is important due to the forces generated when two
particles are too close together.  If overlap occurs, the first
evaluation of forces will return numbers so large as to render the
numerical integration of the equations motion meaningless.  The second
consideration keeps the system from drifting or rotating as a whole.
This arises from the fact that most simulations are of systems in
equilibrium in the absence of outside forces.  Therefore any net
movement would be unphysical and an artifact of the simulation method
used.  The final point addresses the selection of the magnitude of the
initial velocities.  For many simulations it is convenient to use this
opportunity to scale the amount of kinetic energy to reflect the
desired thermal distribution of the system.  However, it must be noted
that due to equipartition, most systems will require further velocity
rescaling after the first few initial simulation steps due to either
loss or gain of kinetic energy from energy stored as potential energy.

\subsection{\label{introSec:mdForce}Force Evaluation}

The evaluation of forces is the most computationally expensive portion
of any molecular dynamics simulation.  This is due entirely to the
evaluation of long range forces in a simulation, which are typically
pair potentials.  These forces are most commonly the van der Waals
force, and sometimes Coulombic forces as well.  For a pair-wise
interaction, there are $N(N-1)/ 2$ pairs to be evaluated, where $N$ is
the number of particles in the system.  This leads to calculations which
scale as $N^2$, making large simulations prohibitive in the absence
of any computation saving techniques.

Another consideration one must resolve, is that in a given simulation,
a disproportionate number of the particles will feel the effects of
the surface.\cite{allen87:csl} For a cubic system of 1000 particles
arranged in a $10 \times 10 \times 10$ cube, 488 particles will be
exposed to the surface.  Unless one is simulating an isolated cluster
in a vacuum, the behavior of the system will be far from the desired
bulk characteristics.  To offset this, simulations employ the use of
periodic images.\cite{born:1912}

The technique involves the use of an algorithm that replicates the
simulation box on an infinite lattice in Cartesian space.  Any
particle leaving the simulation box on one side will have an image of
itself enter on the opposite side (see
Fig.~\ref{introFig:pbc}). Therefore, a pair of particles have an
image of each other, real or periodic, within $\text{box}/2$.  A
discussion of the method used to calculate the periodic image can be
found in Sec.\ref{oopseSec:pbc}.

\begin{figure}
\centering
\includegraphics[width=\linewidth]{pbcFig.eps}
\caption[An illustration of periodic boundary conditions]{A 2-D illustration of periodic boundary conditions. As one particle leaves the right of the simulation box, an image of it enters the left.}
\label{introFig:pbc}
\end{figure}

Returning to the topic of the computational scaling of the force
evaluation, the use of periodic boundary conditions requires that a
cutoff radius be employed.  Using a cutoff radius improves the
efficiency of the force evaluation, as particles farther than a
predetermined distance, $r_{\text{cut}}$, are not included in the
calculation.\cite{Frenkel1996} In a simulation with periodic images,
there are two methods to choose from, both with their own cutoff
limits. In the minimum image convention, $r_{\text{cut}}$ has a
maximum value of $\text{box}/2$. This is because each atom has only
one image that is seen by other atoms. The image used is the one that
minimizes the distance between the two atoms. A system of wrapped
images about a central atom therefore has a maximum length scale of
box on a side (Fig.~\ref{introFig:rMaxMin}). The second convention,
multiple image convention, has a maximum $r_{\text{cut}}$ of the box
length itself. Here multiple images of each atom are replicated in the
periodic cells surrounding the central atom, this causes the atom to
see multiple copies of several atoms. If the cutoff radius is larger
than box, however, then the atom will see an image of itself, and
attempt to calculate an unphysical self-self force interaction
(Fig.~\ref{introFig:rMaxMult}). Due to the increased complexity and
commputaional ineffeciency of the multiple image method, the minimum
image method is the used throughout this research.

\begin{figure}
\centering
\includegraphics[width=\linewidth]{rCutMaxFig.eps}
\caption[An explanation of minimum image convention]{The yellow atom has all other images wrapped to itself as the center. If $r_{\text{cut}}=\text{box}/2$, then the distribution is uniform (blue atoms). However, when $r_{\text{cut}}>\text{box}/2$ the corners are disproportionately weighted (green atoms) vs the axial directions (shaded regions).}
\label{introFig:rMaxMin}
\end{figure}

\begin{figure}
\centering
\includegraphics[width=\linewidth]{rCutMaxMultFig.eps}
\caption[An explanation of multiple image convention]{The yellow atom is the central wrapping point. The blue atoms are the minimum images of the system about the central atom. The boxes with the green atoms are multiple images of the central box. If $r_{\text{cut}} \geq \text{box}$ then the central atom sees multiple images of itself (red atom), creating a self-self force evaluation.}
\label{introFig:rMaxMult}
\end{figure}

With the use of a cutoff radius, however, comes a discontinuity in
the potential energy curve (Fig.~\ref{introFig:shiftPot}). To fix this
discontinuity, one calculates the potential energy at the
$r_{\text{cut}}$, and adds that value to the potential, causing
the function to go smoothly to zero at the cutoff radius.  This
shifted potential ensures conservation of energy when integrating the
Newtonian equations of motion.

\begin{figure}
\centering
\includegraphics[width=\linewidth]{shiftedPot.eps}
\caption[Shifting the Lennard-Jones Potential]{The Lennard-Jones potential (blue line) is shifted (red line) to remove the discontinuity at $r_{\text{cut}}$.}
\label{introFig:shiftPot}
\end{figure}

The second main simplification used in this research is the Verlet
neighbor list.\cite{allen87:csl} In the Verlet method, one generates
a list of all neighbor atoms, $j$, surrounding atom $i$ within some
cutoff $r_{\text{list}}$, where $r_{\text{list}}>r_{\text{cut}}$.
This list is created the first time forces are evaluated, then on
subsequent force evaluations, pair calculations are only calculated
from the neighbor lists.  The lists are updated if any particle
in the system moves farther than $r_{\text{list}}-r_{\text{cut}}$,
which indeicates the possibility that a particle has left or joined the
neighbor list.

\subsection{\label{introSec:mdIntegrate} Integration of the Equations of Motion}

A starting point for the discussion of molecular dynamics integrators
is the Verlet algorithm.\cite{Frenkel1996} It begins with a Taylor
expansion of position in time:
\begin{equation}
q(t+\Delta t)= q(t) + v(t)\Delta t + \frac{F(t)}{2m}\Delta t^2 +
        \frac{\Delta t^3}{3!}\frac{\partial^3 q(t)}{\partial t^3} +
        \mathcal{O}(\Delta t^4) .
\label{introEq:verletForward}
\end{equation}
As well as,
\begin{equation}
q(t-\Delta t)= q(t) - v(t)\Delta t + \frac{F(t)}{2m}\Delta t^2 -
        \frac{\Delta t^3}{3!}\frac{\partial^3 q(t)}{\partial t^3} +
        \mathcal{O}(\Delta t^4) ,
\label{introEq:verletBack}
\end{equation}
where $m$ is the mass of the particle, $q(t)$ is the position at time
$t$, $v(t)$ the velocity, and $F(t)$ the force acting on the
particle. Adding together Eq.~\ref{introEq:verletForward} and
Eq.~\ref{introEq:verletBack} results in,
\begin{equation}
q(t+\Delta t)+q(t-\Delta t) = 
        2q(t) + \frac{F(t)}{m}\Delta t^2 + \mathcal{O}(\Delta t^4) ,
\label{introEq:verletSum}
\end{equation}
or equivalently,
\begin{equation}
q(t+\Delta t) \approx 
        2q(t) - q(t-\Delta t) + \frac{F(t)}{m}\Delta t^2.
\label{introEq:verletFinal}
\end{equation}
Which contains an error in the estimate of the new positions on the
order of $\Delta t^4$.

In practice, however, the simulations in this research were integrated
with the velocity reformulation of the Verlet method.\cite{allen87:csl}
\begin{align}
q(t+\Delta t) &= q(t) + v(t)\Delta t + \frac{F(t)}{2m}\Delta t^2 ,%
\label{introEq:MDvelVerletPos} \\%
%
v(t+\Delta t) &= v(t) + \frac{\Delta t}{2m}[F(t) + F(t+\Delta t)] .%
\label{introEq:MDvelVerletVel}
\end{align}
The original Verlet algorithm can be regained by substituting the
velocity back into Eq.~\ref{introEq:MDvelVerletPos}.  The Verlet
formulations are chosen in this research because the algorithms have
very little long time drift in energy.  Energy conservation in a
molecular dynamics simulation is of extreme importance, as it is a
measure of how closely one is following the ``true'' trajectory with
the finite integration scheme.  An exact solution to the integration
will conserve area in phase space (i.e.~will be symplectic), as well
as be reversible in time, that is, the trajectory integrated forward
or backwards will exactly match itself.  Having a finite algorithm
that both conserves area in phase space and is time reversible,
therefore increases the reliability, but does not guarantee the
``correctness'' of the integrated trajectory.

It can be shown,\cite{Frenkel1996} that although the Verlet algorithm
does not rigorously preserve the actual Hamiltonian, it does preserve
a pseudo-Hamiltonian which shadows the real one in phase space.  This
pseudo-Hamiltonian is provably area-conserving as well as time
reversible.  The fact that it shadows the true Hamiltonian in phase
space is acceptable in actual simulations as one is interested in the
ensemble average of the observable being measured.  From the ergodic
hypothesis (Sec.~\ref{introSec:statThermo}), it is known that the time
average will match the ensemble average, therefore two similar
trajectories in phase space should give matching statistical averages.

\subsection{\label{introSec:MDfurther}Further Considerations}

In the simulations presented in this research, a few additional
parameters are needed to describe the motions.  In the simulations
involving water and phospholipids in Ch.~\ref{chapt:lipid}, we are
required to integrate the equations of motions for dipoles on atoms.
This involves an additional three parameters be specified for each
dipole atom: $\phi$, $\theta$, and $\psi$.  These three angles are
taken to be the Euler angles, where $\phi$ is a rotation about the
$z$-axis, and $\theta$ is a rotation about the new $x$-axis, and
$\psi$ is a final rotation about the new $z$-axis (see
Fig.~\ref{introFig:eulerAngles}).  This sequence of rotations can be
accumulated into a single $3 \times 3$ matrix, $\mathsf{A}$,
defined as follows:
\begin{equation}
\mathsf{A} = 
\begin{bmatrix}
        \cos\phi\cos\psi-\sin\phi\cos\theta\sin\psi &%
        \sin\phi\cos\psi+\cos\phi\cos\theta\sin\psi &%
        \sin\theta\sin\psi \\%
        %
        -\cos\phi\sin\psi-\sin\phi\cos\theta\cos\psi &%
        -\sin\phi\sin\psi+\cos\phi\cos\theta\cos\psi &%
        \sin\theta\cos\psi \\%
        %
        \sin\phi\sin\theta &%
        -\cos\phi\sin\theta &%
        \cos\theta
\end{bmatrix}.
\label{introEq:EulerRotMat}
\end{equation}

\begin{figure}
\centering
\includegraphics[width=\linewidth]{eulerRotFig.eps}
\caption[Euler rotation of Cartesian coordinates]{The rotation scheme for Euler angles. First is a rotation of $\phi$ about the $z$ axis (blue rotation). Next is a rotation of $\theta$ about the new $x$ axis (green rotation). Lastly is a final rotation of $\psi$ about the new $z$ axis (red rotation).}
\label{introFig:eulerAngles}
\end{figure}

The equations of motion for Euler angles can be written down
as\cite{allen87:csl}
\begin{align}
\dot{\phi} &= -\omega^s_x \frac{\sin\phi\cos\theta}{\sin\theta} +
        \omega^s_y \frac{\cos\phi\cos\theta}{\sin\theta} +
        \omega^s_z,
\label{introEq:MDeulerPhi} \\%
%
\dot{\theta} &= \omega^s_x \cos\phi + \omega^s_y \sin\phi,
\label{introEq:MDeulerTheta} \\%
%
\dot{\psi} &= \omega^s_x \frac{\sin\phi}{\sin\theta} - 
        \omega^s_y \frac{\cos\phi}{\sin\theta},
\label{introEq:MDeulerPsi}
\end{align}
where $\omega^s_{\alpha}$ is the angular velocity in the lab space frame
along Cartesian coordinate $\alpha$.  However, a difficulty arises when
attempting to integrate Eq.~\ref{introEq:MDeulerPhi} and
Eq.~\ref{introEq:MDeulerPsi}. The $\frac{1}{\sin \theta}$ present in
both equations means there is a non-physical instability present when
$\theta$ is 0 or $\pi$. To correct for this, the simulations integrate
the rotation matrix, $\mathsf{A}$, directly, thus avoiding the
instability.  This method was proposed by Dullweber
\emph{et. al.}\cite{Dullweber1997}, and is presented in
Sec.~\ref{introSec:MDsymplecticRot}.

\subsection{\label{introSec:MDliouville}Liouville Propagator}

Before discussing the integration of the rotation matrix, it is
necessary to understand the construction of a ``good'' integration
scheme.  It has been previously discussed
(Sec.~\ref{introSec:mdIntegrate}) how it is desirable for an
integrator to be symplectic and time reversible.  The following is an
outline of the Trotter factorization of the Liouville Propagator as a
scheme for generating symplectic, time-reversible
integrators.\cite{Tuckerman92}

For a system with $f$ degrees of freedom the Liouville operator can be
defined as,
\begin{equation}
iL=\sum^f_{j=1} \biggl [\dot{q}_j\frac{\partial}{\partial q_j} +
        F_j\frac{\partial}{\partial p_j} \biggr ].
\label{introEq:LiouvilleOperator}
\end{equation}
Here, $q_j$ and $p_j$ are the position and conjugate momenta of a
degree of freedom, and $F_j$ is the force on that degree of freedom.
$\Gamma$ is defined as the set of all positions and conjugate momenta,
$\{q_j,p_j\}$, and the propagator, $U(t)$, is defined
\begin {equation}
U(t) = e^{iLt}.
\label{introEq:Lpropagator}
\end{equation}
This allows the specification of $\Gamma$ at any time $t$ as 
\begin{equation}
\Gamma(t) = U(t)\Gamma(0).
\label{introEq:Lp2}
\end{equation}
It is important to note, $U(t)$ is a unitary operator meaning
\begin{equation}
U(-t)=U^{-1}(t).
\label{introEq:Lp3}
\end{equation}

Decomposing $L$ into two parts, $iL_1$ and $iL_2$, one can use the
Trotter theorem to yield
\begin{align}
e^{iLt} &= e^{i(L_1 + L_2)t}, \notag \\%
%
        &= \biggl [ e^{i(L_1 +L_2)\frac{t}{P}} \biggr]^P, \notag \\%
%
        &= \biggl [ e^{iL_1\frac{\Delta t}{2}}\, e^{iL_2\Delta t}\,
        e^{iL_1\frac{\Delta t}{2}} \biggr ]^P +
        \mathcal{O}\biggl (\frac{t^3}{P^2} \biggr ), \label{introEq:Lp4}
\end{align}
where $\Delta t = t/P$.
With this, a discrete time operator $G(\Delta t)$ can be defined:
\begin{align}
G(\Delta t) &= e^{iL_1\frac{\Delta t}{2}}\, e^{iL_2\Delta t}\,
        e^{iL_1\frac{\Delta t}{2}}, \notag \\%
%
        &= U_1 \biggl ( \frac{\Delta t}{2} \biggr )\, U_2 ( \Delta t )\,
        U_1 \biggl ( \frac{\Delta t}{2} \biggr ).
\label{introEq:Lp5}
\end{align}
Because $U_1(t)$ and $U_2(t)$ are unitary, $G(\Delta t)$ is also
unitary.  This means that an integrator based on this factorization will be
reversible in time.

As an example, consider the following decomposition of $L$:
\begin{align}
iL_1 &= \dot{q}\frac{\partial}{\partial q},%
\label{introEq:Lp6a} \\%
%
iL_2 &= F(q)\frac{\partial}{\partial p}.%
\label{introEq:Lp6b}
\end{align}
This leads to propagator $G( \Delta t )$ as,
\begin{equation}
G(\Delta t) =  e^{\frac{\Delta t}{2} F(q)\frac{\partial}{\partial p}} \,
        e^{\Delta t\,\dot{q}\frac{\partial}{\partial q}} \,
        e^{\frac{\Delta t}{2} F(q)\frac{\partial}{\partial p}}.
\label{introEq:Lp7}
\end{equation}
Operating $G(\Delta t)$ on $\Gamma(0)$, and utilizing the operator property
\begin{equation}
e^{c\frac{\partial}{\partial x}}\, f(x) = f(x+c),
\label{introEq:Lp8}
\end{equation}
where $c$ is independent of $x$.  One obtains the following:  
\begin{align}
\dot{q}\biggl (\frac{\Delta t}{2}\biggr ) &=
        \dot{q}(0) + \frac{\Delta t}{2m}\, F[q(0)], \label{introEq:Lp9a}\\%
%
q(\Delta t) &= q(0) + \Delta t\, \dot{q}\biggl (\frac{\Delta t}{2}\biggr ),%
        \label{introEq:Lp9b}\\%
%
\dot{q}(\Delta t) &= \dot{q}\biggl (\frac{\Delta t}{2}\biggr ) +
        \frac{\Delta t}{2m}\, F[q(0)]. \label{introEq:Lp9c}
\end{align}
Or written another way,
\begin{align}
q(t+\Delta t) &= q(0) + \dot{q}(0)\Delta t + 
        \frac{F[q(0)]}{m}\frac{\Delta t^2}{2}, %
\label{introEq:Lp10a} \\%
%
\dot{q}(\Delta t) &= \dot{q}(0) + \frac{\Delta t}{2m}
        \biggl [F[q(0)] + F[q(\Delta t)] \biggr]. %
\label{introEq:Lp10b}
\end{align}
This is the velocity Verlet formulation presented in
Sec.~\ref{introSec:mdIntegrate}.  Because this integration scheme is
comprised of unitary propagators, it is symplectic, and therefore area
preserving in phase space.  From the preceding factorization, one can
see that the integration of the equations of motion would follow:
\begin{enumerate}
\item calculate the velocities at the half step, $\frac{\Delta t}{2}$, from the forces calculated at the initial position.

\item Use the half step velocities to move positions one whole step, $\Delta t$.

\item Evaluate the forces at the new positions, $\mathbf{r}(\Delta t)$, and use the new forces to complete the velocity move.

\item Repeat from step 1 with the new position, velocities, and forces assuming the roles of the initial values.
\end{enumerate}

\subsection{\label{introSec:MDsymplecticRot} Symplectic Propagation of the Rotation Matrix}

Based on the factorization from the previous section,
Dullweber\emph{et al}.\cite{Dullweber1997}~ proposed a scheme for the
symplectic propagation of the rotation matrix, $\mathsf{A}$, as an
alternative method for the integration of orientational degrees of
freedom. The method starts with a straightforward splitting of the
Liouville operator:
\begin{align}
iL_{\text{pos}} &= \dot{q}\frac{\partial}{\partial q} +
        \mathsf{\dot{A}}\frac{\partial}{\partial \mathsf{A}} ,
\label{introEq:SR1a} \\%
%
iL_F &= F(q)\frac{\partial}{\partial p},
\label{introEq:SR1b} \\%
iL_{\tau} &= \tau(\mathsf{A})\frac{\partial}{\partial j},
\label{introEq:SR1b} \\%
\end{align}
where $\tau(\mathsf{A})$ is the torque of the system
due to the configuration, and $j$ is the conjugate
angular momenta of the system. The propagator, $G(\Delta t)$, becomes
\begin{equation}
G(\Delta t) = e^{\frac{\Delta t}{2} F(q)\frac{\partial}{\partial p}} \,
        e^{\frac{\Delta t}{2} \tau(\mathsf{A})\frac{\partial}{\partial j}} \,
        e^{\Delta t\,iL_{\text{pos}}} \,
        e^{\frac{\Delta t}{2} \tau(\mathsf{A})\frac{\partial}{\partial j}} \,
        e^{\frac{\Delta t}{2} F(q)\frac{\partial}{\partial p}}.
\label{introEq:SR2}
\end{equation}
Propagation of the linear and angular momenta follows as in the Verlet
scheme.  The propagation of positions also follows the Verlet scheme
with the addition of a further symplectic splitting of the rotation
matrix propagation, $\mathcal{U}_{\text{rot}}(\Delta t)$, within
$U_{\text{pos}}(\Delta t)$.
\begin{equation}
\mathcal{U}_{\text{rot}}(\Delta t) = 
        \mathcal{U}_x \biggl(\frac{\Delta t}{2}\biggr)\,
        \mathcal{U}_y \biggl(\frac{\Delta t}{2}\biggr)\,
        \mathcal{U}_z (\Delta t)\,
        \mathcal{U}_y \biggl(\frac{\Delta t}{2}\biggr)\,
        \mathcal{U}_x \biggl(\frac{\Delta t}{2}\biggr),
\label{introEq:SR3}
\end{equation}
where $\mathcal{U}_{\alpha}$ is a unitary rotation of $\mathsf{A}$ and
$j$ about each axis $\alpha$.  As all propagations are now
unitary and symplectic, the entire integration scheme is also
symplectic and time reversible.

\section{\label{introSec:layout}Dissertation Layout}

This dissertation is divided as follows: Ch.~\ref{chapt:RSA}
presents the random sequential adsorption simulations of related
pthalocyanines on a gold (111) surface. Ch.~\ref{chapt:oopse}
is about our molecular dynamics simulation package
{\sc oopse}. Ch.~\ref{chapt:lipid} regards the simulations of
phospholipid bilayers using a mesoscale model. And lastly,
Ch.~\ref{chapt:conclusion} concludes this dissertation with a
summary of all results. The chapters are arranged in chronological
order, and reflect the progression of techniques I employed during my
research.  

The chapter concerning random sequential adsorption simulations is a
study in applying Statistical Mechanics simulation techniques in order
to obtain a simple model capable of explaining the results.  My
advisor, Dr. Gezelter, and I were approached by a colleague,
Dr. Lieberman, about possible explanations for the partial coverage of
a gold surface by a particular compound synthesized in her group. We
suggested it might be due to the statistical packing fraction of disks
on a plane, and set about simulating this system.  As the events in
our model were not dynamic in nature, a Monte Carlo method was
employed.  Here, if a molecule landed on the surface without
overlapping with another, then its landing was accepted.  However, if there
was overlap, the landing we rejected and a new random landing location
was chosen.  This defined our acceptance rules and allowed us to
construct a Markov chain whose limiting distribution was the surface
coverage in which we were interested.

The following chapter, about the simulation package {\sc oopse},
describes in detail the large body of scientific code that had to be
written in order to study phospholipid bilayers.  Although there are
pre-existing molecular dynamic simulation packages available, none
were capable of implementing the models we were developing. {\sc
oopse} is a unique package capable of not only integrating the
equations of motion in Cartesian space, but is also able to integrate
the rotational motion of rigid bodies and dipoles.  It also has the
ability to perform calculations across distributed parallel processors
and contains a flexible script syntax for creating systems.  {\sc
oopse} has become a very powerful scientific instrument for the
exploration of our model.

In Ch.~\ref{chapt:lipid}, utilizing {\sc oopse}, I have been
able to parameterize a mesoscale model for phospholipid simulations.
This model retains information about solvent ordering around the
bilayer, as well as information regarding the interaction of the
phospholipid head groups' dipoles with each other and the surrounding
solvent.  These simulations give us insight into the dynamic events
that lead to the formation of phospholipid bilayers, as well as
provide the foundation for future exploration of bilayer phase
behavior with this model.  

In the last chapter, I discuss future directions
for both {\sc oopse} and this mesoscale model.  Additionally, I will
give a summary of the results found in this dissertation.
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