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\chapter{\label{chapt:intro}Introduction and Theoretical Background} |
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\section{\label{introSec:theory}Theoretical Background} |
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The techniques used in the course of this research fall under the two |
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main classes of molecular simulation: Molecular Dynamics and Monte |
8 |
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Carlo. Molecular Dynamic simulations integrate the equations of motion |
27 |
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thermodynamic properties of the system are being probed, then chose |
28 |
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which method best suits that objective. |
29 |
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|
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\subsection{\label{introSec:statThermo}Statistical Thermodynamics} |
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\section{\label{introSec:statThermo}Statistical Mechanics} |
31 |
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|
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ergodic hypothesis |
32 |
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The following section serves as a brief introduction to some of the |
33 |
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Statistical Mechanics concepts present in this dissertation. What |
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follows is a brief derivation of Blotzman weighted statistics, and an |
35 |
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explanation of how one can use the information to calculate an |
36 |
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observable for a system. This section then concludes with a brief |
37 |
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discussion of the ergodic hypothesis and its relevance to this |
38 |
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research. |
39 |
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|
40 |
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enesemble averages |
40 |
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\subsection{\label{introSec:boltzman}Boltzman weighted statistics} |
41 |
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|
42 |
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\subsection{\label{introSec:monteCarlo}Monte Carlo Simulations} |
42 |
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Consider a system, $\gamma$, with some total energy,, $E_{\gamma}$. |
43 |
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Let $\Omega(E_{\gamma})$ represent the number of degenerate ways |
44 |
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$\boldsymbol{\Gamma}$, the collection of positions and conjugate |
45 |
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momenta of system $\gamma$, can be configured to give |
46 |
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$E_{\gamma}$. Further, if $\gamma$ is in contact with a bath system |
47 |
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where energy is exchanged between the two systems, $\Omega(E)$, where |
48 |
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$E$ is the total energy of both systems, can be represented as |
49 |
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\begin{equation} |
50 |
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\Omega(E) = \Omega(E_{\gamma}) \times \Omega(E - E_{\gamma}) |
51 |
> |
\label{introEq:SM1} |
52 |
> |
\end{equation} |
53 |
> |
Or additively as |
54 |
> |
\begin{equation} |
55 |
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\ln \Omega(E) = \ln \Omega(E_{\gamma}) + \ln \Omega(E - E_{\gamma}) |
56 |
> |
\label{introEq:SM2} |
57 |
> |
\end{equation} |
58 |
|
|
59 |
+ |
The solution to Eq.~\ref{introEq:SM2} maximizes the number of |
60 |
+ |
degenerative configurations in $E$. \cite{Frenkel1996} |
61 |
+ |
This gives |
62 |
+ |
\begin{equation} |
63 |
+ |
\frac{\partial \ln \Omega(E)}{\partial E_{\gamma}} = 0 = |
64 |
+ |
\frac{\partial \ln \Omega(E_{\gamma})}{\partial E_{\gamma}} |
65 |
+ |
+ |
66 |
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\frac{\partial \ln \Omega(E_{\text{bath}})}{\partial E_{\text{bath}}} |
67 |
+ |
\frac{\partial E_{\text{bath}}}{\partial E_{\gamma}} |
68 |
+ |
\label{introEq:SM3} |
69 |
+ |
\end{equation} |
70 |
+ |
Where $E_{\text{bath}}$ is $E-E_{\gamma}$, and |
71 |
+ |
$\frac{\partial E_{\text{bath}}}{\partial E_{\gamma}}$ is |
72 |
+ |
$-1$. Eq.~\ref{introEq:SM3} becomes |
73 |
+ |
\begin{equation} |
74 |
+ |
\frac{\partial \ln \Omega(E_{\gamma})}{\partial E_{\gamma}} = |
75 |
+ |
\frac{\partial \ln \Omega(E_{\text{bath}})}{\partial E_{\text{bath}}} |
76 |
+ |
\label{introEq:SM4} |
77 |
+ |
\end{equation} |
78 |
+ |
|
79 |
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At this point, one can draw a relationship between the maximization of |
80 |
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degeneracy in Eq.~\ref{introEq:SM3} and the second law of |
81 |
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thermodynamics. Namely, that for a closed system, entropy will |
82 |
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increase for an irreversible process.\cite{chandler:1987} Here the |
83 |
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process is the partitioning of energy among the two systems. This |
84 |
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allows the following definition of entropy: |
85 |
+ |
\begin{equation} |
86 |
+ |
S = k_B \ln \Omega(E) |
87 |
+ |
\label{introEq:SM5} |
88 |
+ |
\end{equation} |
89 |
+ |
Where $k_B$ is the Boltzman constant. Having defined entropy, one can |
90 |
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also define the temperature of the system using the relation |
91 |
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\begin{equation} |
92 |
+ |
\frac{1}{T} = \biggl ( \frac{\partial S}{\partial E} \biggr )_{N,V} |
93 |
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\label{introEq:SM6} |
94 |
+ |
\end{equation} |
95 |
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The temperature in the system $\gamma$ is then |
96 |
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\begin{equation} |
97 |
+ |
\beta( E_{\gamma} ) = \frac{1}{k_B T} = |
98 |
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\frac{\partial \ln \Omega(E_{\gamma})}{\partial E_{\gamma}} |
99 |
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\label{introEq:SM7} |
100 |
+ |
\end{equation} |
101 |
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Applying this to Eq.~\ref{introEq:SM4} gives the following |
102 |
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\begin{equation} |
103 |
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\beta( E_{\gamma} ) = \beta( E_{\text{bath}} ) |
104 |
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\label{introEq:SM8} |
105 |
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\end{equation} |
106 |
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Showing that the partitioning of energy between the two systems is |
107 |
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actually a process of thermal equilibration.\cite{Frenkel1996} |
108 |
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|
109 |
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An application of these results is to formulate the form of an |
110 |
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expectation value of an observable, $A$, in the canonical ensemble. In |
111 |
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the canonical ensemble, the number of particles, $N$, the volume, $V$, |
112 |
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and the temperature, $T$, are all held constant while the energy, $E$, |
113 |
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is allowed to fluctuate. Returning to the previous example, the bath |
114 |
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system is now an infinitly large thermal bath, whose exchange of |
115 |
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energy with the system $\gamma$ holds the temperature constant. The |
116 |
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partitioning of energy in the bath system is then related to the total |
117 |
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energy of both systems and the fluctuations in $E_{\gamma}$: |
118 |
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\begin{equation} |
119 |
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\Omega( E_{\gamma} ) = \Omega( E - E_{\gamma} ) |
120 |
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\label{introEq:SM9} |
121 |
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\end{equation} |
122 |
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As for the expectation value, it can be defined |
123 |
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\begin{equation} |
124 |
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\langle A \rangle = |
125 |
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\int\limits_{\boldsymbol{\Gamma}} d\boldsymbol{\Gamma} |
126 |
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P_{\gamma} A(\boldsymbol{\Gamma}) |
127 |
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\label{introEq:SM10} |
128 |
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\end{equation} |
129 |
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Where $\int\limits_{\boldsymbol{\Gamma}} d\boldsymbol{\Gamma}$ denotes |
130 |
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an integration over all accessable phase space, $P_{\gamma}$ is the |
131 |
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probability of being in a given phase state and |
132 |
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$A(\boldsymbol{\Gamma})$ is some observable that is a function of the |
133 |
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phase state. |
134 |
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|
135 |
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Because entropy seeks to maximize the number of degenerate states at a |
136 |
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given energy, the probability of being in a particular state in |
137 |
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$\gamma$ will be directly proportional to the number of allowable |
138 |
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states the coupled system is able to assume. Namely, |
139 |
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\begin{equation} |
140 |
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P_{\gamma} \propto \Omega( E_{\text{bath}} ) = |
141 |
+ |
e^{\ln \Omega( E - E_{\gamma})} |
142 |
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\label{introEq:SM11} |
143 |
+ |
\end{equation} |
144 |
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With $E_{\gamma} \ll E$, $\ln \Omega$ can be expanded in a Taylor series: |
145 |
+ |
\begin{equation} |
146 |
+ |
\ln \Omega ( E - E_{\gamma}) = |
147 |
+ |
\ln \Omega (E) - |
148 |
+ |
E_{\gamma} \frac{\partial \ln \Omega }{\partial E} |
149 |
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+ \ldots |
150 |
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\label{introEq:SM12} |
151 |
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\end{equation} |
152 |
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Higher order terms are omitted as $E$ is an infinite thermal |
153 |
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bath. Further, using Eq.~\ref{introEq:SM7}, Eq.~\ref{introEq:SM11} can |
154 |
+ |
be rewritten: |
155 |
+ |
\begin{equation} |
156 |
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P_{\gamma} \propto e^{-\beta E_{\gamma}} |
157 |
+ |
\label{introEq:SM13} |
158 |
+ |
\end{equation} |
159 |
+ |
Where $\ln \Omega(E)$ has been factored out of the porpotionality as a |
160 |
+ |
constant. Normalizing the probability ($\int\limits_{\boldsymbol{\Gamma}} |
161 |
+ |
d\boldsymbol{\Gamma} P_{\gamma} = 1$) gives |
162 |
+ |
\begin{equation} |
163 |
+ |
P_{\gamma} = \frac{e^{-\beta E_{\gamma}}} |
164 |
+ |
{\int\limits_{\boldsymbol{\Gamma}} d\boldsymbol{\Gamma} e^{-\beta E_{\gamma}}} |
165 |
+ |
\label{introEq:SM14} |
166 |
+ |
\end{equation} |
167 |
+ |
This result is the standard Boltzman statistical distribution. |
168 |
+ |
Applying it to Eq.~\ref{introEq:SM10} one can obtain the following relation for ensemble averages: |
169 |
+ |
\begin{equation} |
170 |
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\langle A \rangle = |
171 |
+ |
\frac{\int\limits_{\boldsymbol{\Gamma}} d\boldsymbol{\Gamma} |
172 |
+ |
A( \boldsymbol{\Gamma} ) e^{-\beta E_{\gamma}}} |
173 |
+ |
{\int\limits_{\boldsymbol{\Gamma}} d\boldsymbol{\Gamma} e^{-\beta E_{\gamma}}} |
174 |
+ |
\label{introEq:SM15} |
175 |
+ |
\end{equation} |
176 |
+ |
|
177 |
+ |
\subsection{\label{introSec:ergodic}The Ergodic Hypothesis} |
178 |
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|
179 |
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One last important consideration is that of ergodicity. Ergodicity is |
180 |
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the assumption that given an infinite amount of time, a system will |
181 |
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visit every available point in phase space.\cite{Frenkel1996} For most |
182 |
+ |
systems, this is a valid assumption, except in cases where the system |
183 |
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may be trapped in a local feature (\emph{e.g.}~glasses). When valid, |
184 |
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ergodicity allows the unification of a time averaged observation and |
185 |
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an ensemble averged one. If an observation is averaged over a |
186 |
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sufficiently long time, the system is assumed to visit all |
187 |
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appropriately available points in phase space, giving a properly |
188 |
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weighted statistical average. This allows the researcher freedom of |
189 |
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choice when deciding how best to measure a given observable. When an |
190 |
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ensemble averaged approach seems most logical, the Monte Carlo |
191 |
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techniques described in Sec.~\ref{introSec:monteCarlo} can be utilized. |
192 |
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Conversely, if a problem lends itself to a time averaging approach, |
193 |
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the Molecular Dynamics techniques in Sec.~\ref{introSec:MD} can be |
194 |
+ |
employed. |
195 |
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|
196 |
+ |
\section{\label{introSec:monteCarlo}Monte Carlo Simulations} |
197 |
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|
198 |
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The Monte Carlo method was developed by Metropolis and Ulam for their |
199 |
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work in fissionable material.\cite{metropolis:1949} The method is so |
200 |
< |
named, because it heavily uses random numbers in the solution of the |
201 |
< |
problem. |
200 |
> |
named, because it heavily uses random numbers in its |
201 |
> |
solution.\cite{allen87:csl} The Monte Carlo method allows for the |
202 |
> |
solution of integrals through the stochastic sampling of the values |
203 |
> |
within the integral. In the simplest case, the evaluation of an |
204 |
> |
integral would follow a brute force method of |
205 |
> |
sampling.\cite{Frenkel1996} Consider the following single dimensional |
206 |
> |
integral: |
207 |
> |
\begin{equation} |
208 |
> |
I = f(x)dx |
209 |
> |
\label{eq:MCex1} |
210 |
> |
\end{equation} |
211 |
> |
The equation can be recast as: |
212 |
> |
\begin{equation} |
213 |
> |
I = (b-a)\langle f(x) \rangle |
214 |
> |
\label{eq:MCex2} |
215 |
> |
\end{equation} |
216 |
> |
Where $\langle f(x) \rangle$ is the unweighted average over the interval |
217 |
> |
$[a,b]$. The calculation of the integral could then be solved by |
218 |
> |
randomly choosing points along the interval $[a,b]$ and calculating |
219 |
> |
the value of $f(x)$ at each point. The accumulated average would then |
220 |
> |
approach $I$ in the limit where the number of trials is infintely |
221 |
> |
large. |
222 |
|
|
223 |
+ |
However, in Statistical Mechanics, one is typically interested in |
224 |
+ |
integrals of the form: |
225 |
+ |
\begin{equation} |
226 |
+ |
\langle A \rangle = \frac{\int d^N \mathbf{r}~A(\mathbf{r}^N)% |
227 |
+ |
e^{-\beta V(\mathbf{r}^N)}}% |
228 |
+ |
{\int d^N \mathbf{r}~e^{-\beta V(\mathbf{r}^N)}} |
229 |
+ |
\label{eq:mcEnsAvg} |
230 |
+ |
\end{equation} |
231 |
+ |
Where $\mathbf{r}^N$ stands for the coordinates of all $N$ particles |
232 |
+ |
and $A$ is some observable that is only dependent on position. This is |
233 |
+ |
the ensemble average of $A$ as presented in |
234 |
+ |
Sec.~\ref{introSec:statThermo}, except here $A$ is independent of |
235 |
+ |
momentum. Therefore the momenta contribution of the integral can be |
236 |
+ |
factored out, leaving the configurational integral. Application of the |
237 |
+ |
brute force method to this system would yield highly inefficient |
238 |
+ |
results. Due to the Boltzman weighting of this integral, most random |
239 |
+ |
configurations will have a near zero contribution to the ensemble |
240 |
+ |
average. This is where importance sampling comes into |
241 |
+ |
play.\cite{allen87:csl} |
242 |
|
|
243 |
< |
\subsection{\label{introSec:md}Molecular Dynamics Simulations} |
243 |
> |
Importance Sampling is a method where one selects a distribution from |
244 |
> |
which the random configurations are chosen in order to more |
245 |
> |
efficiently calculate the integral.\cite{Frenkel1996} Consider again |
246 |
> |
Eq.~\ref{eq:MCex1} rewritten to be: |
247 |
> |
\begin{equation} |
248 |
> |
I = \int^b_a \frac{f(x)}{\rho(x)} \rho(x) dx |
249 |
> |
\label{introEq:Importance1} |
250 |
> |
\end{equation} |
251 |
> |
Where $\rho(x)$ is an arbitrary probability distribution in $x$. If |
252 |
> |
one conducts $\tau$ trials selecting a random number, $\zeta_\tau$, |
253 |
> |
from the distribution $\rho(x)$ on the interval $[a,b]$, then |
254 |
> |
Eq.~\ref{introEq:Importance1} becomes |
255 |
> |
\begin{equation} |
256 |
> |
I= \biggl \langle \frac{f(x)}{\rho(x)} \biggr \rangle_{\text{trials}} |
257 |
> |
\label{introEq:Importance2} |
258 |
> |
\end{equation} |
259 |
> |
Looking at Eq.~\ref{eq:mcEnsAvg}, and realizing |
260 |
> |
\begin {equation} |
261 |
> |
\rho_{kT}(\mathbf{r}^N) = |
262 |
> |
\frac{e^{-\beta V(\mathbf{r}^N)}} |
263 |
> |
{\int d^N \mathbf{r}~e^{-\beta V(\mathbf{r}^N)}} |
264 |
> |
\label{introEq:MCboltzman} |
265 |
> |
\end{equation} |
266 |
> |
Where $\rho_{kT}$ is the boltzman distribution. The ensemble average |
267 |
> |
can be rewritten as |
268 |
> |
\begin{equation} |
269 |
> |
\langle A \rangle = \int d^N \mathbf{r}~A(\mathbf{r}^N) |
270 |
> |
\rho_{kT}(\mathbf{r}^N) |
271 |
> |
\label{introEq:Importance3} |
272 |
> |
\end{equation} |
273 |
> |
Applying Eq.~\ref{introEq:Importance1} one obtains |
274 |
> |
\begin{equation} |
275 |
> |
\langle A \rangle = \biggl \langle |
276 |
> |
\frac{ A \rho_{kT}(\mathbf{r}^N) } |
277 |
> |
{\rho(\mathbf{r}^N)} \biggr \rangle_{\text{trials}} |
278 |
> |
\label{introEq:Importance4} |
279 |
> |
\end{equation} |
280 |
> |
By selecting $\rho(\mathbf{r}^N)$ to be $\rho_{kT}(\mathbf{r}^N)$ |
281 |
> |
Eq.~\ref{introEq:Importance4} becomes |
282 |
> |
\begin{equation} |
283 |
> |
\langle A \rangle = \langle A(\mathbf{r}^N) \rangle_{\text{trials}} |
284 |
> |
\label{introEq:Importance5} |
285 |
> |
\end{equation} |
286 |
> |
The difficulty is selecting points $\mathbf{r}^N$ such that they are |
287 |
> |
sampled from the distribution $\rho_{kT}(\mathbf{r}^N)$. A solution |
288 |
> |
was proposed by Metropolis et al.\cite{metropolis:1953} which involved |
289 |
> |
the use of a Markov chain whose limiting distribution was |
290 |
> |
$\rho_{kT}(\mathbf{r}^N)$. |
291 |
|
|
292 |
< |
time averages |
292 |
> |
\subsection{\label{introSec:markovChains}Markov Chains} |
293 |
|
|
294 |
< |
time integrating schemes |
294 |
> |
A Markov chain is a chain of states satisfying the following |
295 |
> |
conditions:\cite{leach01:mm} |
296 |
> |
\begin{enumerate} |
297 |
> |
\item The outcome of each trial depends only on the outcome of the previous trial. |
298 |
> |
\item Each trial belongs to a finite set of outcomes called the state space. |
299 |
> |
\end{enumerate} |
300 |
> |
If given two configuartions, $\mathbf{r}^N_m$ and $\mathbf{r}^N_n$, |
301 |
> |
$\rho_m$ and $\rho_n$ are the probablilities of being in state |
302 |
> |
$\mathbf{r}^N_m$ and $\mathbf{r}^N_n$ respectively. Further, the two |
303 |
> |
states are linked by a transition probability, $\pi_{mn}$, which is the |
304 |
> |
probability of going from state $m$ to state $n$. |
305 |
|
|
306 |
< |
time reversible |
306 |
> |
\newcommand{\accMe}{\operatorname{acc}} |
307 |
|
|
308 |
< |
symplectic methods |
308 |
> |
The transition probability is given by the following: |
309 |
> |
\begin{equation} |
310 |
> |
\pi_{mn} = \alpha_{mn} \times \accMe(m \rightarrow n) |
311 |
> |
\label{introEq:MCpi} |
312 |
> |
\end{equation} |
313 |
> |
Where $\alpha_{mn}$ is the probability of attempting the move $m |
314 |
> |
\rightarrow n$, and $\accMe$ is the probability of accepting the move |
315 |
> |
$m \rightarrow n$. Defining a probability vector, |
316 |
> |
$\boldsymbol{\rho}$, such that |
317 |
> |
\begin{equation} |
318 |
> |
\boldsymbol{\rho} = \{\rho_1, \rho_2, \ldots \rho_m, \rho_n, |
319 |
> |
\ldots \rho_N \} |
320 |
> |
\label{introEq:MCrhoVector} |
321 |
> |
\end{equation} |
322 |
> |
a transition matrix $\boldsymbol{\Pi}$ can be defined, |
323 |
> |
whose elements are $\pi_{mn}$, for each given transition. The |
324 |
> |
limiting distribution of the Markov chain can then be found by |
325 |
> |
applying the transition matrix an infinite number of times to the |
326 |
> |
distribution vector. |
327 |
> |
\begin{equation} |
328 |
> |
\boldsymbol{\rho}_{\text{limit}} = |
329 |
> |
\lim_{N \rightarrow \infty} \boldsymbol{\rho}_{\text{initial}} |
330 |
> |
\boldsymbol{\Pi}^N |
331 |
> |
\label{introEq:MCmarkovLimit} |
332 |
> |
\end{equation} |
333 |
> |
The limiting distribution of the chain is independent of the starting |
334 |
> |
distribution, and successive applications of the transition matrix |
335 |
> |
will only yield the limiting distribution again. |
336 |
> |
\begin{equation} |
337 |
> |
\boldsymbol{\rho}_{\text{limit}} = \boldsymbol{\rho}_{\text{initial}} |
338 |
> |
\boldsymbol{\Pi} |
339 |
> |
\label{introEq:MCmarkovEquil} |
340 |
> |
\end{equation} |
341 |
|
|
342 |
< |
Extended ensembles (NVT NPT) |
342 |
> |
\subsection{\label{introSec:metropolisMethod}The Metropolis Method} |
343 |
|
|
344 |
< |
constrained dynamics |
344 |
> |
In the Metropolis method\cite{metropolis:1953} |
345 |
> |
Eq.~\ref{introEq:MCmarkovEquil} is solved such that |
346 |
> |
$\boldsymbol{\rho}_{\text{limit}}$ matches the Boltzman distribution |
347 |
> |
of states. The method accomplishes this by imposing the strong |
348 |
> |
condition of microscopic reversibility on the equilibrium |
349 |
> |
distribution. Meaning, that at equilibrium the probability of going |
350 |
> |
from $m$ to $n$ is the same as going from $n$ to $m$. |
351 |
> |
\begin{equation} |
352 |
> |
\rho_m\pi_{mn} = \rho_n\pi_{nm} |
353 |
> |
\label{introEq:MCmicroReverse} |
354 |
> |
\end{equation} |
355 |
> |
Further, $\boldsymbol{\alpha}$ is chosen to be a symetric matrix in |
356 |
> |
the Metropolis method. Using Eq.~\ref{introEq:MCpi}, |
357 |
> |
Eq.~\ref{introEq:MCmicroReverse} becomes |
358 |
> |
\begin{equation} |
359 |
> |
\frac{\accMe(m \rightarrow n)}{\accMe(n \rightarrow m)} = |
360 |
> |
\frac{\rho_n}{\rho_m} |
361 |
> |
\label{introEq:MCmicro2} |
362 |
> |
\end{equation} |
363 |
> |
For a Boltxman limiting distribution, |
364 |
> |
\begin{equation} |
365 |
> |
\frac{\rho_n}{\rho_m} = e^{-\beta[\mathcal{U}(n) - \mathcal{U}(m)]} |
366 |
> |
= e^{-\beta \Delta \mathcal{U}} |
367 |
> |
\label{introEq:MCmicro3} |
368 |
> |
\end{equation} |
369 |
> |
This allows for the following set of acceptance rules be defined: |
370 |
> |
\begin{equation} |
371 |
> |
\accMe( m \rightarrow n ) = |
372 |
> |
\begin{cases} |
373 |
> |
1& \text{if $\Delta \mathcal{U} \leq 0$,} \\ |
374 |
> |
e^{-\beta \Delta \mathcal{U}}& \text{if $\Delta \mathcal{U} > 0$.} |
375 |
> |
\end{cases} |
376 |
> |
\label{introEq:accRules} |
377 |
> |
\end{equation} |
378 |
|
|
379 |
< |
\section{\label{introSec:chapterLayout}Chapter Layout} |
379 |
> |
Using the acceptance criteria from Eq.~\ref{introEq:accRules} the |
380 |
> |
Metropolis method proceeds as follows |
381 |
> |
\begin{enumerate} |
382 |
> |
\item Generate an initial configuration $\mathbf{r}^N$ which has some finite probability in $\rho_{kT}$. |
383 |
> |
\item Modify $\mathbf{r}^N$, to generate configuratioon $\mathbf{r^{\prime}}^N$. |
384 |
> |
\item If the new configuration lowers the energy of the system, accept the move with unity ($\mathbf{r}^N$ becomes $\mathbf{r^{\prime}}^N$). Otherwise accept with probability $e^{-\beta \Delta \mathcal{U}}$. |
385 |
> |
\item Accumulate the average for the configurational observable of intereest. |
386 |
> |
\item Repeat from step 2 until the average converges. |
387 |
> |
\end{enumerate} |
388 |
> |
One important note is that the average is accumulated whether the move |
389 |
> |
is accepted or not, this ensures proper weighting of the average. |
390 |
> |
Using Eq.~\ref{introEq:Importance4} it becomes clear that the |
391 |
> |
accumulated averages are the ensemble averages, as this method ensures |
392 |
> |
that the limiting distribution is the Boltzman distribution. |
393 |
|
|
394 |
< |
\subsection{\label{introSec:RSA}Random Sequential Adsorption} |
394 |
> |
\section{\label{introSec:MD}Molecular Dynamics Simulations} |
395 |
|
|
396 |
< |
\subsection{\label{introSec:OOPSE}The OOPSE Simulation Package} |
396 |
> |
The main simulation tool used in this research is Molecular Dynamics. |
397 |
> |
Molecular Dynamics is when the equations of motion for a system are |
398 |
> |
integrated in order to obtain information about both the positions and |
399 |
> |
momentum of a system, allowing the calculation of not only |
400 |
> |
configurational observables, but momenta dependent ones as well: |
401 |
> |
diffusion constants, velocity auto correlations, folding/unfolding |
402 |
> |
events, etc. Due to the principle of ergodicity, |
403 |
> |
Sec.~\ref{introSec:ergodic}, the average of these observables over the |
404 |
> |
time period of the simulation are taken to be the ensemble averages |
405 |
> |
for the system. |
406 |
|
|
407 |
< |
\subsection{\label{introSec:bilayers}A Mesoscale Model for Phospholipid Bilayers} |
407 |
> |
The choice of when to use molecular dynamics over Monte Carlo |
408 |
> |
techniques, is normally decided by the observables in which the |
409 |
> |
researcher is interested. If the observables depend on momenta in |
410 |
> |
any fashion, then the only choice is molecular dynamics in some form. |
411 |
> |
However, when the observable is dependent only on the configuration, |
412 |
> |
then most of the time Monte Carlo techniques will be more efficent. |
413 |
> |
|
414 |
> |
The focus of research in the second half of this dissertation is |
415 |
> |
centered around the dynamic properties of phospholipid bilayers, |
416 |
> |
making molecular dynamics key in the simulation of those properties. |
417 |
> |
|
418 |
> |
\subsection{\label{introSec:mdAlgorithm}The Molecular Dynamics Algorithm} |
419 |
> |
|
420 |
> |
To illustrate how the molecular dynamics technique is applied, the |
421 |
> |
following sections will describe the sequence involved in a |
422 |
> |
simulation. Sec.~\ref{introSec:mdInit} deals with the initialization |
423 |
> |
of a simulation. Sec.~\ref{introSec:mdForce} discusses issues |
424 |
> |
involved with the calculation of the forces. |
425 |
> |
Sec.~\ref{introSec:mdIntegrate} concludes the algorithm discussion |
426 |
> |
with the integration of the equations of motion.\cite{Frenkel1996} |
427 |
> |
|
428 |
> |
\subsection{\label{introSec:mdInit}Initialization} |
429 |
> |
|
430 |
> |
When selecting the initial configuration for the simulation it is |
431 |
> |
important to consider what dynamics one is hoping to observe. |
432 |
> |
Ch.~\ref{chapt:lipid} deals with the formation and equilibrium dynamics of |
433 |
> |
phospholipid membranes. Therefore in these simulations initial |
434 |
> |
positions were selected that in some cases dispersed the lipids in |
435 |
> |
water, and in other cases structured the lipids into preformed |
436 |
> |
bilayers. Important considerations at this stage of the simulation are: |
437 |
> |
\begin{itemize} |
438 |
> |
\item There are no major overlaps of molecular or atomic orbitals |
439 |
> |
\item Velocities are chosen in such a way as to not gie the system a non=zero total momentum or angular momentum. |
440 |
> |
\item It is also sometimes desireable to select the velocities to correctly sample the target temperature. |
441 |
> |
\end{itemize} |
442 |
> |
|
443 |
> |
The first point is important due to the amount of potential energy |
444 |
> |
generated by having two particles too close together. If overlap |
445 |
> |
occurs, the first evaluation of forces will return numbers so large as |
446 |
> |
to render the numerical integration of teh motion meaningless. The |
447 |
> |
second consideration keeps the system from drifting or rotating as a |
448 |
> |
whole. This arises from the fact that most simulations are of systems |
449 |
> |
in equilibrium in the absence of outside forces. Therefore any net |
450 |
> |
movement would be unphysical and an artifact of the simulation method |
451 |
> |
used. The final point addresses the selection of the magnitude of the |
452 |
> |
initial velocities. For many simulations it is convienient to use |
453 |
> |
this opportunity to scale the amount of kinetic energy to reflect the |
454 |
> |
desired thermal distribution of the system. However, it must be noted |
455 |
> |
that most systems will require further velocity rescaling after the |
456 |
> |
first few initial simulation steps due to either loss or gain of |
457 |
> |
kinetic energy from energy stored in potential degrees of freedom. |
458 |
> |
|
459 |
> |
\subsection{\label{introSec:mdForce}Force Evaluation} |
460 |
> |
|
461 |
> |
The evaluation of forces is the most computationally expensive portion |
462 |
> |
of a given molecular dynamics simulation. This is due entirely to the |
463 |
> |
evaluation of long range forces in a simulation, typically pair-wise. |
464 |
> |
These forces are most commonly the Van der Waals force, and sometimes |
465 |
> |
Coulombic forces as well. For a pair-wise force, there are $N(N-1)/ 2$ |
466 |
> |
pairs to be evaluated, where $N$ is the number of particles in the |
467 |
> |
system. This leads to the calculations scaling as $N^2$, making large |
468 |
> |
simulations prohibitive in the absence of any computation saving |
469 |
> |
techniques. |
470 |
> |
|
471 |
> |
Another consideration one must resolve, is that in a given simulation |
472 |
> |
a disproportionate number of the particles will feel the effects of |
473 |
> |
the surface.\cite{allen87:csl} For a cubic system of 1000 particles |
474 |
> |
arranged in a $10 \times 10 \times 10$ cube, 488 particles will be |
475 |
> |
exposed to the surface. Unless one is simulating an isolated particle |
476 |
> |
group in a vacuum, the behavior of the system will be far from the |
477 |
> |
desired bulk charecteristics. To offset this, simulations employ the |
478 |
> |
use of periodic boundary images.\cite{born:1912} |
479 |
> |
|
480 |
> |
The technique involves the use of an algorithm that replicates the |
481 |
> |
simulation box on an infinite lattice in cartesian space. Any given |
482 |
> |
particle leaving the simulation box on one side will have an image of |
483 |
> |
itself enter on the opposite side (see Fig.~\ref{introFig:pbc}). In |
484 |
> |
addition, this sets that any given particle pair has an image, real or |
485 |
> |
periodic, within $fix$ of each other. A discussion of the method used |
486 |
> |
to calculate the periodic image can be found in |
487 |
> |
Sec.\ref{oopseSec:pbc}. |
488 |
> |
|
489 |
> |
\begin{figure} |
490 |
> |
\centering |
491 |
> |
\includegraphics[width=\linewidth]{pbcFig.eps} |
492 |
> |
\caption[An illustration of periodic boundry conditions]{A 2-D illustration of periodic boundry conditions. As one particle leaves the right of the simulation box, an image of it enters the left.} |
493 |
> |
\label{introFig:pbc} |
494 |
> |
\end{figure} |
495 |
> |
|
496 |
> |
Returning to the topic of the computational scale of the force |
497 |
> |
evaluation, the use of periodic boundary conditions requires that a |
498 |
> |
cutoff radius be employed. Using a cutoff radius improves the |
499 |
> |
efficiency of the force evaluation, as particles farther than a |
500 |
> |
predetermined distance, $r_{\text{cut}}$, are not included in the |
501 |
> |
calculation.\cite{Frenkel1996} In a simultation with periodic images, |
502 |
> |
$r_{\text{cut}}$ has a maximum value of $\text{box}/2$. |
503 |
> |
Fig.~\ref{introFig:rMax} illustrates how when using an |
504 |
> |
$r_{\text{cut}}$ larger than this value, or in the extreme limit of no |
505 |
> |
$r_{\text{cut}}$ at all, the corners of the simulation box are |
506 |
> |
unequally weighted due to the lack of particle images in the $x$, $y$, |
507 |
> |
or $z$ directions past a disance of $\text{box} / 2$. |
508 |
> |
|
509 |
> |
\begin{figure} |
510 |
> |
\centering |
511 |
> |
\includegraphics[width=\linewidth]{rCutMaxFig.eps} |
512 |
> |
\caption |
513 |
> |
\label{introFig:rMax} |
514 |
> |
\end{figure} |
515 |
> |
|
516 |
> |
With the use of an $fix$, however, comes a discontinuity in the |
517 |
> |
potential energy curve (Fig.~\ref{fix}). To fix this discontinuity, |
518 |
> |
one calculates the potential energy at the $r_{\text{cut}}$, and add |
519 |
> |
that value to the potential. This causes the function to go smoothly |
520 |
> |
to zero at the cutoff radius. This ensures conservation of energy |
521 |
> |
when integrating the Newtonian equations of motion. |
522 |
> |
|
523 |
> |
The second main simplification used in this research is the Verlet |
524 |
> |
neighbor list. \cite{allen87:csl} In the Verlet method, one generates |
525 |
> |
a list of all neighbor atoms, $j$, surrounding atom $i$ within some |
526 |
> |
cutoff $r_{\text{list}}$, where $r_{\text{list}}>r_{\text{cut}}$. |
527 |
> |
This list is created the first time forces are evaluated, then on |
528 |
> |
subsequent force evaluations, pair calculations are only calculated |
529 |
> |
from the neighbor lists. The lists are updated if any given particle |
530 |
> |
in the system moves farther than $r_{\text{list}}-r_{\text{cut}}$, |
531 |
> |
giving rise to the possibility that a particle has left or joined a |
532 |
> |
neighbor list. |
533 |
> |
|
534 |
> |
\subsection{\label{introSec:mdIntegrate} Integration of the equations of motion} |
535 |
> |
|
536 |
> |
A starting point for the discussion of molecular dynamics integrators |
537 |
> |
is the Verlet algorithm. \cite{Frenkel1996} It begins with a Taylor |
538 |
> |
expansion of position in time: |
539 |
> |
\begin{equation} |
540 |
> |
eq here |
541 |
> |
\label{introEq:verletForward} |
542 |
> |
\end{equation} |
543 |
> |
As well as, |
544 |
> |
\begin{equation} |
545 |
> |
eq here |
546 |
> |
\label{introEq:verletBack} |
547 |
> |
\end{equation} |
548 |
> |
Adding together Eq.~\ref{introEq:verletForward} and |
549 |
> |
Eq.~\ref{introEq:verletBack} results in, |
550 |
> |
\begin{equation} |
551 |
> |
eq here |
552 |
> |
\label{introEq:verletSum} |
553 |
> |
\end{equation} |
554 |
> |
Or equivalently, |
555 |
> |
\begin{equation} |
556 |
> |
eq here |
557 |
> |
\label{introEq:verletFinal} |
558 |
> |
\end{equation} |
559 |
> |
Which contains an error in the estimate of the new positions on the |
560 |
> |
order of $\Delta t^4$. |
561 |
> |
|
562 |
> |
In practice, however, the simulations in this research were integrated |
563 |
> |
with a velocity reformulation of teh Verlet method.\cite{allen87:csl} |
564 |
> |
\begin{equation} |
565 |
> |
eq here |
566 |
> |
\label{introEq:MDvelVerletPos} |
567 |
> |
\end{equation} |
568 |
> |
\begin{equation} |
569 |
> |
eq here |
570 |
> |
\label{introEq:MDvelVerletVel} |
571 |
> |
\end{equation} |
572 |
> |
The original Verlet algorithm can be regained by substituting the |
573 |
> |
velocity back into Eq.~\ref{introEq:MDvelVerletPos}. The Verlet |
574 |
> |
formulations are chosen in this research because the algorithms have |
575 |
> |
very little long term drift in energy conservation. Energy |
576 |
> |
conservation in a molecular dynamics simulation is of extreme |
577 |
> |
importance, as it is a measure of how closely one is following the |
578 |
> |
``true'' trajectory wtih the finite integration scheme. An exact |
579 |
> |
solution to the integration will conserve area in phase space, as well |
580 |
> |
as be reversible in time, that is, the trajectory integrated forward |
581 |
> |
or backwards will exactly match itself. Having a finite algorithm |
582 |
> |
that both conserves area in phase space and is time reversible, |
583 |
> |
therefore increases, but does not guarantee the ``correctness'' or the |
584 |
> |
integrated trajectory. |
585 |
> |
|
586 |
> |
It can be shown,\cite{Frenkel1996} that although the Verlet algorithm |
587 |
> |
does not rigorously preserve the actual Hamiltonian, it does preserve |
588 |
> |
a pseudo-Hamiltonian which shadows the real one in phase space. This |
589 |
> |
pseudo-Hamiltonian is proveably area-conserving as well as time |
590 |
> |
reversible. The fact that it shadows the true Hamiltonian in phase |
591 |
> |
space is acceptable in actual simulations as one is interested in the |
592 |
> |
ensemble average of the observable being measured. From the ergodic |
593 |
> |
hypothesis (Sec.~\ref{introSec:StatThermo}), it is known that the time |
594 |
> |
average will match the ensemble average, therefore two similar |
595 |
> |
trajectories in phase space should give matching statistical averages. |
596 |
> |
|
597 |
> |
\subsection{\label{introSec:MDfurther}Further Considerations} |
598 |
> |
In the simulations presented in this research, a few additional |
599 |
> |
parameters are needed to describe the motions. The simulations |
600 |
> |
involving water and phospholipids in Chapt.~\ref{chaptLipids} are |
601 |
> |
required to integrate the equations of motions for dipoles on atoms. |
602 |
> |
This involves an additional three parameters be specified for each |
603 |
> |
dipole atom: $\phi$, $\theta$, and $\psi$. These three angles are |
604 |
> |
taken to be the Euler angles, where $\phi$ is a rotation about the |
605 |
> |
$z$-axis, and $\theta$ is a rotation about the new $x$-axis, and |
606 |
> |
$\psi$ is a final rotation about the new $z$-axis (see |
607 |
> |
Fig.~\ref{introFig:euleerAngles}). This sequence of rotations can be |
608 |
> |
accumulated into a single $3 \times 3$ matrix $\mathbf{A}$ |
609 |
> |
defined as follows: |
610 |
> |
\begin{equation} |
611 |
> |
eq here |
612 |
> |
\label{introEq:EulerRotMat} |
613 |
> |
\end{equation} |
614 |
> |
|
615 |
> |
The equations of motion for Euler angles can be written down as |
616 |
> |
\cite{allen87:csl} |
617 |
> |
\begin{equation} |
618 |
> |
eq here |
619 |
> |
\label{introEq:MDeuleeerPsi} |
620 |
> |
\end{equation} |
621 |
> |
Where $\omega^s_i$ is the angular velocity in the lab space frame |
622 |
> |
along cartesian coordinate $i$. However, a difficulty arises when |
623 |
> |
attempting to integrate Eq.~\ref{introEq:MDeulerPhi} and |
624 |
> |
Eq.~\ref{introEq:MDeulerPsi}. The $\frac{1}{\sin \theta}$ present in |
625 |
> |
both equations means there is a non-physical instability present when |
626 |
> |
$\theta$ is 0 or $\pi$. |
627 |
> |
|
628 |
> |
To correct for this, the simulations integrate the rotation matrix, |
629 |
> |
$\mathbf{A}$, directly, thus avoiding the instability. |
630 |
> |
This method was proposed by Dullwebber |
631 |
> |
\emph{et. al.}\cite{Dullwebber:1997}, and is presented in |
632 |
> |
Sec.~\ref{introSec:MDsymplecticRot}. |
633 |
> |
|
634 |
> |
\subsubsection{\label{introSec:MDliouville}Liouville Propagator} |
635 |
> |
|
636 |
> |
Before discussing the integration of the rotation matrix, it is |
637 |
> |
necessary to understand the construction of a ``good'' integration |
638 |
> |
scheme. It has been previously |
639 |
> |
discussed(Sec.~\ref{introSec:MDintegrate}) how it is desirable for an |
640 |
> |
integrator to be symplectic, or time reversible. The following is an |
641 |
> |
outline of the Trotter factorization of the Liouville Propagator as a |
642 |
> |
scheme for generating symplectic integrators. \cite{Tuckerman:1992} |
643 |
> |
|
644 |
> |
For a system with $f$ degrees of freedom the Liouville operator can be |
645 |
> |
defined as, |
646 |
> |
\begin{equation} |
647 |
> |
eq here |
648 |
> |
\label{introEq:LiouvilleOperator} |
649 |
> |
\end{equation} |
650 |
> |
Here, $r_j$ and $p_j$ are the position and conjugate momenta of a |
651 |
> |
degree of freedom, and $f_j$ is the force on that degree of freedom. |
652 |
> |
$\Gamma$ is defined as the set of all positions nad conjugate momenta, |
653 |
> |
$\{r_j,p_j\}$, and the propagator, $U(t)$, is defined |
654 |
> |
\begin {equation} |
655 |
> |
eq here |
656 |
> |
\label{introEq:Lpropagator} |
657 |
> |
\end{equation} |
658 |
> |
This allows the specification of $\Gamma$ at any time $t$ as |
659 |
> |
\begin{equation} |
660 |
> |
eq here |
661 |
> |
\label{introEq:Lp2} |
662 |
> |
\end{equation} |
663 |
> |
It is important to note, $U(t)$ is a unitary operator meaning |
664 |
> |
\begin{equation} |
665 |
> |
U(-t)=U^{-1}(t) |
666 |
> |
\label{introEq:Lp3} |
667 |
> |
\end{equation} |
668 |
> |
|
669 |
> |
Decomposing $L$ into two parts, $iL_1$ and $iL_2$, one can use the |
670 |
> |
Trotter theorem to yield |
671 |
> |
\begin{equation} |
672 |
> |
eq here |
673 |
> |
\label{introEq:Lp4} |
674 |
> |
\end{equation} |
675 |
> |
Where $\Delta t = \frac{t}{P}$. |
676 |
> |
With this, a discrete time operator $G(\Delta t)$ can be defined: |
677 |
> |
\begin{equation} |
678 |
> |
eq here |
679 |
> |
\label{introEq:Lp5} |
680 |
> |
\end{equation} |
681 |
> |
Because $U_1(t)$ and $U_2(t)$ are unitary, $G|\Delta t)$ is also |
682 |
> |
unitary. Meaning an integrator based on this factorization will be |
683 |
> |
reversible in time. |
684 |
> |
|
685 |
> |
As an example, consider the following decomposition of $L$: |
686 |
> |
\begin{equation} |
687 |
> |
eq here |
688 |
> |
\label{introEq:Lp6} |
689 |
> |
\end{equation} |
690 |
> |
Operating $G(\Delta t)$ on $\Gamma)0)$, and utilizing the operator property |
691 |
> |
\begin{equation} |
692 |
> |
eq here |
693 |
> |
\label{introEq:Lp8} |
694 |
> |
\end{equation} |
695 |
> |
Where $c$ is independent of $q$. One obtains the following: |
696 |
> |
\begin{equation} |
697 |
> |
eq here |
698 |
> |
\label{introEq:Lp8} |
699 |
> |
\end{equation} |
700 |
> |
Or written another way, |
701 |
> |
\begin{equation} |
702 |
> |
eq here |
703 |
> |
\label{intorEq:Lp9} |
704 |
> |
\end{equation} |
705 |
> |
This is the velocity Verlet formulation presented in |
706 |
> |
Sec.~\ref{introSec:MDintegrate}. Because this integration scheme is |
707 |
> |
comprised of unitary propagators, it is symplectic, and therefore area |
708 |
> |
preserving in phase space. From the preceeding fatorization, one can |
709 |
> |
see that the integration of the equations of motion would follow: |
710 |
> |
\begin{enumerate} |
711 |
> |
\item calculate the velocities at the half step, $\frac{\Delta t}{2}$, from the forces calculated at the initial position. |
712 |
> |
|
713 |
> |
\item Use the half step velocities to move positions one whole step, $\Delta t$. |
714 |
> |
|
715 |
> |
\item Evaluate the forces at the new positions, $\mathbf{r}(\Delta t)$, and use the new forces to complete the velocity move. |
716 |
> |
|
717 |
> |
\item Repeat from step 1 with the new position, velocities, and forces assuming the roles of the initial values. |
718 |
> |
\end{enumerate} |
719 |
> |
|
720 |
> |
\subsubsection{\label{introSec:MDsymplecticRot} Symplectic Propagation of the Rotation Matrix} |
721 |
> |
|
722 |
> |
Based on the factorization from the previous section, |
723 |
> |
Dullweber\emph{et al.}\cite{Dullweber:1997}~ proposed a scheme for the |
724 |
> |
symplectic propagation of the rotation matrix, $\mathbf{A}$, as an |
725 |
> |
alternative method for the integration of orientational degrees of |
726 |
> |
freedom. The method starts with a straightforward splitting of the |
727 |
> |
Liouville operator: |
728 |
> |
\begin{equation} |
729 |
> |
eq here |
730 |
> |
\label{introEq:SR1} |
731 |
> |
\end{equation} |
732 |
> |
Where $\boldsymbol{\tau}(\mathbf{A})$ are the tourques of the system |
733 |
> |
due to the configuration, and $\boldsymbol{/pi}$ are the conjugate |
734 |
> |
angular momenta of the system. The propagator, $G(\Delta t)$, becomes |
735 |
> |
\begin{equation} |
736 |
> |
eq here |
737 |
> |
\label{introEq:SR2} |
738 |
> |
\end{equation} |
739 |
> |
Propagation fo the linear and angular momenta follows as in the Verlet |
740 |
> |
scheme. The propagation of positions also follows the verlet scheme |
741 |
> |
with the addition of a further symplectic splitting of the rotation |
742 |
> |
matrix propagation, $\mathcal{G}_{\text{rot}}(\Delta t)$. |
743 |
> |
\begin{equation} |
744 |
> |
eq here |
745 |
> |
\label{introEq:SR3} |
746 |
> |
\end{equation} |
747 |
> |
Where $\mathcal{G}_j$ is a unitary rotation of $\mathbf{A}$ and |
748 |
> |
$\boldsymbol{\pi}$ about each axis $j$. As all propagations are now |
749 |
> |
unitary and symplectic, the entire integration scheme is also |
750 |
> |
symplectic and time reversible. |
751 |
> |
|
752 |
> |
\section{\label{introSec:layout}Dissertation Layout} |
753 |
> |
|
754 |
> |
This dissertation is divided as follows:Chapt.~\ref{chapt:RSA} |
755 |
> |
presents the random sequential adsorption simulations of related |
756 |
> |
pthalocyanines on a gold (111) surface. Chapt.~\ref{chapt:OOPSE} |
757 |
> |
is about the writing of the molecular dynamics simulation package |
758 |
> |
{\sc oopse}, Chapt.~\ref{chapt:lipid} regards the simulations of |
759 |
> |
phospholipid bilayers using a mesoscale model, and lastly, |
760 |
> |
Chapt.~\ref{chapt:conclusion} concludes this dissertation with a |
761 |
> |
summary of all results. The chapters are arranged in chronological |
762 |
> |
order, and reflect the progression of techniques I employed during my |
763 |
> |
research. |
764 |
> |
|
765 |
> |
The chapter concerning random sequential adsorption |
766 |
> |
simulations is a study in applying the principles of theoretical |
767 |
> |
research in order to obtain a simple model capaable of explaining the |
768 |
> |
results. My advisor, Dr. Gezelter, and I were approached by a |
769 |
> |
colleague, Dr. Lieberman, about possible explanations for partial |
770 |
> |
coverge of a gold surface by a particular compound of hers. We |
771 |
> |
suggested it might be due to the statistical packing fraction of disks |
772 |
> |
on a plane, and set about to simulate this system. As the events in |
773 |
> |
our model were not dynamic in nature, a Monte Carlo method was |
774 |
> |
emplyed. Here, if a molecule landed on the surface without |
775 |
> |
overlapping another, then its landing was accepted. However, if there |
776 |
> |
was overlap, the landing we rejected and a new random landing location |
777 |
> |
was chosen. This defined our acceptance rules and allowed us to |
778 |
> |
construct a Markov chain whose limiting distribution was the surface |
779 |
> |
coverage in which we were interested. |
780 |
> |
|
781 |
> |
The following chapter, about the simulation package {\sc oopse}, |
782 |
> |
describes in detail the large body of scientific code that had to be |
783 |
> |
written in order to study phospholipid bilayer. Although there are |
784 |
> |
pre-existing molecular dynamic simulation packages available, none |
785 |
> |
were capable of implementing the models we were developing.{\sc oopse} |
786 |
> |
is a unique package capable of not only integrating the equations of |
787 |
> |
motion in cartesian space, but is also able to integrate the |
788 |
> |
rotational motion of rigid bodies and dipoles. Add to this the |
789 |
> |
ability to perform calculations across parallel processors and a |
790 |
> |
flexible script syntax for creating systems, and {\sc oopse} becomes a |
791 |
> |
very powerful scientific instrument for the exploration of our model. |
792 |
> |
|
793 |
> |
Bringing us to Chapt.~\ref{chapt:lipid}. Using {\sc oopse}, I have been |
794 |
> |
able to parametrize a mesoscale model for phospholipid simulations. |
795 |
> |
This model retains information about solvent ordering about the |
796 |
> |
bilayer, as well as information regarding the interaction of the |
797 |
> |
phospholipid head groups' dipole with each other and the surrounding |
798 |
> |
solvent. These simulations give us insight into the dynamic events |
799 |
> |
that lead to the formation of phospholipid bilayers, as well as |
800 |
> |
provide the foundation for future exploration of bilayer phase |
801 |
> |
behavior with this model. |
802 |
> |
|
803 |
> |
Which leads into the last chapter, where I discuss future directions |
804 |
> |
for both{\sc oopse} and this mesoscale model. Additionally, I will |
805 |
> |
give a summary of results for this dissertation. |
806 |
> |
|
807 |
> |
|