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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 |
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Carlo. Molecular Dynamic simulations integrate the equations of motion |
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for a given system of particles, allowing the researher to gain |
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for a given system of particles, allowing the researcher to gain |
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insight into the time dependent evolution of a system. Diffusion |
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phenomena are readily studied with this simulation technique, making |
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Molecular Dynamics the main simulation technique used in this |
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research. Other aspects of the research fall under the Monte Carlo |
14 |
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class of simulations. In Monte Carlo, the configuration space |
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available to the collection of particles is sampled stochastichally, |
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available to the collection of particles is sampled stochastically, |
16 |
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or randomly. Each configuration is chosen with a given probability |
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based on the Maxwell Boltzman distribution. These types of simulations |
17 |
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based on the Maxwell Boltzmann distribution. These types of simulations |
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are best used to probe properties of a system that are only dependent |
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only on the state of the system. Structural information about a system |
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is most readily obtained through these types of methods. |
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thermodynamic properties of the system are being probed, then chose |
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which method best suits that objective. |
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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 Boltzmann 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 |
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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}Boltzmann weighted statistics} |
41 |
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|
42 |
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\subsection{\label{introSec:monteCarlo}Monte Carlo Simulations} |
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Consider a system, $\gamma$, with some total energy,, $E_{\gamma}$. |
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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 |
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$E_{\gamma}$. Further, if $\gamma$ is in contact with a bath system |
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where energy is exchanged between the two systems, $\Omega(E)$, where |
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$E$ is the total energy of both systems, can be represented as |
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\begin{equation} |
50 |
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\Omega(E) = \Omega(E_{\gamma}) \times \Omega(E - E_{\gamma}) |
51 |
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\label{introEq:SM1} |
52 |
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\end{equation} |
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Or additively as |
54 |
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\begin{equation} |
55 |
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\ln \Omega(E) = \ln \Omega(E_{\gamma}) + \ln \Omega(E - E_{\gamma}) |
56 |
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\label{introEq:SM2} |
57 |
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\end{equation} |
58 |
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|
59 |
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The solution to Eq.~\ref{introEq:SM2} maximizes the number of |
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degenerative configurations in $E$. \cite{Frenkel1996} |
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This gives |
62 |
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\begin{equation} |
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\frac{\partial \ln \Omega(E)}{\partial E_{\gamma}} = 0 = |
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\frac{\partial \ln \Omega(E_{\gamma})}{\partial E_{\gamma}} |
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+ |
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\frac{\partial \ln \Omega(E_{\text{bath}})}{\partial E_{\text{bath}}} |
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\frac{\partial E_{\text{bath}}}{\partial E_{\gamma}} |
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\label{introEq:SM3} |
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\end{equation} |
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Where $E_{\text{bath}}$ is $E-E_{\gamma}$, and |
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$\frac{\partial E_{\text{bath}}}{\partial E_{\gamma}}$ is |
72 |
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$-1$. Eq.~\ref{introEq:SM3} becomes |
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\begin{equation} |
74 |
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\frac{\partial \ln \Omega(E_{\gamma})}{\partial E_{\gamma}} = |
75 |
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\frac{\partial \ln \Omega(E_{\text{bath}})}{\partial E_{\text{bath}}} |
76 |
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\label{introEq:SM4} |
77 |
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\end{equation} |
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|
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At this point, one can draw a relationship between the maximization of |
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degeneracy in Eq.~\ref{introEq:SM3} and the second law of |
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thermodynamics. Namely, that for a closed system, entropy will |
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increase for an irreversible process.\cite{chandler:1987} Here the |
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process is the partitioning of energy among the two systems. This |
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allows the following definition of entropy: |
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\begin{equation} |
86 |
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S = k_B \ln \Omega(E) |
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\label{introEq:SM5} |
88 |
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\end{equation} |
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Where $k_B$ is the Boltzmann constant. Having defined entropy, one can |
90 |
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also define the temperature of the system using the relation |
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\begin{equation} |
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\frac{1}{T} = \biggl ( \frac{\partial S}{\partial E} \biggr )_{N,V} |
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\label{introEq:SM6} |
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\end{equation} |
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The temperature in the system $\gamma$ is then |
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\begin{equation} |
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\beta( E_{\gamma} ) = \frac{1}{k_B T} = |
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\frac{\partial \ln \Omega(E_{\gamma})}{\partial E_{\gamma}} |
99 |
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\label{introEq:SM7} |
100 |
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\end{equation} |
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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 |
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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, $E$, |
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is allowed to fluctuate. Returning to the previous example, the bath |
114 |
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system is now an infinitely large thermal bath, whose exchange of |
115 |
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energy with the system $\gamma$ holds the temperature constant. The |
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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} ) |
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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 accessible 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 |
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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 |
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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 |
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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 |
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\begin{equation} |
146 |
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\ln \Omega ( E - E_{\gamma}) = |
147 |
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\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 |
> |
\end{equation} |
152 |
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Higher order terms are omitted as $E$ is an infinite thermal |
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bath. Further, using Eq.~\ref{introEq:SM7}, Eq.~\ref{introEq:SM11} can |
154 |
> |
be rewritten: |
155 |
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\begin{equation} |
156 |
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P_{\gamma} \propto e^{-\beta E_{\gamma}} |
157 |
> |
\label{introEq:SM13} |
158 |
> |
\end{equation} |
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Where $\ln \Omega(E)$ has been factored out of the proportionality as a |
160 |
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constant. Normalizing the probability ($\int\limits_{\boldsymbol{\Gamma}} |
161 |
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d\boldsymbol{\Gamma} P_{\gamma} = 1$) gives |
162 |
> |
\begin{equation} |
163 |
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P_{\gamma} = \frac{e^{-\beta E_{\gamma}}} |
164 |
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{\int\limits_{\boldsymbol{\Gamma}} d\boldsymbol{\Gamma} e^{-\beta E_{\gamma}}} |
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\label{introEq:SM14} |
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\end{equation} |
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This result is the standard Boltzmann statistical distribution. |
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Applying it to Eq.~\ref{introEq:SM10} one can obtain the following relation for ensemble averages: |
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\begin{equation} |
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\langle A \rangle = |
171 |
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\frac{\int\limits_{\boldsymbol{\Gamma}} d\boldsymbol{\Gamma} |
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A( \boldsymbol{\Gamma} ) e^{-\beta E_{\gamma}}} |
173 |
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{\int\limits_{\boldsymbol{\Gamma}} d\boldsymbol{\Gamma} e^{-\beta E_{\gamma}}} |
174 |
> |
\label{introEq:SM15} |
175 |
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\end{equation} |
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|
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\subsection{\label{introSec:ergodic}The Ergodic Hypothesis} |
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|
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One last important consideration is that of ergodicity. Ergodicity is |
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the assumption that given an infinite amount of time, a system will |
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visit every available point in phase space.\cite{Frenkel1996} For most |
182 |
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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, |
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ergodicity allows the unification of a time averaged observation and |
185 |
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an ensemble averaged one. If an observation is averaged over a |
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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 |
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weighted statistical average. This allows the researcher freedom of |
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choice when deciding how best to measure a given observable. When an |
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ensemble averaged approach seems most logical, the Monte Carlo |
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techniques described in Sec.~\ref{introSec:monteCarlo} can be utilized. |
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Conversely, if a problem lends itself to a time averaging approach, |
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the Molecular Dynamics techniques in Sec.~\ref{introSec:MD} can be |
194 |
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employed. |
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|
196 |
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\section{\label{introSec:monteCarlo}Monte Carlo Simulations} |
197 |
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|
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The Monte Carlo method was developed by Metropolis and Ulam for their |
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work in fissionable material.\cite{metropolis:1949} The method is so |
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named, because it heavily uses random numbers in its |
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$[a,b]$. The calculation of the integral could then be solved by |
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randomly choosing points along the interval $[a,b]$ and calculating |
219 |
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the value of $f(x)$ at each point. The accumulated average would then |
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approach $I$ in the limit where the number of trials is infintely |
220 |
> |
approach $I$ in the limit where the number of trials is infinitely |
221 |
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large. |
222 |
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|
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|
However, in Statistical Mechanics, one is typically interested in |
229 |
|
\label{eq:mcEnsAvg} |
230 |
|
\end{equation} |
231 |
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Where $\mathbf{r}^N$ stands for the coordinates of all $N$ particles |
232 |
< |
and $A$ is some observable that is only dependent on |
233 |
< |
position. $\langle A \rangle$ is the ensemble average of $A$ as |
234 |
< |
presented in Sec.~\ref{introSec:statThermo}. Because $A$ is |
235 |
< |
independent of momentum, the momenta contribution of the integral can |
236 |
< |
be factored out, leaving the configurational integral. Application of |
237 |
< |
the brute force method to this system would yield highly inefficient |
238 |
< |
results. Due to the Boltzman weighting of this integral, most random |
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 Boltzmann weighting of this integral, most random |
239 |
|
configurations will have a near zero contribution to the ensemble |
240 |
< |
average. This is where a importance sampling comes into |
240 |
> |
average. This is where importance sampling comes into |
241 |
|
play.\cite{allen87:csl} |
242 |
|
|
243 |
|
Importance Sampling is a method where one selects a distribution from |
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 |
266 |
> |
Where $\rho_{kT}$ is the Boltzmann 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) |
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 |
288 |
> |
was proposed by Metropolis \emph{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 |
< |
\subsubsection{\label{introSec:markovChains}Markov Chains} |
292 |
> |
\subsection{\label{introSec:markovChains}Markov Chains} |
293 |
|
|
294 |
|
A Markov chain is a chain of states satisfying the following |
295 |
|
conditions:\cite{leach01:mm} |
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 |
300 |
> |
If given two configurations, $\mathbf{r}^N_m$ and $\mathbf{r}^N_n$, |
301 |
> |
$\rho_m$ and $\rho_n$ are the probabilities 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 $n$. |
339 |
|
\label{introEq:MCmarkovEquil} |
340 |
|
\end{equation} |
341 |
|
|
342 |
< |
\subsubsection{\label{introSec:metropolisMethod}The Metropolis Method} |
342 |
> |
\subsection{\label{introSec:metropolisMethod}The Metropolis Method} |
343 |
|
|
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 |
346 |
> |
$\boldsymbol{\rho}_{\text{limit}}$ matches the Boltzmann 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 |
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 |
355 |
> |
Further, $\boldsymbol{\alpha}$ is chosen to be a symmetric matrix in |
356 |
|
the Metropolis method. Using Eq.~\ref{introEq:MCpi}, |
357 |
|
Eq.~\ref{introEq:MCmicroReverse} becomes |
358 |
|
\begin{equation} |
360 |
|
\frac{\rho_n}{\rho_m} |
361 |
|
\label{introEq:MCmicro2} |
362 |
|
\end{equation} |
363 |
< |
For a Boltxman limiting distribution, |
363 |
> |
For a Boltzmann 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}} |
368 |
|
\end{equation} |
369 |
|
This allows for the following set of acceptance rules be defined: |
370 |
|
\begin{equation} |
371 |
< |
EQ Here |
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 |
< |
Using the acceptance criteria from Eq.~\ref{fix} the Metropolis method |
380 |
< |
proceeds as follows |
381 |
< |
\begin{itemize} |
382 |
< |
\item Generate an initial configuration $fix$ which has some finite probability in $fix$. |
383 |
< |
\item Modify $fix$, to generate configuratioon $fix$. |
384 |
< |
\item If configuration $n$ lowers the energy of the system, accept the move with unity ($fix$ becomes $fix$). Otherwise accept with probability $fix$. |
385 |
< |
\item Accumulate the average for the configurational observable of intereest. |
386 |
< |
\item Repeat from step 2 until average converges. |
387 |
< |
\end{itemize} |
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 configuration $\mathbf{r^{\prime}}^N$. |
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 interest. |
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{fix} it becomes clear that the accumulated averages are |
391 |
< |
the ensemble averages, as this method ensures that the limiting |
392 |
< |
distribution is the Boltzman distribution. |
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 Boltzmann distribution. |
393 |
|
|
394 |
< |
\subsection{\label{introSec:MD}Molecular Dynamics Simulations} |
394 |
> |
\section{\label{introSec:MD}Molecular Dynamics Simulations} |
395 |
|
|
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 |
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, Eq.~\ref{fix}, the |
403 |
< |
average of these observables over the time period of the simulation |
404 |
< |
are taken to be the ensemble averages for the system. |
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 |
|
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 observabvles depend on momenta in |
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. |
412 |
> |
then most of the time Monte Carlo techniques will be more efficient. |
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 |
< |
\subsubsection{Molecular dynamics Algorithm} |
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{fix} deals with the initialization of a |
423 |
< |
simulation. Sec.~\ref{fix} discusses issues involved with the |
424 |
< |
calculation of the forces. Sec.~\ref{fix} concludes the algorithm |
425 |
< |
discussion with the integration of the equations of motion. \cite{fix} |
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 |
< |
\subsubsection{initialization} |
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{fix} deals with the formation and equilibrium dynamics of |
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 |
435 |
> |
water, and in other cases structured the lipids into performed |
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. |
439 |
> |
\item Velocities are chosen in such a way as to not give the system a non=zero total momentum or angular momentum. |
440 |
> |
\item It is also sometimes desirable 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 |
446 |
> |
to render the numerical integration of the 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 teh selection of the magnitude of the |
452 |
< |
initial velocities. For many simulations it is convienient to use |
451 |
> |
used. The final point addresses the selection of the magnitude of the |
452 |
> |
initial velocities. For many simulations it is convenient 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 |
< |
\subsubsection{Force Evaluation} |
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 $fix$ |
466 |
< |
pairs to be evaluated, where $n$ is the number of particles in the |
467 |
< |
system. This leads to the calculations scaling as $fix$, making large |
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{fix} For a cubic system of 1000 particles arranged |
474 |
< |
in a $10x10x10$ cube, 488 particles will be exposed to the surface. |
475 |
< |
Unless one is simulating an isolated particle group in a vacuum, the |
476 |
< |
behavior of the system will be far from the desired bulk |
477 |
< |
charecteristics. To offset this, simulations employ the use of |
478 |
< |
periodic boundary images. \cite{fix} |
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 characteristics. 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 |
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{fix}). |
484 |
< |
\begin{equation} |
485 |
< |
EQ Here |
486 |
< |
\end{equation} |
487 |
< |
In addition, this sets that any given particle pair has an image, real |
324 |
< |
or periodic, within $fix$ of each other. A discussion of the method |
325 |
< |
used to calculate the periodic image can be found in Sec.\ref{fix}. |
483 |
> |
itself enter on the opposite side (see Fig.~\ref{introFig:pbc}). In |
484 |
> |
addition, this sets that any two particles have an image, real or |
485 |
> |
periodic, within $\text{box}/2$ of each other. A discussion of the |
486 |
> |
method used 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 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.} |
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, $fix$, are not included in the |
501 |
< |
calculation. \cite{fix} In a simultation with periodic images, $fix$ |
502 |
< |
has a maximum value of $fix$. Fig.~\ref{fix} illustrates how using an |
503 |
< |
$fix$ larger than this value, or in the extreme limit of no $fix$ at |
504 |
< |
all, the corners of the simulation box are unequally weighted due to |
505 |
< |
the lack of particle images in the $x$, $y$, or $z$ directions past a |
506 |
< |
disance of $fix$. |
500 |
> |
predetermined distance, $r_{\text{cut}}$, are not included in the |
501 |
> |
calculation.\cite{Frenkel1996} In a simulation 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 distance of $\text{box} / 2$. |
508 |
|
|
509 |
< |
With the use of an $fix$, however, comes a discontinuity in the |
510 |
< |
potential energy curve (Fig.~\ref{fix}). To fix this discontinuity, |
511 |
< |
one calculates the potential energy at the $r_{\text{cut}}$, and add |
512 |
< |
that value to the potential. This causes the function to go smoothly |
513 |
< |
to zero at the cutoff radius. This ensures conservation of energy |
514 |
< |
when integrating the Newtonian equations of motion. |
509 |
> |
\begin{figure} |
510 |
> |
\centering |
511 |
> |
\includegraphics[width=\linewidth]{rCutMaxFig.eps} |
512 |
> |
\caption[An explanation of $r_{\text{cut}}$]{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).} |
513 |
> |
\label{introFig:rMax} |
514 |
> |
\end{figure} |
515 |
> |
|
516 |
> |
With the use of an $r_{\text{cut}}$, however, comes a discontinuity in |
517 |
> |
the potential energy curve (Fig.~\ref{introFig:shiftPot}). To fix this |
518 |
> |
discontinuity, one calculates the potential energy at the |
519 |
> |
$r_{\text{cut}}$, and adds that value to the potential, causing |
520 |
> |
the function to go smoothly to zero at the cutoff radius. This |
521 |
> |
shifted potential ensures conservation of energy when integrating the |
522 |
> |
Newtonian equations of motion. |
523 |
> |
|
524 |
> |
\begin{figure} |
525 |
> |
\centering |
526 |
> |
\includegraphics[width=\linewidth]{shiftedPot.eps} |
527 |
> |
\caption[Shifting the Lennard-Jones Potential]{The Lennard-Jones potential (blue line) is shifted (red line) to remove the discontinuity at $r_{\text{cut}}$.} |
528 |
> |
\label{introFig:shiftPot} |
529 |
> |
\end{figure} |
530 |
|
|
531 |
|
The second main simplification used in this research is the Verlet |
532 |
|
neighbor list. \cite{allen87:csl} In the Verlet method, one generates |
539 |
|
giving rise to the possibility that a particle has left or joined a |
540 |
|
neighbor list. |
541 |
|
|
542 |
< |
\subsection{\label{introSec:MDintegrate} Integration of the equations of motion} |
542 |
> |
\subsection{\label{introSec:mdIntegrate} Integration of the equations of motion} |
543 |
|
|
544 |
|
A starting point for the discussion of molecular dynamics integrators |
545 |
< |
is the Verlet algorithm. \cite{Frenkel1996} It begins with a Taylor |
545 |
> |
is the Verlet algorithm.\cite{Frenkel1996} It begins with a Taylor |
546 |
|
expansion of position in time: |
547 |
|
\begin{equation} |
548 |
< |
eq here |
548 |
> |
q(t+\Delta t)= q(t) + v(t)\Delta t + \frac{F(t)}{2m}\Delta t^2 + |
549 |
> |
\frac{\Delta t^3}{3!}\frac{\partial q(t)}{\partial t} + |
550 |
> |
\mathcal{O}(\Delta t^4) |
551 |
|
\label{introEq:verletForward} |
552 |
|
\end{equation} |
553 |
|
As well as, |
554 |
|
\begin{equation} |
555 |
< |
eq here |
555 |
> |
q(t-\Delta t)= q(t) - v(t)\Delta t + \frac{F(t)}{2m}\Delta t^2 - |
556 |
> |
\frac{\Delta t^3}{3!}\frac{\partial q(t)}{\partial t} + |
557 |
> |
\mathcal{O}(\Delta t^4) |
558 |
|
\label{introEq:verletBack} |
559 |
|
\end{equation} |
560 |
< |
Adding together Eq.~\ref{introEq:verletForward} and |
560 |
> |
Where $m$ is the mass of the particle, $q(t)$ is the position at time |
561 |
> |
$t$, $v(t)$ the velocity, and $F(t)$ the force acting on the |
562 |
> |
particle. Adding together Eq.~\ref{introEq:verletForward} and |
563 |
|
Eq.~\ref{introEq:verletBack} results in, |
564 |
|
\begin{equation} |
565 |
< |
eq here |
565 |
> |
q(t+\Delta t)+q(t-\Delta t) = |
566 |
> |
2q(t) + \frac{F(t)}{m}\Delta t^2 + \mathcal{O}(\Delta t^4) |
567 |
|
\label{introEq:verletSum} |
568 |
|
\end{equation} |
569 |
|
Or equivalently, |
570 |
|
\begin{equation} |
571 |
< |
eq here |
571 |
> |
q(t+\Delta t) = |
572 |
> |
2q(t) - q(t-\Delta t) + \frac{F(t)}{m}\Delta t^2 + |
573 |
> |
\mathcal{O}(\Delta t^4) |
574 |
|
\label{introEq:verletFinal} |
575 |
|
\end{equation} |
576 |
|
Which contains an error in the estimate of the new positions on the |
577 |
|
order of $\Delta t^4$. |
578 |
|
|
579 |
|
In practice, however, the simulations in this research were integrated |
580 |
< |
with a velocity reformulation of teh Verlet method. \cite{allen87:csl} |
580 |
> |
with a velocity reformulation of the Verlet method.\cite{allen87:csl} |
581 |
|
\begin{equation} |
582 |
< |
eq here |
582 |
> |
q(t+\Delta t)= q(t) + v(t)\Delta t + \frac{F(t)}{2m}\Delta t^2 |
583 |
|
\label{introEq:MDvelVerletPos} |
584 |
|
\end{equation} |
585 |
|
\begin{equation} |
586 |
< |
eq here |
586 |
> |
v(t+\Delta t) = v(t) + \frac{\Delta t}{2m}[F(t) + F(t+\Delta t)] |
587 |
|
\label{introEq:MDvelVerletVel} |
588 |
|
\end{equation} |
589 |
|
The original Verlet algorithm can be regained by substituting the |
592 |
|
very little long term drift in energy conservation. Energy |
593 |
|
conservation in a molecular dynamics simulation is of extreme |
594 |
|
importance, as it is a measure of how closely one is following the |
595 |
< |
``true'' trajectory wtih the finite integration scheme. An exact |
595 |
> |
``true'' trajectory with the finite integration scheme. An exact |
596 |
|
solution to the integration will conserve area in phase space, as well |
597 |
|
as be reversible in time, that is, the trajectory integrated forward |
598 |
|
or backwards will exactly match itself. Having a finite algorithm |
600 |
|
therefore increases, but does not guarantee the ``correctness'' or the |
601 |
|
integrated trajectory. |
602 |
|
|
603 |
< |
It can be shown, \cite{Frenkel1996} that although the Verlet algorithm |
603 |
> |
It can be shown,\cite{Frenkel1996} that although the Verlet algorithm |
604 |
|
does not rigorously preserve the actual Hamiltonian, it does preserve |
605 |
|
a pseudo-Hamiltonian which shadows the real one in phase space. This |
606 |
< |
pseudo-Hamiltonian is proveably area-conserving as well as time |
606 |
> |
pseudo-Hamiltonian is provably area-conserving as well as time |
607 |
|
reversible. The fact that it shadows the true Hamiltonian in phase |
608 |
|
space is acceptable in actual simulations as one is interested in the |
609 |
|
ensemble average of the observable being measured. From the ergodic |
614 |
|
\subsection{\label{introSec:MDfurther}Further Considerations} |
615 |
|
In the simulations presented in this research, a few additional |
616 |
|
parameters are needed to describe the motions. The simulations |
617 |
< |
involving water and phospholipids in Chapt.~\ref{chaptLipids} are |
617 |
> |
involving water and phospholipids in Ch.~\ref{chaptLipids} are |
618 |
|
required to integrate the equations of motions for dipoles on atoms. |
619 |
|
This involves an additional three parameters be specified for each |
620 |
|
dipole atom: $\phi$, $\theta$, and $\psi$. These three angles are |
636 |
|
\label{introEq:MDeuleeerPsi} |
637 |
|
\end{equation} |
638 |
|
Where $\omega^s_i$ is the angular velocity in the lab space frame |
639 |
< |
along cartesian coordinate $i$. However, a difficulty arises when |
639 |
> |
along Cartesian coordinate $i$. However, a difficulty arises when |
640 |
|
attempting to integrate Eq.~\ref{introEq:MDeulerPhi} and |
641 |
|
Eq.~\ref{introEq:MDeulerPsi}. The $\frac{1}{\sin \theta}$ present in |
642 |
|
both equations means there is a non-physical instability present when |
666 |
|
\end{equation} |
667 |
|
Here, $r_j$ and $p_j$ are the position and conjugate momenta of a |
668 |
|
degree of freedom, and $f_j$ is the force on that degree of freedom. |
669 |
< |
$\Gamma$ is defined as the set of all positions nad conjugate momenta, |
669 |
> |
$\Gamma$ is defined as the set of all positions and conjugate momenta, |
670 |
|
$\{r_j,p_j\}$, and the propagator, $U(t)$, is defined |
671 |
|
\begin {equation} |
672 |
|
eq here |
722 |
|
This is the velocity Verlet formulation presented in |
723 |
|
Sec.~\ref{introSec:MDintegrate}. Because this integration scheme is |
724 |
|
comprised of unitary propagators, it is symplectic, and therefore area |
725 |
< |
preserving in phase space. From the preceeding fatorization, one can |
725 |
> |
preserving in phase space. From the preceding factorization, one can |
726 |
|
see that the integration of the equations of motion would follow: |
727 |
|
\begin{enumerate} |
728 |
|
\item calculate the velocities at the half step, $\frac{\Delta t}{2}$, from the forces calculated at the initial position. |
746 |
|
eq here |
747 |
|
\label{introEq:SR1} |
748 |
|
\end{equation} |
749 |
< |
Where $\boldsymbol{\tau}(\mathbf{A})$ are the tourques of the system |
749 |
> |
Where $\boldsymbol{\tau}(\mathbf{A})$ are the torques of the system |
750 |
|
due to the configuration, and $\boldsymbol{/pi}$ are the conjugate |
751 |
|
angular momenta of the system. The propagator, $G(\Delta t)$, becomes |
752 |
|
\begin{equation} |
753 |
|
eq here |
754 |
|
\label{introEq:SR2} |
755 |
|
\end{equation} |
756 |
< |
Propagation fo the linear and angular momenta follows as in the Verlet |
757 |
< |
scheme. The propagation of positions also follows the verlet scheme |
756 |
> |
Propagation of the linear and angular momenta follows as in the Verlet |
757 |
> |
scheme. The propagation of positions also follows the Verlet scheme |
758 |
|
with the addition of a further symplectic splitting of the rotation |
759 |
|
matrix propagation, $\mathcal{G}_{\text{rot}}(\Delta t)$. |
760 |
|
\begin{equation} |
766 |
|
unitary and symplectic, the entire integration scheme is also |
767 |
|
symplectic and time reversible. |
768 |
|
|
769 |
< |
\section{\label{introSec:chapterLayout}Chapter Layout} |
769 |
> |
\section{\label{introSec:layout}Dissertation Layout} |
770 |
> |
|
771 |
> |
This dissertation is divided as follows:Chapt.~\ref{chapt:RSA} |
772 |
> |
presents the random sequential adsorption simulations of related |
773 |
> |
pthalocyanines on a gold (111) surface. Ch.~\ref{chapt:OOPSE} |
774 |
> |
is about the writing of the molecular dynamics simulation package |
775 |
> |
{\sc oopse}, Ch.~\ref{chapt:lipid} regards the simulations of |
776 |
> |
phospholipid bilayers using a mesoscale model, and lastly, |
777 |
> |
Ch.~\ref{chapt:conclusion} concludes this dissertation with a |
778 |
> |
summary of all results. The chapters are arranged in chronological |
779 |
> |
order, and reflect the progression of techniques I employed during my |
780 |
> |
research. |
781 |
|
|
782 |
< |
\subsection{\label{introSec:RSA}Random Sequential Adsorption} |
782 |
> |
The chapter concerning random sequential adsorption |
783 |
> |
simulations is a study in applying the principles of theoretical |
784 |
> |
research in order to obtain a simple model capable of explaining the |
785 |
> |
results. My advisor, Dr. Gezelter, and I were approached by a |
786 |
> |
colleague, Dr. Lieberman, about possible explanations for partial |
787 |
> |
coverage of a gold surface by a particular compound of hers. We |
788 |
> |
suggested it might be due to the statistical packing fraction of disks |
789 |
> |
on a plane, and set about to simulate this system. As the events in |
790 |
> |
our model were not dynamic in nature, a Monte Carlo method was |
791 |
> |
employed. Here, if a molecule landed on the surface without |
792 |
> |
overlapping another, then its landing was accepted. However, if there |
793 |
> |
was overlap, the landing we rejected and a new random landing location |
794 |
> |
was chosen. This defined our acceptance rules and allowed us to |
795 |
> |
construct a Markov chain whose limiting distribution was the surface |
796 |
> |
coverage in which we were interested. |
797 |
|
|
798 |
< |
\subsection{\label{introSec:OOPSE}The OOPSE Simulation Package} |
798 |
> |
The following chapter, about the simulation package {\sc oopse}, |
799 |
> |
describes in detail the large body of scientific code that had to be |
800 |
> |
written in order to study phospholipid bilayer. Although there are |
801 |
> |
pre-existing molecular dynamic simulation packages available, none |
802 |
> |
were capable of implementing the models we were developing.{\sc oopse} |
803 |
> |
is a unique package capable of not only integrating the equations of |
804 |
> |
motion in Cartesian space, but is also able to integrate the |
805 |
> |
rotational motion of rigid bodies and dipoles. Add to this the |
806 |
> |
ability to perform calculations across parallel processors and a |
807 |
> |
flexible script syntax for creating systems, and {\sc oopse} becomes a |
808 |
> |
very powerful scientific instrument for the exploration of our model. |
809 |
|
|
810 |
< |
\subsection{\label{introSec:bilayers}A Mesoscale Model for |
811 |
< |
Phospholipid Bilayers} |
810 |
> |
Bringing us to Ch.~\ref{chapt:lipid}. Using {\sc oopse}, I have been |
811 |
> |
able to parameterize a mesoscale model for phospholipid simulations. |
812 |
> |
This model retains information about solvent ordering about the |
813 |
> |
bilayer, as well as information regarding the interaction of the |
814 |
> |
phospholipid head groups' dipole with each other and the surrounding |
815 |
> |
solvent. These simulations give us insight into the dynamic events |
816 |
> |
that lead to the formation of phospholipid bilayers, as well as |
817 |
> |
provide the foundation for future exploration of bilayer phase |
818 |
> |
behavior with this model. |
819 |
> |
|
820 |
> |
Which leads into the last chapter, where I discuss future directions |
821 |
> |
for both{\sc oopse} and this mesoscale model. Additionally, I will |
822 |
> |
give a summary of results for this dissertation. |
823 |
> |
|
824 |
> |
|