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\chapter{\label{chap:intro}INTRODUCTION AND BACKGROUND} |
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\section{Background on the Problem\label{In:sec:pro}} |
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Phospholipid molecules are chosen to be studied in this dissertation |
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because of their critical role as a foundation of the bio-membrane |
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construction. The self assembled bilayer of the lipids when dispersed |
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in water is the micro structure of the membrane. The phase behavior of |
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lipid bilayer is explored experimentally~\cite{Cevc87}, however, fully |
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understanding on the mechanism is far beyond accomplished. |
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Phospholipid molecules are the primary topic of this dissertation |
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because of their critical role as the foundation of biological |
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membranes. The chemical structure of phospholipids includes the polar |
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head group which is due to a large charge separation between phosphate |
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and amino alcohol, and the nonpolar tails that contains fatty acid |
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chains. Depending on the alcohol which phosphate and fatty acid chains |
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are esterified to, the phospholipids are divided into |
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glycerophospholipids and sphingophospholipids.~\cite{Cevc80} The |
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chemical structures are shown in figure~\ref{Infig:lipid}. |
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\begin{figure} |
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\centering |
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\includegraphics[width=\linewidth]{./figures/inLipid.pdf} |
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\caption{The chemical structure of glycerophospholipids (left) and |
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sphingophospholipids (right).\cite{Cevc80}} |
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\label{Infig:lipid} |
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\end{figure} |
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The glycerophospholipid is the dominant phospholipid in membranes. The |
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types of glycerophospholipids depend on the X group, and the |
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chains. For example, if X is choline, the lipids are known as |
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phosphatidylcholine (PC), or if X is ethanolamine, the lipids are |
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known as phosphatidyethanolamine (PE). Table~\ref{Intab:pc} listed a |
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number types of phosphatidycholine with different fatty acids as the |
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lipid chains. |
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\begin{table*} |
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\begin{minipage}{\linewidth} |
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\begin{center} |
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\caption{A number types of phosphatidycholine.} |
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\begin{tabular}{lll} |
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\hline |
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& Fatty acid & Generic Name \\ |
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\hline |
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\textcolor{red}{DMPC} & Myristic: CH$_3$(CH$_2$)$_{12}$COOH & |
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\textcolor{red}{D}i\textcolor{red}{M}yristoyl\textcolor{red}{P}hosphatidyl\textcolor{red}{C}holine \\ |
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\textcolor{red}{DPPC} & Palmitic: CH$_3$(CH$_2$)$_{14}$COOH & \textcolor{red}{D}i\textcolor{red}{P}almtoyl\textcolor{red}{P}hosphatidyl\textcolor{red}{C}holine |
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\\ |
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\textcolor{red}{DSPC} & Stearic: CH$_3$(CH$_2$)$_{16}$COOH & \textcolor{red}{D}i\textcolor{red}{S}tearoyl\textcolor{red}{P}hosphatidyl\textcolor{red}{C}holine \\ |
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\end{tabular} |
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\label{Intab:pc} |
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\end{center} |
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\end{minipage} |
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\end{table*} |
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When dispersed in water, lipids self assemble into a mumber of |
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topologically distinct bilayer structures. The phase behavior of lipid |
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bilayers has been explored experimentally~\cite{Cevc80}, however, a |
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complete understanding of the mechanism and driving forces behind the |
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various phases has not been achieved. |
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\subsection{Ripple Phase\label{In:ssec:ripple}} |
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The {\it ripple phase} $P_{\beta'}$ of lipid bilayers, named from the |
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The $P_{\beta'}$ {\it ripple phase} of lipid bilayers, named from the |
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periodic buckling of the membrane, is an intermediate phase which is |
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developed either from heating the gel phase $L_{\beta'}$ or cooling |
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the fluid phase $L_\alpha$. Although the ripple phase is observed in |
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different |
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experiments~\cite{Sun96,Katsaras00,Copeland80,Meyer96,Kaasgaard03}, |
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the mechanism of the formation of the ripple phase has never been |
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explained and the microscopic structure of the ripple phase has never |
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been elucidated by experiments. Computational simulation is a perfect |
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tool to study the microscopic properties for a system, however, the |
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long range dimension of the ripple structure and the long time scale |
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of the formation of the ripples are crucial obstacles to performing |
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the actual work. The idea to break through this dilemma forks into: |
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the fluid phase $L_\alpha$. A Sketch is shown in |
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figure~\ref{Infig:phaseDiagram}.~\cite{Cevc80} |
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\begin{figure} |
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\centering |
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\includegraphics[width=\linewidth]{./figures/inPhaseDiagram.pdf} |
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\caption{A phase diagram of lipid bilayer. With increasing the |
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temperature, the bilayer can go through a gel ($L_{\beta'}$), ripple |
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($P_{\beta'}$) to fluid ($L_\alpha$) phase transition.~\cite{Cevc80}} |
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\label{Infig:phaseDiagram} |
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\end{figure} |
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Most structural information of the ripple phase has been obtained by |
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the X-ray diffraction~\cite{Sun96,Katsaras00} and freeze-fracture |
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electron microscopy (FFEM).~\cite{Copeland80,Meyer96} The X-ray |
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diffraction work by Katsaras {\it et al.} showed that a rich phase |
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diagram exhibiting both {\it asymmetric} and {\it symmetric} ripples |
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is possible for lecithin bilayers.\cite{Katsaras00} Recently, |
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Kaasgaard {\it et al.} used atomic force microscopy (AFM) to observe |
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ripple phase morphology in bilayers supported on |
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mica.~\cite{Kaasgaard03} |
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\begin{figure} |
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\centering |
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\includegraphics[width=\linewidth]{./figures/inRipple.pdf} |
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\caption{The experimental observed ripple phase. The top image is |
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obtained by Sun {\it et al.} using X-ray diffraction~\cite{Sun96}, |
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and the bottom one is observed by Kaasgaard {\it et al.} using |
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AFM.~\cite{Kaasgaard03}} |
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\label{Infig:ripple} |
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\end{figure} |
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Figure~\ref{Infig:ripple} shows the ripple phase oberved by X-ray |
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diffraction and AFM. The experimental results provide strong support |
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for a 2-dimensional triangular packing lattice of the lipid molecules |
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within the ripple phase. This is a notable change from the observed |
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lipid packing within the gel phase,~\cite{Cevc80} although Tenchov |
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{\it et al.} have recently observed near-hexagonal packing in some |
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phosphatidylcholine (PC) gel phases.~\cite{Tenchov2001} However, the |
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physical mechanism for the formation of the ripple phase has never |
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been explained and the microscopic structure of the ripple phase has |
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never been elucidated by experiments. Computational simulation is a |
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perfect tool to study the microscopic properties for a |
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system. However, the large length scale the ripple structure and the |
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long time scale of the formation of the ripples are crucial obstacles |
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to performing the actual work. The principal ideas explored in this |
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dissertation are attempts to break the computational task up by |
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\begin{itemize} |
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\item Simplify the lipid model. |
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\item Improve the integrating algorithm. |
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\item Simplifying the lipid model. |
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\item Improving algorithm for integrating the equations of motion. |
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\end{itemize} |
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In Ch.~\ref{chap:mc} and~\ref{chap:md}, we use a simple point dipole |
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model and a coarse-grained model to perform the Monte Carlo and |
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Molecular Dynamics simulations respectively, and in Ch.~\ref{chap:ld}, |
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we implement a Langevin Dynamics algorithm to exclude the explicit |
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solvent to improve the efficiency of the simulations. |
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In chapters~\ref{chap:mc} and~\ref{chap:md}, we use a simple point |
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dipole spin model and a coarse-grained molecualr scale model to |
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perform the Monte Carlo and Molecular Dynamics simulations |
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respectively, and in chapter~\ref{chap:ld}, we develop a Langevin |
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Dynamics algorithm which excludes the explicit solvent to improve the |
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efficiency of the simulations. |
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\subsection{Lattice Model\label{In:ssec:model}} |
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The gel like characteristic of the ripple phase ensures the feasiblity |
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of applying the lattice model to study the system. It is claimed that |
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the packing of the lipid molecules in ripple phase is |
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hexagonal~\cite{Cevc87}. The popular $2$ dimensional lattice models, |
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{\it i.e.}, Ising model, Heisenberg model and $X-Y$ model, show |
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{\it frustration} on triangular lattice. |
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The gel-like characteristic (relatively immobile molecules) exhibited |
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by the ripple phase makes it feasible to apply a lattice model to |
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study the system. The popular $2$ dimensional lattice models, {\it |
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i.e.}, the Ising, $X-Y$, and Heisenberg models, show {\it frustration} |
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on triangular lattices. The Hamiltonians of these systems are given by |
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\begin{equation} |
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H = |
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\begin{cases} |
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-J \sum_n \sum_{n'} s_n s_n' & \text{Ising}, \\ |
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-J \sum_n \sum_{n'} \vec s_n \cdot \vec s_{n'} & \text{$X-Y$ and |
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Heisenberg}, |
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\end{cases} |
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\end{equation} |
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where $J$ has non zero value only when spins $s_n$ ($\vec s_n$) and |
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$s_{n'}$ ($\vec s_{n'}$) are nearest neighbors. When $J > 0$, spins |
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prefer an aligned structure, and if $J < 0$, spins prefer an |
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anti-aligned structure. |
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|
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\begin{figure} |
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\centering |
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\includegraphics[width=\linewidth]{./figures/frustration.pdf} |
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\caption{Sketch to illustrate the frustration on triangular |
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lattice. Spins are represented by arrows, no matter which direction |
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the spin on the top of triangle points to, the Hamiltonian of the |
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system is the same, hence there are infinite possibilities for the |
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packing of the spins.} |
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\label{fig:frustration} |
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\includegraphics[width=3in]{./figures/inFrustration.pdf} |
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\caption{Frustration on triangular lattice, the spins and dipoles are |
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represented by arrows. The multiple local minima of energy states |
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induce the frustration for spins and dipoles picking the directions.} |
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\label{Infig:frustration} |
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\end{figure} |
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Figure~\ref{fig:frustration} shows an illustration of the frustration |
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on a triangular lattice. The direction of the spin on top of the |
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triangle has no effects on the Hamiltonian of the system, therefore |
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infinite possibilities for the packing of spins induce the frustration |
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of the lattice. |
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The spins in figure~\ref{Infig:frustration} shows an illustration of |
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the frustration for $J < 0$ on a triangular lattice. There are |
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multiple local minima energy states which are independent of the |
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direction of the spin on top of the triangle, therefore infinite |
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possibilities for the packing of spins which induces what is known as |
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``complete regular frustration'' which leads to disordered low |
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temperature phases. The similarity goes to the dipoles on a hexagonal |
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lattice, which are shown by the dipoles in |
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figure~\ref{Infig:frustration}. In this circumstance, the dipoles want |
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to be aligned, however, due to the long wave fluctuation, at low |
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temperature, the aligned state becomes unstable, vortex is formed and |
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results in multiple local minima of energy states. The dipole on the |
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center of the hexagonal lattice is frustrated. |
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|
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The lack of translational degree of freedom in lattice models prevents |
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their utilization on investigating the emergence of the surface |
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buckling which is the imposition of the ripple formation. In this |
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dissertation, a modified lattice model is introduced to this specific |
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situation in Ch.~\ref{chap:mc}. |
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The lack of translational degrees of freedom in lattice models |
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prevents their utilization in models for surface buckling. In |
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chapter~\ref{chap:mc}, a modified lattice model is introduced to |
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tackle this specific situation. |
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|
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\section{Overview of Classical Statistical Mechanics\label{In:sec:SM}} |
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Statistical mechanics provides a way to calculate the macroscopic |
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computational simulations. This section serves as a brief introduction |
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to key concepts of classical statistical mechanics that we used in |
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this dissertation. Tolman gives an excellent introduction to the |
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principles of statistical mechanics~\cite{Tolman1979}. A large part of |
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principles of statistical mechanics.~\cite{Tolman1979} A large part of |
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section~\ref{In:sec:SM} will follow Tolman's notation. |
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|
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\subsection{Ensembles\label{In:ssec:ensemble}} |
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In classical mechanics, the state of the system is completely |
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described by the positions and momenta of all particles. If we have an |
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$N$ particle system, there are $6N$ coordinates ($3N$ position $(q_1, |
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$N$ particle system, there are $6N$ coordinates ($3N$ positions $(q_1, |
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q_2, \ldots, q_{3N})$ and $3N$ momenta $(p_1, p_2, \ldots, p_{3N})$) |
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to define the instantaneous state of the system. Each single set of |
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the $6N$ coordinates can be considered as a unique point in a $6N$ |
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normalize $\rho$ to unity, |
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\begin{equation} |
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1 = \int d \vec q~^N \int d \vec p~^N \rho, |
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\label{normalized} |
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\label{Ineq:normalized} |
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\end{equation} |
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then the value of $\rho$ gives the probability of finding the system |
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in a unit volume in the phase space. |
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in a unit volume in phase space. |
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|
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Liouville's theorem describes the change in density $\rho$ with |
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time. The number of representive points at a given volume in the phase |
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time. The number of representative points at a given volume in phase |
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space at any instant can be written as: |
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\begin{equation} |
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\label{eq:deltaN} |
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\label{Ineq:deltaN} |
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\delta N = \rho~\delta q_1 \delta q_2 \ldots \delta q_N \delta p_1 \delta p_2 \ldots \delta p_N. |
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\end{equation} |
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To calculate the change in the number of representive points in this |
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To calculate the change in the number of representative points in this |
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volume, let us consider a simple condition: the change in the number |
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of representive points in $q_1$ axis. The rate of the number of the |
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representive points entering the volume at $q_1$ per unit time is: |
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of representative points along the $q_1$ axis. The rate of the number |
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of the representative points entering the volume at $q_1$ per unit time |
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is: |
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\begin{equation} |
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\label{eq:deltaNatq1} |
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\label{Ineq:deltaNatq1} |
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\rho~\dot q_1 \delta q_2 \ldots \delta q_N \delta p_1 \delta p_2 \ldots \delta p_N, |
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\end{equation} |
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and the rate of the number of representive points leaving the volume |
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and the rate of the number of representative points leaving the volume |
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at another position $q_1 + \delta q_1$ is: |
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\begin{equation} |
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\label{eq:deltaNatq1plusdeltaq1} |
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\label{Ineq:deltaNatq1plusdeltaq1} |
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\left( \rho + \frac{\partial \rho}{\partial q_1} \delta q_1 \right)\left(\dot q_1 + |
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\frac{\partial \dot q_1}{\partial q_1} \delta q_1 \right)\delta q_2 \ldots \delta q_N \delta p_1 \delta p_2 \ldots \delta p_N. |
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\end{equation} |
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Here the higher order differentials are neglected. So the change of |
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the number of the representive points is the difference of |
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eq.~\ref{eq:deltaNatq1} and eq.~\ref{eq:deltaNatq1plusdeltaq1}, which |
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gives us: |
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Here the higher order differentials are neglected. So the change in |
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the number of representative points is the difference between |
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eq.~\ref{Ineq:deltaNatq1} and eq.~\ref{Ineq:deltaNatq1plusdeltaq1}, |
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which gives us: |
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\begin{equation} |
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\label{eq:deltaNatq1axis} |
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\label{Ineq:deltaNatq1axis} |
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-\left(\rho \frac{\partial {\dot q_1}}{\partial q_1} + \frac{\partial {\rho}}{\partial q_1} \dot q_1 \right)\delta q_1 \delta q_2 \ldots \delta q_N \delta p_1 \delta p_2 \ldots \delta p_N, |
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\end{equation} |
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where, higher order differetials are neglected. If we sum over all the |
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axes in the phase space, we can get the change of the number of |
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representive points in a given volume with time: |
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axes in the phase space, we can get the change in the number of |
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representative points in a given volume with time: |
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\begin{equation} |
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\label{eq:deltaNatGivenVolume} |
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\label{Ineq:deltaNatGivenVolume} |
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\frac{d(\delta N)}{dt} = -\sum_{i=1}^N \left[\rho \left(\frac{\partial |
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{\dot q_i}}{\partial q_i} + \frac{\partial |
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{\dot p_i}}{\partial p_i}\right) + \left( \frac{\partial {\rho}}{\partial |
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q_i} \dot q_i + \frac{\partial {\rho}}{\partial p_i} \dot p_i\right)\right]\delta q_1 \delta q_2 \ldots \delta q_N \delta p_1 \delta p_2 \ldots \delta p_N. |
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\end{equation} |
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From Hamilton's equation of motion, |
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From Hamilton's equations of motion, |
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\begin{equation} |
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\frac{\partial {\dot q_i}}{\partial q_i} = - \frac{\partial |
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{\dot p_i}}{\partial p_i}, |
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\label{eq:canonicalFormOfEquationOfMotion} |
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\label{Ineq:canonicalFormOfEquationOfMotion} |
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\end{equation} |
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this cancels out the first term on the right side of |
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eq.~\ref{eq:deltaNatGivenVolume}. If both sides of |
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eq.~\ref{eq:deltaNatGivenVolume} are divided by $\delta q_1 \delta q_2 |
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eq.~\ref{Ineq:deltaNatGivenVolume}. If both sides of |
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eq.~\ref{Ineq:deltaNatGivenVolume} are divided by $\delta q_1 \delta q_2 |
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\ldots \delta q_N \delta p_1 \delta p_2 \ldots \delta p_N$, then we |
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can derive Liouville's theorem: |
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arrive at Liouville's theorem: |
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\begin{equation} |
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\left( \frac{\partial \rho}{\partial t} \right)_{q, p} = -\sum_{i} \left( |
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\frac{\partial {\rho}}{\partial |
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q_i} \dot q_i + \frac{\partial {\rho}}{\partial p_i} \dot p_i \right). |
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\label{eq:simpleFormofLiouville} |
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\label{Ineq:simpleFormofLiouville} |
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\end{equation} |
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This is the basis of statistical mechanics. If we move the right |
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side of equation~\ref{eq:simpleFormofLiouville} to the left, we |
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side of equation~\ref{Ineq:simpleFormofLiouville} to the left, we |
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will obtain |
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\begin{equation} |
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\left( \frac{\partial \rho}{\partial t} \right)_{q, p} + \sum_{i} \left( |
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\frac{\partial {\rho}}{\partial |
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q_i} \dot q_i + \frac{\partial {\rho}}{\partial p_i} \dot p_i \right) |
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= 0. |
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\label{eq:anotherFormofLiouville} |
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\label{Ineq:anotherFormofLiouville} |
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\end{equation} |
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It is easy to note that the left side of |
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equation~\ref{eq:anotherFormofLiouville} is the total derivative of |
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< |
$\rho$ with respect of $t$, which means |
| 263 |
> |
equation~\ref{Ineq:anotherFormofLiouville} is the total derivative of |
| 264 |
> |
$\rho$ with respect to $t$, which means |
| 265 |
|
\begin{equation} |
| 266 |
|
\frac{d \rho}{dt} = 0, |
| 267 |
< |
\label{eq:conservationofRho} |
| 267 |
> |
\label{Ineq:conservationofRho} |
| 268 |
|
\end{equation} |
| 269 |
|
and the rate of density change is zero in the neighborhood of any |
| 270 |
< |
selected moving representive points in the phase space. |
| 270 |
> |
selected moving representative points in the phase space. |
| 271 |
|
|
| 272 |
|
The condition of the ensemble is determined by the density |
| 273 |
|
distribution. If we consider the density distribution as only a |
| 274 |
|
function of $q$ and $p$, which means the rate of change of the phase |
| 275 |
< |
space density in the neighborhood of all representive points in the |
| 275 |
> |
space density in the neighborhood of all representative points in the |
| 276 |
|
phase space is zero, |
| 277 |
|
\begin{equation} |
| 278 |
|
\left( \frac{\partial \rho}{\partial t} \right)_{q, p} = 0. |
| 279 |
< |
\label{eq:statEquilibrium} |
| 279 |
> |
\label{Ineq:statEquilibrium} |
| 280 |
|
\end{equation} |
| 281 |
|
We may conclude the ensemble is in {\it statistical equilibrium}. An |
| 282 |
< |
ensemble in statistical equilibrium often means the system is also in |
| 282 |
> |
ensemble in statistical equilibrium means the system is also in |
| 283 |
|
macroscopic equilibrium. If $\left( \frac{\partial \rho}{\partial t} |
| 284 |
|
\right)_{q, p} = 0$, then |
| 285 |
|
\begin{equation} |
| 287 |
|
\frac{\partial {\rho}}{\partial |
| 288 |
|
q_i} \dot q_i + \frac{\partial {\rho}}{\partial p_i} \dot p_i \right) |
| 289 |
|
= 0. |
| 290 |
< |
\label{constantofMotion} |
| 290 |
> |
\label{Ineq:constantofMotion} |
| 291 |
|
\end{equation} |
| 292 |
|
If $\rho$ is a function only of some constant of the motion, $\rho$ is |
| 293 |
|
independent of time. For a conservative system, the energy of the |
| 294 |
< |
system is one of the constants of the motion. Here are several |
| 295 |
< |
examples: when the density distribution is constant everywhere in the |
| 296 |
< |
phase space, |
| 294 |
> |
system is one of the constants of the motion. There are many |
| 295 |
> |
thermodynamically relevant ensembles: when the density distribution is |
| 296 |
> |
constant everywhere in the phase space, |
| 297 |
|
\begin{equation} |
| 298 |
|
\rho = \mathrm{const.} |
| 299 |
< |
\label{eq:uniformEnsemble} |
| 299 |
> |
\label{Ineq:uniformEnsemble} |
| 300 |
|
\end{equation} |
| 301 |
< |
the ensemble is called {\it uniform ensemble}. Another useful |
| 302 |
< |
ensemble is called {\it microcanonical ensemble}, for which: |
| 301 |
> |
the ensemble is called {\it uniform ensemble}. |
| 302 |
> |
|
| 303 |
> |
\subsubsection{The Microcanonical Ensemble\label{In:sssec:microcanonical}} |
| 304 |
> |
Another useful ensemble is the {\it microcanonical ensemble}, for |
| 305 |
> |
which: |
| 306 |
|
\begin{equation} |
| 307 |
|
\rho = \delta \left( H(q^N, p^N) - E \right) \frac{1}{\Sigma (N, V, E)} |
| 308 |
< |
\label{eq:microcanonicalEnsemble} |
| 308 |
> |
\label{Ineq:microcanonicalEnsemble} |
| 309 |
|
\end{equation} |
| 310 |
|
where $\Sigma(N, V, E)$ is a normalization constant parameterized by |
| 311 |
|
$N$, the total number of particles, $V$, the total physical volume and |
| 315 |
|
Hamiltonian of the system. The Gibbs entropy is defined as |
| 316 |
|
\begin{equation} |
| 317 |
|
S = - k_B \int d \vec q~^N \int d \vec p~^N \rho \ln [C^N \rho], |
| 318 |
< |
\label{eq:gibbsEntropy} |
| 318 |
> |
\label{Ineq:gibbsEntropy} |
| 319 |
|
\end{equation} |
| 320 |
|
where $k_B$ is the Boltzmann constant and $C^N$ is a number which |
| 321 |
< |
makes the argument of $\ln$ dimensionless, in this case, it is the |
| 322 |
< |
total phase space volume of one state. The entropy in microcanonical |
| 321 |
> |
makes the argument of $\ln$ dimensionless. In this case, $C^N$ is the |
| 322 |
> |
total phase space volume of one state. The entropy of a microcanonical |
| 323 |
|
ensemble is given by |
| 324 |
|
\begin{equation} |
| 325 |
|
S = k_B \ln \left(\frac{\Sigma(N, V, E)}{C^N}\right). |
| 326 |
< |
\label{eq:entropy} |
| 326 |
> |
\label{Ineq:entropy} |
| 327 |
|
\end{equation} |
| 328 |
+ |
|
| 329 |
+ |
\subsubsection{The Canonical Ensemble\label{In:sssec:canonical}} |
| 330 |
|
If the density distribution $\rho$ is given by |
| 331 |
|
\begin{equation} |
| 332 |
|
\rho = \frac{1}{Z_N}e^{-H(q^N, p^N) / k_B T}, |
| 333 |
< |
\label{eq:canonicalEnsemble} |
| 333 |
> |
\label{Ineq:canonicalEnsemble} |
| 334 |
|
\end{equation} |
| 335 |
|
the ensemble is known as the {\it canonical ensemble}. Here, |
| 336 |
|
\begin{equation} |
| 337 |
|
Z_N = \int d \vec q~^N \int_\Gamma d \vec p~^N e^{-H(q^N, p^N) / k_B T}, |
| 338 |
< |
\label{eq:partitionFunction} |
| 338 |
> |
\label{Ineq:partitionFunction} |
| 339 |
|
\end{equation} |
| 340 |
< |
which is also known as {\it partition function}. $\Gamma$ indicates |
| 341 |
< |
that the integral is over all the phase space. In the canonical |
| 340 |
> |
which is also known as the canonical{\it partition function}. $\Gamma$ |
| 341 |
> |
indicates that the integral is over all phase space. In the canonical |
| 342 |
|
ensemble, $N$, the total number of particles, $V$, total volume, and |
| 343 |
< |
$T$, the temperature are constants. The systems with the lowest |
| 343 |
> |
$T$, the temperature, are constants. The systems with the lowest |
| 344 |
|
energies hold the largest population. According to maximum principle, |
| 345 |
< |
the thermodynamics maximizes the entropy $S$, |
| 345 |
> |
thermodynamics maximizes the entropy $S$, implying that |
| 346 |
|
\begin{equation} |
| 347 |
|
\begin{array}{ccc} |
| 348 |
|
\delta S = 0 & \mathrm{and} & \delta^2 S < 0. |
| 349 |
|
\end{array} |
| 350 |
< |
\label{eq:maximumPrinciple} |
| 350 |
> |
\label{Ineq:maximumPrinciple} |
| 351 |
|
\end{equation} |
| 352 |
< |
From Eq.~\ref{eq:maximumPrinciple} and two constrains of the canonical |
| 353 |
< |
ensemble, {\it i.e.}, total probability and average energy conserved, |
| 354 |
< |
the partition function is calculated as |
| 352 |
> |
From Eq.~\ref{Ineq:maximumPrinciple} and two constrains on the |
| 353 |
> |
canonical ensemble, {\it i.e.}, total probability and average energy |
| 354 |
> |
must be conserved, the partition function can be shown to be |
| 355 |
> |
equivalent to |
| 356 |
|
\begin{equation} |
| 357 |
|
Z_N = e^{-A/k_B T}, |
| 358 |
< |
\label{eq:partitionFunctionWithFreeEnergy} |
| 358 |
> |
\label{Ineq:partitionFunctionWithFreeEnergy} |
| 359 |
|
\end{equation} |
| 360 |
|
where $A$ is the Helmholtz free energy. The significance of |
| 361 |
< |
Eq.~\ref{eq:entropy} and~\ref{eq:partitionFunctionWithFreeEnergy} is |
| 361 |
> |
Eq.~\ref{Ineq:entropy} and~\ref{Ineq:partitionFunctionWithFreeEnergy} is |
| 362 |
|
that they serve as a connection between macroscopic properties of the |
| 363 |
< |
system and the distribution of the microscopic states. |
| 363 |
> |
system and the distribution of microscopic states. |
| 364 |
|
|
| 365 |
|
There is an implicit assumption that our arguments are based on so |
| 366 |
< |
far. A representive point in the phase space is equally to be found in |
| 367 |
< |
any same extent of the regions. In other words, all energetically |
| 368 |
< |
accessible states are represented equally, the probabilities to find |
| 369 |
< |
the system in any of the accessible states is equal. This is called |
| 370 |
< |
equal a {\it priori} probabilities. |
| 366 |
> |
far. A representative point in the phase space is equally likely to be |
| 367 |
> |
found in any energetically allowed region. In other words, all |
| 368 |
> |
energetically accessible states are represented equally, the |
| 369 |
> |
probabilities to find the system in any of the accessible states is |
| 370 |
> |
equal. This is called the principle of equal a {\it priori} |
| 371 |
> |
probabilities. |
| 372 |
|
|
| 373 |
< |
\subsection{Statistical Average\label{In:ssec:average}} |
| 374 |
< |
Given the density distribution $\rho$ in the phase space, the average |
| 373 |
> |
\subsection{Statistical Averages\label{In:ssec:average}} |
| 374 |
> |
Given a density distribution $\rho$ in phase space, the average |
| 375 |
|
of any quantity ($F(q^N, p^N$)) which depends on the coordinates |
| 376 |
|
($q^N$) and the momenta ($p^N$) for all the systems in the ensemble |
| 377 |
|
can be calculated based on the definition shown by |
| 378 |
< |
Eq.~\ref{eq:statAverage1} |
| 378 |
> |
Eq.~\ref{Ineq:statAverage1} |
| 379 |
|
\begin{equation} |
| 380 |
< |
\langle F(q^N, p^N, t) \rangle = \frac{\int d \vec q~^N \int d \vec p~^N |
| 381 |
< |
F(q^N, p^N, t) \rho}{\int d \vec q~^N \int d \vec p~^N \rho}. |
| 382 |
< |
\label{eq:statAverage1} |
| 380 |
> |
\langle F(q^N, p^N) \rangle = \frac{\int d \vec q~^N \int d \vec p~^N |
| 381 |
> |
F(q^N, p^N) \rho}{\int d \vec q~^N \int d \vec p~^N \rho}. |
| 382 |
> |
\label{Ineq:statAverage1} |
| 383 |
|
\end{equation} |
| 384 |
|
Since the density distribution $\rho$ is normalized to unity, the mean |
| 385 |
|
value of $F(q^N, p^N)$ is simplified to |
| 386 |
|
\begin{equation} |
| 387 |
< |
\langle F(q^N, p^N, t) \rangle = \int d \vec q~^N \int d \vec p~^N F(q^N, |
| 388 |
< |
p^N, t) \rho, |
| 389 |
< |
\label{eq:statAverage2} |
| 387 |
> |
\langle F(q^N, p^N) \rangle = \int d \vec q~^N \int d \vec p~^N F(q^N, |
| 388 |
> |
p^N) \rho, |
| 389 |
> |
\label{Ineq:statAverage2} |
| 390 |
|
\end{equation} |
| 391 |
< |
called {\it ensemble average}. However, the quantity is often averaged |
| 392 |
< |
for a finite time in real experiments, |
| 391 |
> |
called the {\it ensemble average}. However, the quantity is often |
| 392 |
> |
averaged for a finite time in real experiments, |
| 393 |
|
\begin{equation} |
| 394 |
|
\langle F(q^N, p^N) \rangle_t = \lim_{T \rightarrow \infty} |
| 395 |
< |
\frac{1}{T} \int_{t_0}^{t_0+T} F(q^N, p^N, t) dt. |
| 396 |
< |
\label{eq:timeAverage1} |
| 395 |
> |
\frac{1}{T} \int_{t_0}^{t_0+T} F[q^N(t), p^N(t)] dt. |
| 396 |
> |
\label{Ineq:timeAverage1} |
| 397 |
|
\end{equation} |
| 398 |
|
Usually this time average is independent of $t_0$ in statistical |
| 399 |
< |
mechanics, so Eq.~\ref{eq:timeAverage1} becomes |
| 399 |
> |
mechanics, so Eq.~\ref{Ineq:timeAverage1} becomes |
| 400 |
|
\begin{equation} |
| 401 |
|
\langle F(q^N, p^N) \rangle_t = \lim_{T \rightarrow \infty} |
| 402 |
< |
\frac{1}{T} \int_{0}^{T} F(q^N, p^N, t) dt |
| 403 |
< |
\label{eq:timeAverage2} |
| 402 |
> |
\frac{1}{T} \int_{0}^{T} F[q^N(t), p^N(t)] dt |
| 403 |
> |
\label{Ineq:timeAverage2} |
| 404 |
|
\end{equation} |
| 405 |
|
for an infinite time interval. |
| 406 |
|
|
| 407 |
< |
{\it ergodic hypothesis}, an important hypothesis from the statistical |
| 408 |
< |
mechanics point of view, states that the system will eventually pass |
| 407 |
> |
\subsubsection{Ergodicity\label{In:sssec:ergodicity}} |
| 408 |
> |
The {\it ergodic hypothesis}, an important hypothesis governing modern |
| 409 |
> |
computer simulations states that the system will eventually pass |
| 410 |
|
arbitrarily close to any point that is energetically accessible in |
| 411 |
|
phase space. Mathematically, this leads to |
| 412 |
|
\begin{equation} |
| 413 |
< |
\langle F(q^N, p^N, t) \rangle = \langle F(q^N, p^N) \rangle_t. |
| 414 |
< |
\label{eq:ergodicity} |
| 413 |
> |
\langle F(q^N, p^N) \rangle = \langle F(q^N, p^N) \rangle_t. |
| 414 |
> |
\label{Ineq:ergodicity} |
| 415 |
|
\end{equation} |
| 416 |
< |
Eq.~\ref{eq:ergodicity} validates the Monte Carlo method which we will |
| 417 |
< |
discuss in section~\ref{In:ssec:mc}. An ensemble average of a quantity |
| 418 |
< |
can be related to the time average measured in the experiments. |
| 416 |
> |
Eq.~\ref{Ineq:ergodicity} validates Molecular Dynamics as a form of |
| 417 |
> |
averaging for sufficiently ergodic systems. Also Monte Carlo may be |
| 418 |
> |
used to obtain ensemble averages of a quantity which are related to |
| 419 |
> |
time averages measured in experiments. |
| 420 |
|
|
| 421 |
< |
\subsection{Correlation Function\label{In:ssec:corr}} |
| 422 |
< |
Thermodynamic properties can be computed by equillibrium statistical |
| 423 |
< |
mechanics. On the other hand, {\it Time correlation function} is a |
| 424 |
< |
powerful method to understand the evolution of a dynamic system in |
| 425 |
< |
non-equillibrium statistical mechanics. Imagine a property $A(q^N, |
| 426 |
< |
p^N, t)$ as a function of coordinates $q^N$ and momenta $p^N$ has an |
| 427 |
< |
intial value at $t_0$, at a later time $t_0 + \tau$ this value is |
| 428 |
< |
changed. If $\tau$ is very small, the change of the value is minor, |
| 429 |
< |
and the later value of $A(q^N, p^N, t_0 + |
| 430 |
< |
\tau)$ is correlated to its initial value. Howere, when $\tau$ is large, |
| 431 |
< |
this correlation is lost. The correlation function is a measurement of |
| 432 |
< |
this relationship and is defined by~\cite{Berne90} |
| 421 |
> |
\subsection{Correlation Functions\label{In:ssec:corr}} |
| 422 |
> |
Thermodynamic properties can be computed by equilibrium statistical |
| 423 |
> |
mechanics. On the other hand, {\it Time correlation functions} are a |
| 424 |
> |
powerful tool to understand the evolution of a dynamical |
| 425 |
> |
systems. Imagine that property $A(q^N, p^N, t)$ as a function of |
| 426 |
> |
coordinates $q^N$ and momenta $p^N$ has an intial value at $t_0$, and |
| 427 |
> |
at a later time $t_0 + \tau$ this value has changed. If $\tau$ is very |
| 428 |
> |
small, the change of the value is minor, and the later value of |
| 429 |
> |
$A(q^N, p^N, t_0 + \tau)$ is correlated to its initial value. However, |
| 430 |
> |
when $\tau$ is large, this correlation is lost. A time correlation |
| 431 |
> |
function measures this relationship and is defined |
| 432 |
> |
by~\cite{Berne90} |
| 433 |
|
\begin{equation} |
| 434 |
< |
C(t) = \langle A(0)A(\tau) \rangle = \lim_{T \rightarrow \infty} |
| 434 |
> |
C_{AA}(\tau) = \langle A(0)A(\tau) \rangle = \lim_{T \rightarrow |
| 435 |
> |
\infty} |
| 436 |
|
\frac{1}{T} \int_{0}^{T} dt A(t) A(t + \tau). |
| 437 |
< |
\label{eq:autocorrelationFunction} |
| 437 |
> |
\label{Ineq:autocorrelationFunction} |
| 438 |
|
\end{equation} |
| 439 |
< |
Eq.~\ref{eq:autocorrelationFunction} is the correlation function of a |
| 440 |
< |
single variable, called {\it autocorrelation function}. The defination |
| 441 |
< |
of the correlation function for two different variables is similar to |
| 442 |
< |
that of autocorrelation function, which is |
| 439 |
> |
Eq.~\ref{Ineq:autocorrelationFunction} is the correlation function of |
| 440 |
> |
a single variable, called an {\it autocorrelation function}. The |
| 441 |
> |
definition of the correlation function for two different variables is |
| 442 |
> |
similar to that of autocorrelation function, which is |
| 443 |
|
\begin{equation} |
| 444 |
< |
C(t) = \langle A(0)B(\tau) \rangle = \lim_{T \rightarrow \infty} |
| 444 |
> |
C_{AB}(\tau) = \langle A(0)B(\tau) \rangle = \lim_{T \rightarrow \infty} |
| 445 |
|
\frac{1}{T} \int_{0}^{T} dt A(t) B(t + \tau), |
| 446 |
< |
\label{eq:crosscorrelationFunction} |
| 446 |
> |
\label{Ineq:crosscorrelationFunction} |
| 447 |
|
\end{equation} |
| 448 |
|
and called {\it cross correlation function}. |
| 449 |
|
|
| 450 |
< |
In section~\ref{In:ssec:average} we know from Eq.~\ref{eq:ergodicity} |
| 451 |
< |
the relationship between time average and ensemble average. We can put |
| 452 |
< |
the correlation function in a classical mechanics form, |
| 450 |
> |
We know from the ergodic hypothesis that there is a relationship |
| 451 |
> |
between time average and ensemble average. We can put the correlation |
| 452 |
> |
function in a classical mechanics form, |
| 453 |
|
\begin{equation} |
| 454 |
< |
C(t) = \langle A(0)A(\tau) \rangle = \int d \vec q~^N \int d \vec p~^N A(t) A(t + \tau) \rho(q, p) |
| 455 |
< |
\label{eq:autocorrelationFunctionCM} |
| 454 |
> |
C_{AA}(\tau) = \int d \vec q~^N \int d \vec p~^N A[(q^N(t), p^N(t)] |
| 455 |
> |
A[q^N(t+\tau), p^N(t+\tau)] \rho(q, p) |
| 456 |
> |
\label{Ineq:autocorrelationFunctionCM} |
| 457 |
|
\end{equation} |
| 458 |
|
and |
| 459 |
|
\begin{equation} |
| 460 |
< |
C(t) = \langle A(0)B(\tau) \rangle = \int d \vec q~^N \int d \vec p~^N A(t) B(t + \tau) |
| 461 |
< |
\rho(q, p) |
| 462 |
< |
\label{eq:crosscorrelationFunctionCM} |
| 460 |
> |
C_{AB}(\tau) = \int d \vec q~^N \int d \vec p~^N A[(q^N(t), p^N(t)] |
| 461 |
> |
B[q^N(t+\tau), p^N(t+\tau)] \rho(q, p) |
| 462 |
> |
\label{Ineq:crosscorrelationFunctionCM} |
| 463 |
|
\end{equation} |
| 464 |
< |
as autocorrelation function and cross correlation function |
| 464 |
> |
as the autocorrelation function and cross correlation functions |
| 465 |
|
respectively. $\rho(q, p)$ is the density distribution at equillibrium |
| 466 |
< |
in phase space. In many cases, the correlation function decay is a |
| 467 |
< |
single exponential |
| 466 |
> |
in phase space. In many cases, correlation functions decay as a |
| 467 |
> |
single exponential in time |
| 468 |
|
\begin{equation} |
| 469 |
|
C(t) \sim e^{-t / \tau_r}, |
| 470 |
< |
\label{eq:relaxation} |
| 470 |
> |
\label{Ineq:relaxation} |
| 471 |
|
\end{equation} |
| 472 |
< |
where $\tau_r$ is known as relaxation time which discribes the rate of |
| 472 |
> |
where $\tau_r$ is known as relaxation time which describes the rate of |
| 473 |
|
the decay. |
| 474 |
|
|
| 475 |
< |
\section{Methodolody\label{In:sec:method}} |
| 476 |
< |
The simulations performed in this dissertation are branched into two |
| 477 |
< |
main catalog, Monte Carlo and Molecular Dynamics. There are two main |
| 478 |
< |
difference between Monte Carlo and Molecular Dynamics simulations. One |
| 479 |
< |
is that the Monte Carlo simulation is time independent, and Molecular |
| 480 |
< |
Dynamics simulation is time involved. Another dissimilar is that the |
| 481 |
< |
Monte Carlo is a stochastic process, the configuration of the system |
| 482 |
< |
is not determinated by its past, however, using Moleuclar Dynamics, |
| 483 |
< |
the system is propagated by Newton's equation of motion, the |
| 484 |
< |
trajectory of the system evolved in the phase space is determined. A |
| 485 |
< |
brief introduction of the two algorithms are given in |
| 486 |
< |
section~\ref{In:ssec:mc} and~\ref{In:ssec:md}. An extension of the |
| 487 |
< |
Molecular Dynamics, Langevin Dynamics, is introduced by |
| 475 |
> |
\section{Methodology\label{In:sec:method}} |
| 476 |
> |
The simulations performed in this dissertation branch into two main |
| 477 |
> |
categories, Monte Carlo and Molecular Dynamics. There are two main |
| 478 |
> |
differences between Monte Carlo and Molecular Dynamics |
| 479 |
> |
simulations. One is that the Monte Carlo simulations are time |
| 480 |
> |
independent methods of sampling structural features of an ensemble, |
| 481 |
> |
while Molecular Dynamics simulations provide dynamic |
| 482 |
> |
information. Additionally, Monte Carlo methods are a stochastic |
| 483 |
> |
processes, the future configurations of the system are not determined |
| 484 |
> |
by its past. However, in Molecular Dynamics, the system is propagated |
| 485 |
> |
by Newton's equation of motion, and the trajectory of the system |
| 486 |
> |
evolving in phase space is deterministic. Brief introductions of the |
| 487 |
> |
two algorithms are given in section~\ref{In:ssec:mc} |
| 488 |
> |
and~\ref{In:ssec:md}. Langevin Dynamics, an extension of the Molecular |
| 489 |
> |
Dynamics that includes implicit solvent effects, is introduced by |
| 490 |
|
section~\ref{In:ssec:ld}. |
| 491 |
|
|
| 492 |
|
\subsection{Monte Carlo\label{In:ssec:mc}} |
| 493 |
< |
Monte Carlo algorithm was first introduced by Metropolis {\it et |
| 494 |
< |
al.}.~\cite{Metropolis53} Basic Monte Carlo algorithm is usually |
| 495 |
< |
applied to the canonical ensemble, a Boltzmann-weighted ensemble, in |
| 496 |
< |
which the $N$, the total number of particles, $V$, total volume, $T$, |
| 497 |
< |
temperature are constants. The average energy is given by substituding |
| 498 |
< |
Eq.~\ref{eq:canonicalEnsemble} into Eq.~\ref{eq:statAverage2}, |
| 493 |
> |
A Monte Carlo integration algorithm was first introduced by Metropolis |
| 494 |
> |
{\it et al.}~\cite{Metropolis53} The basic Metropolis Monte Carlo |
| 495 |
> |
algorithm is usually applied to the canonical ensemble, a |
| 496 |
> |
Boltzmann-weighted ensemble, in which the $N$, the total number of |
| 497 |
> |
particles, $V$, total volume, $T$, temperature are constants. An |
| 498 |
> |
average in this ensemble is given |
| 499 |
|
\begin{equation} |
| 500 |
< |
\langle E \rangle = \frac{1}{Z_N} \int d \vec q~^N \int d \vec p~^N E e^{-H(q^N, p^N) / k_B T}. |
| 501 |
< |
\label{eq:energyofCanonicalEnsemble} |
| 500 |
> |
\langle A \rangle = \frac{1}{Z_N} \int d \vec q~^N \int d \vec p~^N |
| 501 |
> |
A(q^N, p^N) e^{-H(q^N, p^N) / k_B T}. |
| 502 |
> |
\label{Ineq:energyofCanonicalEnsemble} |
| 503 |
|
\end{equation} |
| 504 |
< |
So are the other properties of the system. The Hamiltonian is the |
| 505 |
< |
summation of Kinetic energy $K(p^N)$ as a function of momenta and |
| 506 |
< |
Potential energy $U(q^N)$ as a function of positions, |
| 504 |
> |
The Hamiltonian is the sum of the kinetic energy, $K(p^N)$, a function |
| 505 |
> |
of momenta and the potential energy, $U(q^N)$, a function of |
| 506 |
> |
positions, |
| 507 |
|
\begin{equation} |
| 508 |
|
H(q^N, p^N) = K(p^N) + U(q^N). |
| 509 |
< |
\label{eq:hamiltonian} |
| 509 |
> |
\label{Ineq:hamiltonian} |
| 510 |
|
\end{equation} |
| 511 |
< |
If the property $A$ is only a function of position ($ A = A(q^N)$), |
| 512 |
< |
the mean value of $A$ is reduced to |
| 511 |
> |
If the property $A$ is a function only of position ($ A = A(q^N)$), |
| 512 |
> |
the mean value of $A$ can be reduced to |
| 513 |
|
\begin{equation} |
| 514 |
< |
\langle A \rangle = \frac{\int d \vec q~^N \int d \vec p~^N A e^{-U(q^N) / k_B T}}{\int d \vec q~^N \int d \vec p~^N e^{-U(q^N) / k_B T}}, |
| 515 |
< |
\label{eq:configurationIntegral} |
| 514 |
> |
\langle A \rangle = \frac{\int d \vec q~^N A e^{-U(q^N) / k_B T}}{\int d \vec q~^N e^{-U(q^N) / k_B T}}, |
| 515 |
> |
\label{Ineq:configurationIntegral} |
| 516 |
|
\end{equation} |
| 517 |
|
The kinetic energy $K(p^N)$ is factored out in |
| 518 |
< |
Eq.~\ref{eq:configurationIntegral}. $\langle A |
| 519 |
< |
\rangle$ is a configuration integral now, and the |
| 520 |
< |
Eq.~\ref{eq:configurationIntegral} is equivalent to |
| 518 |
> |
Eq.~\ref{Ineq:configurationIntegral}. $\langle A |
| 519 |
> |
\rangle$ is now a configuration integral, and |
| 520 |
> |
Eq.~\ref{Ineq:configurationIntegral} is equivalent to |
| 521 |
|
\begin{equation} |
| 522 |
|
\langle A \rangle = \int d \vec q~^N A \rho(q^N). |
| 523 |
< |
\label{eq:configurationAve} |
| 523 |
> |
\label{Ineq:configurationAve} |
| 524 |
|
\end{equation} |
| 525 |
|
|
| 526 |
< |
In a Monte Carlo simulation of canonical ensemble, the probability of |
| 527 |
< |
the system being in a state $s$ is $\rho_s$, the change of this |
| 528 |
< |
probability with time is given by |
| 526 |
> |
In a Monte Carlo simulation of a system in the canonical ensemble, the |
| 527 |
> |
probability of the system being in a state $s$ is $\rho_s$, the change |
| 528 |
> |
of this probability with time is given by |
| 529 |
|
\begin{equation} |
| 530 |
|
\frac{d \rho_s}{dt} = \sum_{s'} [ -w_{ss'}\rho_s + w_{s's}\rho_{s'} ], |
| 531 |
< |
\label{eq:timeChangeofProb} |
| 531 |
> |
\label{Ineq:timeChangeofProb} |
| 532 |
|
\end{equation} |
| 533 |
|
where $w_{ss'}$ is the tansition probability of going from state $s$ |
| 534 |
|
to state $s'$. Since $\rho_s$ is independent of time at equilibrium, |
| 535 |
|
\begin{equation} |
| 536 |
|
\frac{d \rho_{s}^{equilibrium}}{dt} = 0, |
| 537 |
< |
\label{eq:equiProb} |
| 537 |
> |
\label{Ineq:equiProb} |
| 538 |
|
\end{equation} |
| 539 |
|
which means $\sum_{s'} [ -w_{ss'}\rho_s + w_{s's}\rho_{s'} ]$ is $0$ |
| 540 |
|
for all $s'$. So |
| 541 |
|
\begin{equation} |
| 542 |
|
\frac{\rho_s^{equilibrium}}{\rho_{s'}^{equilibrium}} = \frac{w_{s's}}{w_{ss'}}. |
| 543 |
< |
\label{eq:timeChangeofProb} |
| 543 |
> |
\label{Ineq:relationshipofRhoandW} |
| 544 |
|
\end{equation} |
| 545 |
< |
If |
| 545 |
> |
If the ratio of state populations |
| 546 |
|
\begin{equation} |
| 547 |
< |
\frac{w_{s's}}{w_{ss'}} = e^{-(U_s - U_{s'}) / k_B T}, |
| 548 |
< |
\label{eq:conditionforBoltzmannStatistics} |
| 547 |
> |
\frac{\rho_s^{equilibrium}}{\rho_{s'}^{equilibrium}} = e^{-(U_s - U_{s'}) / k_B T}. |
| 548 |
> |
\label{Ineq:satisfyofBoltzmannStatistics} |
| 549 |
|
\end{equation} |
| 550 |
< |
then |
| 550 |
> |
then the ratio of transition probabilities, |
| 551 |
|
\begin{equation} |
| 552 |
< |
\frac{\rho_s^{equilibrium}}{\rho_{s'}^{equilibrium}} = e^{-(U_s - U_{s'}) / k_B T}. |
| 553 |
< |
\label{eq:satisfyofBoltzmannStatistics} |
| 552 |
> |
\frac{w_{s's}}{w_{ss'}} = e^{-(U_s - U_{s'}) / k_B T}, |
| 553 |
> |
\label{Ineq:conditionforBoltzmannStatistics} |
| 554 |
|
\end{equation} |
| 555 |
< |
Eq.~\ref{eq:satisfyofBoltzmannStatistics} implies that |
| 556 |
< |
$\rho^{equilibrium}$ satisfies Boltzmann statistics. An algorithm, |
| 557 |
< |
shows how Monte Carlo simulation generates a transition probability |
| 452 |
< |
governed by \ref{eq:conditionforBoltzmannStatistics}, is schemed as |
| 555 |
> |
An algorithm that shows how Monte Carlo simulation generates a |
| 556 |
> |
transition probability governed by |
| 557 |
> |
\ref{Ineq:conditionforBoltzmannStatistics}, is given schematically as, |
| 558 |
|
\begin{enumerate} |
| 559 |
< |
\item\label{itm:oldEnergy} Choose an particle randomly, calculate the energy. |
| 560 |
< |
\item\label{itm:newEnergy} Make a random displacement for particle, |
| 561 |
< |
calculate the new energy. |
| 559 |
> |
\item\label{Initm:oldEnergy} Choose a particle randomly, and calculate |
| 560 |
> |
the energy of the rest of the system due to the location of the particle. |
| 561 |
> |
\item\label{Initm:newEnergy} Make a random displacement of the particle, |
| 562 |
> |
calculate the new energy taking the movement of the particle into account. |
| 563 |
|
\begin{itemize} |
| 564 |
< |
\item Keep the new configuration and return to step~\ref{itm:oldEnergy} if energy |
| 565 |
< |
goes down. |
| 566 |
< |
\item Pick a random number between $[0,1]$ if energy goes up. |
| 564 |
> |
\item If the energy goes down, keep the new configuration and return to |
| 565 |
> |
step~\ref{Initm:oldEnergy}. |
| 566 |
> |
\item If the energy goes up, pick a random number between $[0,1]$. |
| 567 |
|
\begin{itemize} |
| 568 |
< |
\item Keep the new configuration and return to |
| 569 |
< |
step~\ref{itm:oldEnergy} if the random number smaller than |
| 570 |
< |
$e^{-(U_{new} - U_{old})} / k_B T$. |
| 571 |
< |
\item Keep the old configuration and return to |
| 572 |
< |
step~\ref{itm:oldEnergy} if the random number larger than |
| 573 |
< |
$e^{-(U_{new} - U_{old})} / k_B T$. |
| 568 |
> |
\item If the random number smaller than |
| 569 |
> |
$e^{-(U_{new} - U_{old})} / k_B T$, keep the new configuration and return to |
| 570 |
> |
step~\ref{Initm:oldEnergy}. |
| 571 |
> |
\item If the random number is larger than |
| 572 |
> |
$e^{-(U_{new} - U_{old})} / k_B T$, keep the old configuration and return to |
| 573 |
> |
step~\ref{Initm:oldEnergy}. |
| 574 |
|
\end{itemize} |
| 575 |
|
\end{itemize} |
| 576 |
< |
\item\label{itm:accumulateAvg} Accumulate the average after it converges. |
| 576 |
> |
\item\label{Initm:accumulateAvg} Accumulate the averages based on the |
| 577 |
> |
current configuartion. |
| 578 |
> |
\item Go to step~\ref{Initm:oldEnergy}. |
| 579 |
|
\end{enumerate} |
| 580 |
< |
It is important to notice that the old configuration has to be sampled |
| 581 |
< |
again if it is kept. |
| 580 |
> |
It is important for sampling accurately that the old configuration is |
| 581 |
> |
sampled again if it is kept. |
| 582 |
|
|
| 583 |
|
\subsection{Molecular Dynamics\label{In:ssec:md}} |
| 584 |
|
Although some of properites of the system can be calculated from the |
| 585 |
< |
ensemble average in Monte Carlo simulations, due to the nature of |
| 586 |
< |
lacking in the time dependence, it is impossible to gain information |
| 587 |
< |
of those dynamic properties from Monte Carlo simulations. Molecular |
| 588 |
< |
Dynamics is a measurement of the evolution of the positions and |
| 589 |
< |
momenta of the particles in the system. The evolution of the system |
| 590 |
< |
obeys laws of classical mechanics, in most situations, there is no |
| 591 |
< |
need for the count of the quantum effects. For a real experiment, the |
| 592 |
< |
instantaneous positions and momenta of the particles in the system are |
| 593 |
< |
neither important nor measurable, the observable quantities are |
| 594 |
< |
usually a average value for a finite time interval. These quantities |
| 595 |
< |
are expressed as a function of positions and momenta in Melecular |
| 596 |
< |
Dynamics simulations. Like the thermal temperature of the system is |
| 489 |
< |
defined by |
| 585 |
> |
ensemble average in Monte Carlo simulations, due to the absence of the |
| 586 |
> |
time dependence, it is impossible to gain information on dynamic |
| 587 |
> |
properties from Monte Carlo simulations. Molecular Dynamics evolves |
| 588 |
> |
the positions and momenta of the particles in the system. The |
| 589 |
> |
evolution of the system obeys the laws of classical mechanics, and in |
| 590 |
> |
most situations, there is no need to account for quantum effects. In a |
| 591 |
> |
real experiment, the instantaneous positions and momenta of the |
| 592 |
> |
particles in the system are neither important nor measurable, the |
| 593 |
> |
observable quantities are usually an average value for a finite time |
| 594 |
> |
interval. These quantities are expressed as a function of positions |
| 595 |
> |
and momenta in Molecular Dynamics simulations. For example, |
| 596 |
> |
temperature of the system is defined by |
| 597 |
|
\begin{equation} |
| 598 |
< |
\frac{1}{2} k_B T = \langle \frac{1}{2} m v_\alpha \rangle, |
| 599 |
< |
\label{eq:temperature} |
| 598 |
> |
\frac{3}{2} N k_B T = \langle \sum_{i=1}^N \frac{1}{2} m_i v_i \rangle, |
| 599 |
> |
\label{Ineq:temperature} |
| 600 |
|
\end{equation} |
| 601 |
< |
here $m$ is the mass of the particle and $v_\alpha$ is the $\alpha$ |
| 602 |
< |
component of the velocity of the particle. The right side of |
| 603 |
< |
Eq.~\ref{eq:temperature} is the average kinetic energy of the |
| 497 |
< |
system. A simple Molecular Dynamics simulation scheme |
| 498 |
< |
is:~\cite{Frenkel1996} |
| 499 |
< |
\begin{enumerate} |
| 500 |
< |
\item\label{itm:initialize} Assign the initial positions and momenta |
| 501 |
< |
for the particles in the system. |
| 502 |
< |
\item\label{itm:calcForce} Calculate the forces. |
| 503 |
< |
\item\label{itm:equationofMotion} Integrate the equation of motion. |
| 504 |
< |
\begin{itemize} |
| 505 |
< |
\item Return to step~\ref{itm:calcForce} if the equillibrium is |
| 506 |
< |
not achieved. |
| 507 |
< |
\item Go to step~\ref{itm:calcAvg} if the equillibrium is |
| 508 |
< |
achieved. |
| 509 |
< |
\end{itemize} |
| 510 |
< |
\item\label{itm:calcAvg} Compute the quantities we are interested in. |
| 511 |
< |
\end{enumerate} |
| 512 |
< |
The initial positions of the particles are chosen as that there is no |
| 513 |
< |
overlap for the particles. The initial velocities at first are |
| 514 |
< |
distributed randomly to the particles, and then shifted to make the |
| 515 |
< |
momentum of the system $0$, at last scaled to the desired temperature |
| 516 |
< |
of the simulation according Eq.~\ref{eq:temperature}. |
| 601 |
> |
here $m_i$ is the mass of particle $i$ and $v_i$ is the velocity of |
| 602 |
> |
particle $i$. The right side of Eq.~\ref{Ineq:temperature} is the |
| 603 |
> |
average kinetic energy of the system. |
| 604 |
|
|
| 605 |
< |
The core of Molecular Dynamics simulations is step~\ref{itm:calcForce} |
| 606 |
< |
and~\ref{itm:equationofMotion}. The calculation of the forces are |
| 607 |
< |
often involved numerous effort, this is the most time consuming step |
| 608 |
< |
in the Molecular Dynamics scheme. The evaluation of the forces is |
| 609 |
< |
followed by |
| 605 |
> |
The initial positions of the particles are chosen so that there is no |
| 606 |
> |
overlap of the particles. The initial velocities at first are |
| 607 |
> |
distributed randomly to the particles using a Maxwell-Boltzmann |
| 608 |
> |
ditribution, and then shifted to make the total linear momentum of the |
| 609 |
> |
system $0$. |
| 610 |
> |
|
| 611 |
> |
The core of Molecular Dynamics simulations is the calculation of |
| 612 |
> |
forces and the integration algorithm. Calculation of the forces often |
| 613 |
> |
involves enormous effort. This is the most time consuming step in the |
| 614 |
> |
Molecular Dynamics scheme. Evaluation of the forces is mathematically |
| 615 |
> |
simple, |
| 616 |
|
\begin{equation} |
| 617 |
|
f(q) = - \frac{\partial U(q)}{\partial q}, |
| 618 |
< |
\label{eq:force} |
| 618 |
> |
\label{Ineq:force} |
| 619 |
|
\end{equation} |
| 620 |
< |
$U(q)$ is the potential of the system. Once the forces computed, are |
| 621 |
< |
the positions and velocities updated by integrating Newton's equation |
| 622 |
< |
of motion, |
| 620 |
> |
where $U(q)$ is the potential of the system. However, the numerical |
| 621 |
> |
details of this computation are often quite complex. Once the forces |
| 622 |
> |
computed, the positions and velocities are updated by integrating |
| 623 |
> |
Hamilton's equations of motion, |
| 624 |
> |
\begin{eqnarray} |
| 625 |
> |
\dot p_i & = & -\frac{\partial H}{\partial q_i} = -\frac{\partial |
| 626 |
> |
U(q_i)}{\partial q_i} = f(q_i) \\ |
| 627 |
> |
\dot q_i & = & p_i |
| 628 |
> |
\label{Ineq:newton} |
| 629 |
> |
\end{eqnarray} |
| 630 |
> |
The classic example of an integrating algorithm is the Verlet |
| 631 |
> |
algorithm, which is one of the simplest algorithms for integrating the |
| 632 |
> |
equations of motion. The Taylor expansion of the position at time $t$ |
| 633 |
> |
is |
| 634 |
|
\begin{equation} |
| 531 |
– |
f(q) = \frac{dp}{dt} = \frac{m dv}{dt}. |
| 532 |
– |
\label{eq:newton} |
| 533 |
– |
\end{equation} |
| 534 |
– |
Here is an example of integrating algorithms, Verlet algorithm, which |
| 535 |
– |
is one of the best algorithms to integrate Newton's equation of |
| 536 |
– |
motion. The Taylor expension of the position at time $t$ is |
| 537 |
– |
\begin{equation} |
| 635 |
|
q(t+\Delta t)= q(t) + v(t) \Delta t + \frac{f(t)}{2m}\Delta t^2 + |
| 636 |
|
\frac{\Delta t^3}{3!}\frac{\partial^3 q(t)}{\partial t^3} + |
| 637 |
|
\mathcal{O}(\Delta t^4) |
| 638 |
< |
\label{eq:verletFuture} |
| 638 |
> |
\label{Ineq:verletFuture} |
| 639 |
|
\end{equation} |
| 640 |
|
for a later time $t+\Delta t$, and |
| 641 |
|
\begin{equation} |
| 642 |
|
q(t-\Delta t)= q(t) - v(t) \Delta t + \frac{f(t)}{2m}\Delta t^2 - |
| 643 |
|
\frac{\Delta t^3}{3!}\frac{\partial^3 q(t)}{\partial t^3} + |
| 644 |
|
\mathcal{O}(\Delta t^4) , |
| 645 |
< |
\label{eq:verletPrevious} |
| 645 |
> |
\label{Ineq:verletPrevious} |
| 646 |
|
\end{equation} |
| 647 |
< |
for a previous time $t-\Delta t$. The summation of the |
| 648 |
< |
Eq.~\ref{eq:verletFuture} and~\ref{eq:verletPrevious} gives |
| 647 |
> |
for a previous time $t-\Delta t$. Adding Eq.~\ref{Ineq:verletFuture} |
| 648 |
> |
and~\ref{Ineq:verletPrevious} gives |
| 649 |
|
\begin{equation} |
| 650 |
|
q(t+\Delta t)+q(t-\Delta t) = |
| 651 |
|
2q(t) + \frac{f(t)}{m}\Delta t^2 + \mathcal{O}(\Delta t^4), |
| 652 |
< |
\label{eq:verletSum} |
| 652 |
> |
\label{Ineq:verletSum} |
| 653 |
|
\end{equation} |
| 654 |
|
so, the new position can be expressed as |
| 655 |
|
\begin{equation} |
| 656 |
|
q(t+\Delta t) \approx |
| 657 |
|
2q(t) - q(t-\Delta t) + \frac{f(t)}{m}\Delta t^2. |
| 658 |
< |
\label{eq:newPosition} |
| 658 |
> |
\label{Ineq:newPosition} |
| 659 |
|
\end{equation} |
| 660 |
< |
The higher order of the $\Delta t$ is omitted. |
| 660 |
> |
The higher order terms in $\Delta t$ are omitted. |
| 661 |
|
|
| 662 |
< |
Numerous technics and tricks are applied to Molecular Dynamics |
| 663 |
< |
simulation to gain more efficiency or more accuracy. The simulation |
| 664 |
< |
engine used in this dissertation for the Molecular Dynamics |
| 665 |
< |
simulations is {\sc oopse}, more details of the algorithms and |
| 666 |
< |
technics can be found in~\cite{Meineke2005}. |
| 662 |
> |
Numerous techniques and tricks have been applied to Molecular Dynamics |
| 663 |
> |
simulations to gain greater efficiency or accuracy. The engine used in |
| 664 |
> |
this dissertation for the Molecular Dynamics simulations is {\sc |
| 665 |
> |
oopse}. More details of the algorithms and techniques used in this |
| 666 |
> |
code can be found in Ref.~\cite{Meineke2005}. |
| 667 |
|
|
| 668 |
|
\subsection{Langevin Dynamics\label{In:ssec:ld}} |
| 669 |
|
In many cases, the properites of the solvent in a system, like the |
| 670 |
< |
lipid-water system studied in this dissertation, are less important to |
| 671 |
< |
the researchers. However, the major computational expense is spent on |
| 672 |
< |
the solvent in the Molecular Dynamics simulations because of the large |
| 673 |
< |
number of the solvent molecules compared to that of solute molecules, |
| 674 |
< |
the ratio of the number of lipid molecules to the number of water |
| 670 |
> |
water in the lipid-water system studied in this dissertation, are less |
| 671 |
> |
interesting to the researchers than the behavior of the |
| 672 |
> |
solute. However, the major computational expense is ofter the |
| 673 |
> |
solvent-solvent interation, this is due to the large number of the |
| 674 |
> |
solvent molecules when compared to the number of solute molecules, the |
| 675 |
> |
ratio of the number of lipid molecules to the number of water |
| 676 |
|
molecules is $1:25$ in our lipid-water system. The efficiency of the |
| 677 |
< |
Molecular Dynamics simulations is greatly reduced. |
| 677 |
> |
Molecular Dynamics simulations is greatly reduced, with up to 85\% of |
| 678 |
> |
CPU time spent calculating only water-water interactions. |
| 679 |
|
|
| 680 |
< |
As an extension of the Molecular Dynamics simulations, the Langevin |
| 681 |
< |
Dynamics seeks a way to avoid integrating equation of motion for |
| 682 |
< |
solvent particles without losing the Brownian properites of solute |
| 683 |
< |
particles. A common approximation is that the coupling of the solute |
| 684 |
< |
and solvent is expressed as a set of harmonic oscillators. So the |
| 685 |
< |
Hamiltonian of such a system is written as |
| 680 |
> |
As an extension of the Molecular Dynamics methodologies, Langevin |
| 681 |
> |
Dynamics seeks a way to avoid integrating the equations of motion for |
| 682 |
> |
solvent particles without losing the solvent effects on the solute |
| 683 |
> |
particles. One common approximation is to express the coupling of the |
| 684 |
> |
solute and solvent as a set of harmonic oscillators. The Hamiltonian |
| 685 |
> |
of such a system is written as |
| 686 |
|
\begin{equation} |
| 687 |
|
H = \frac{p^2}{2m} + U(q) + H_B + \Delta U(q), |
| 688 |
< |
\label{eq:hamiltonianofCoupling} |
| 688 |
> |
\label{Ineq:hamiltonianofCoupling} |
| 689 |
|
\end{equation} |
| 690 |
< |
where $H_B$ is the Hamiltonian of the bath which equals to |
| 690 |
> |
where $H_B$ is the Hamiltonian of the bath which is a set of N |
| 691 |
> |
harmonic oscillators |
| 692 |
|
\begin{equation} |
| 693 |
|
H_B = \sum_{\alpha = 1}^{N} \left\{ \frac{p_\alpha^2}{2m_\alpha} + |
| 694 |
|
\frac{1}{2} m_\alpha \omega_\alpha^2 q_\alpha^2\right\}, |
| 695 |
< |
\label{eq:hamiltonianofBath} |
| 695 |
> |
\label{Ineq:hamiltonianofBath} |
| 696 |
|
\end{equation} |
| 697 |
< |
$\alpha$ is all the degree of freedoms of the bath, $\omega$ is the |
| 698 |
< |
bath frequency, and $\Delta U(q)$ is the bilinear coupling given by |
| 697 |
> |
$\alpha$ runs over all the degree of freedoms of the bath, |
| 698 |
> |
$\omega_\alpha$ is the bath frequency of oscillator $\alpha$, and |
| 699 |
> |
$\Delta U(q)$ is the bilinear coupling given by |
| 700 |
|
\begin{equation} |
| 701 |
|
\Delta U = -\sum_{\alpha = 1}^{N} g_\alpha q_\alpha q, |
| 702 |
< |
\label{eq:systemBathCoupling} |
| 702 |
> |
\label{Ineq:systemBathCoupling} |
| 703 |
|
\end{equation} |
| 704 |
< |
where $g$ is the coupling constant. By solving the Hamilton's equation |
| 705 |
< |
of motion, the {\it Generalized Langevin Equation} for this system is |
| 706 |
< |
derived to |
| 704 |
> |
where $g_\alpha$ is the coupling constant for oscillator $\alpha$. By |
| 705 |
> |
solving the Hamilton's equations of motion, the {\it Generalized |
| 706 |
> |
Langevin Equation} for this system is derived as |
| 707 |
|
\begin{equation} |
| 708 |
|
m \ddot q = -\frac{\partial W(q)}{\partial q} - \int_0^t \xi(t) \dot q(t-t')dt' + R(t), |
| 709 |
< |
\label{eq:gle} |
| 709 |
> |
\label{Ineq:gle} |
| 710 |
|
\end{equation} |
| 711 |
|
with mean force, |
| 712 |
|
\begin{equation} |
| 713 |
|
W(q) = U(q) - \sum_{\alpha = 1}^N \frac{g_\alpha^2}{2m_\alpha |
| 714 |
< |
\omega_\alpha^2}q^2, |
| 715 |
< |
\label{eq:meanForce} |
| 714 |
> |
\omega_\alpha^2}q^2. |
| 715 |
> |
\label{Ineq:meanForce} |
| 716 |
|
\end{equation} |
| 717 |
< |
being only a dependence of coordinates of the solute particles, {\it |
| 718 |
< |
friction kernel}, |
| 717 |
> |
The {\it friction kernel}, $\xi(t)$, depends only on the coordinates |
| 718 |
> |
of the solute particles, |
| 719 |
|
\begin{equation} |
| 720 |
|
\xi(t) = \sum_{\alpha = 1}^N \frac{-g_\alpha}{m_\alpha |
| 721 |
|
\omega_\alpha} \cos(\omega_\alpha t), |
| 722 |
< |
\label{eq:xiforGLE} |
| 722 |
> |
\label{Ineq:xiforGLE} |
| 723 |
|
\end{equation} |
| 724 |
< |
and the random force, |
| 724 |
> |
and a ``random'' force, |
| 725 |
|
\begin{equation} |
| 726 |
|
R(t) = \sum_{\alpha = 1}^N \left( g_\alpha q_\alpha(0)-\frac{g_\alpha}{m_\alpha |
| 727 |
|
\omega_\alpha^2}q(0)\right) \cos(\omega_\alpha t) + \frac{\dot |
| 728 |
|
q_\alpha(0)}{\omega_\alpha} \sin(\omega_\alpha t), |
| 729 |
< |
\label{eq:randomForceforGLE} |
| 729 |
> |
\label{Ineq:randomForceforGLE} |
| 730 |
|
\end{equation} |
| 731 |
< |
as only a dependence of the initial conditions. The relationship of |
| 732 |
< |
friction kernel $\xi(t)$ and random force $R(t)$ is given by |
| 731 |
> |
depends only on the initial conditions. The relationship of friction |
| 732 |
> |
kernel $\xi(t)$ and random force $R(t)$ is given by the second |
| 733 |
> |
fluctuation dissipation theorem, |
| 734 |
|
\begin{equation} |
| 735 |
< |
\xi(t) = \frac{1}{k_B T} \langle R(t)R(0) \rangle |
| 736 |
< |
\label{eq:relationshipofXiandR} |
| 735 |
> |
\xi(t) = \frac{1}{k_B T} \langle R(t)R(0) \rangle. |
| 736 |
> |
\label{Ineq:relationshipofXiandR} |
| 737 |
|
\end{equation} |
| 738 |
< |
from their definitions. In Langevin limit, the friction is treated |
| 739 |
< |
static, which means |
| 738 |
> |
In the harmonic bath this relation is exact and provable from the |
| 739 |
> |
definitions of these quantities. In the limit of static friction, |
| 740 |
|
\begin{equation} |
| 741 |
|
\xi(t) = 2 \xi_0 \delta(t). |
| 742 |
< |
\label{eq:xiofStaticFriction} |
| 742 |
> |
\label{Ineq:xiofStaticFriction} |
| 743 |
|
\end{equation} |
| 744 |
< |
After substitude $\xi(t)$ into Eq.~\ref{eq:gle} with |
| 745 |
< |
Eq.~\ref{eq:xiofStaticFriction}, {\it Langevin Equation} is extracted |
| 746 |
< |
to |
| 744 |
> |
After substituting $\xi(t)$ into Eq.~\ref{Ineq:gle} with |
| 745 |
> |
Eq.~\ref{Ineq:xiofStaticFriction}, the {\it Langevin Equation} is |
| 746 |
> |
extracted, |
| 747 |
|
\begin{equation} |
| 748 |
|
m \ddot q = -\frac{\partial U(q)}{\partial q} - \xi \dot q(t) + R(t). |
| 749 |
< |
\label{eq:langevinEquation} |
| 749 |
> |
\label{Ineq:langevinEquation} |
| 750 |
|
\end{equation} |
| 751 |
< |
The applying of Langevin Equation to dynamic simulations is discussed |
| 752 |
< |
in Ch.~\ref{chap:ld}. |
| 751 |
> |
Application of the Langevin Equation to dynamic simulations is |
| 752 |
> |
discussed in Ch.~\ref{chap:ld}. |
