| 6 |
|
Closely related to Classical Mechanics, Molecular Dynamics |
| 7 |
|
simulations are carried out by integrating the equations of motion |
| 8 |
|
for a given system of particles. There are three fundamental ideas |
| 9 |
< |
behind classical mechanics. Firstly, One can determine the state of |
| 9 |
> |
behind classical mechanics. Firstly, one can determine the state of |
| 10 |
|
a mechanical system at any time of interest; Secondly, all the |
| 11 |
|
mechanical properties of the system at that time can be determined |
| 12 |
|
by combining the knowledge of the properties of the system with the |
| 17 |
|
\subsection{\label{introSection:newtonian}Newtonian Mechanics} |
| 18 |
|
The discovery of Newton's three laws of mechanics which govern the |
| 19 |
|
motion of particles is the foundation of the classical mechanics. |
| 20 |
< |
Newton¡¯s first law defines a class of inertial frames. Inertial |
| 20 |
> |
Newton's first law defines a class of inertial frames. Inertial |
| 21 |
|
frames are reference frames where a particle not interacting with |
| 22 |
|
other bodies will move with constant speed in the same direction. |
| 23 |
< |
With respect to inertial frames Newton¡¯s second law has the form |
| 23 |
> |
With respect to inertial frames, Newton's second law has the form |
| 24 |
|
\begin{equation} |
| 25 |
< |
F = \frac {dp}{dt} = \frac {mv}{dt} |
| 25 |
> |
F = \frac {dp}{dt} = \frac {mdv}{dt} |
| 26 |
|
\label{introEquation:newtonSecondLaw} |
| 27 |
|
\end{equation} |
| 28 |
|
A point mass interacting with other bodies moves with the |
| 29 |
|
acceleration along the direction of the force acting on it. Let |
| 30 |
|
$F_{ij}$ be the force that particle $i$ exerts on particle $j$, and |
| 31 |
|
$F_{ji}$ be the force that particle $j$ exerts on particle $i$. |
| 32 |
< |
Newton¡¯s third law states that |
| 32 |
> |
Newton's third law states that |
| 33 |
|
\begin{equation} |
| 34 |
|
F_{ij} = -F_{ji} |
| 35 |
|
\label{introEquation:newtonThirdLaw} |
| 46 |
|
\end{equation} |
| 47 |
|
The torque $\tau$ with respect to the same origin is defined to be |
| 48 |
|
\begin{equation} |
| 49 |
< |
N \equiv r \times F \label{introEquation:torqueDefinition} |
| 49 |
> |
\tau \equiv r \times F \label{introEquation:torqueDefinition} |
| 50 |
|
\end{equation} |
| 51 |
|
Differentiating Eq.~\ref{introEquation:angularMomentumDefinition}, |
| 52 |
|
\[ |
| 59 |
|
\] |
| 60 |
|
thus, |
| 61 |
|
\begin{equation} |
| 62 |
< |
\dot L = r \times \dot p = N |
| 62 |
> |
\dot L = r \times \dot p = \tau |
| 63 |
|
\end{equation} |
| 64 |
|
If there are no external torques acting on a body, the angular |
| 65 |
|
momentum of it is conserved. The last conservation theorem state |
| 68 |
|
\end{equation} |
| 69 |
|
is conserved. All of these conserved quantities are |
| 70 |
|
important factors to determine the quality of numerical integration |
| 71 |
< |
scheme for rigid body \cite{Dullweber1997}. |
| 71 |
> |
schemes for rigid bodies \cite{Dullweber1997}. |
| 72 |
|
|
| 73 |
|
\subsection{\label{introSection:lagrangian}Lagrangian Mechanics} |
| 74 |
|
|
| 75 |
< |
Newtonian Mechanics suffers from two important limitations: it |
| 76 |
< |
describes their motion in special cartesian coordinate systems. |
| 77 |
< |
Another limitation of Newtonian mechanics becomes obvious when we |
| 78 |
< |
try to describe systems with large numbers of particles. It becomes |
| 79 |
< |
very difficult to predict the properties of the system by carrying |
| 80 |
< |
out calculations involving the each individual interaction between |
| 81 |
< |
all the particles, even if we know all of the details of the |
| 82 |
< |
interaction. In order to overcome some of the practical difficulties |
| 83 |
< |
which arise in attempts to apply Newton's equation to complex |
| 84 |
< |
system, alternative procedures may be developed. |
| 75 |
> |
Newtonian Mechanics suffers from two important limitations: motions |
| 76 |
> |
can only be described in cartesian coordinate systems. Moreover, It |
| 77 |
> |
become impossible to predict analytically the properties of the |
| 78 |
> |
system even if we know all of the details of the interaction. In |
| 79 |
> |
order to overcome some of the practical difficulties which arise in |
| 80 |
> |
attempts to apply Newton's equation to complex system, approximate |
| 81 |
> |
numerical procedures may be developed. |
| 82 |
|
|
| 83 |
< |
\subsubsection{\label{introSection:halmiltonPrinciple}Hamilton's |
| 84 |
< |
Principle} |
| 83 |
> |
\subsubsection{\label{introSection:halmiltonPrinciple}\textbf{Hamilton's |
| 84 |
> |
Principle}} |
| 85 |
|
|
| 86 |
|
Hamilton introduced the dynamical principle upon which it is |
| 87 |
< |
possible to base all of mechanics and, indeed, most of classical |
| 88 |
< |
physics. Hamilton's Principle may be stated as follow, |
| 87 |
> |
possible to base all of mechanics and most of classical physics. |
| 88 |
> |
Hamilton's Principle may be stated as follows, |
| 89 |
|
|
| 90 |
|
The actual trajectory, along which a dynamical system may move from |
| 91 |
|
one point to another within a specified time, is derived by finding |
| 92 |
|
the path which minimizes the time integral of the difference between |
| 93 |
< |
the kinetic, $K$, and potential energies, $U$ \cite{Tolman1979}. |
| 93 |
> |
the kinetic, $K$, and potential energies, $U$. |
| 94 |
|
\begin{equation} |
| 95 |
|
\delta \int_{t_1 }^{t_2 } {(K - U)dt = 0} , |
| 96 |
|
\label{introEquation:halmitonianPrinciple1} |
| 97 |
|
\end{equation} |
| 98 |
|
|
| 99 |
|
For simple mechanical systems, where the forces acting on the |
| 100 |
< |
different part are derivable from a potential and the velocities are |
| 101 |
< |
small compared with that of light, the Lagrangian function $L$ can |
| 102 |
< |
be define as the difference between the kinetic energy of the system |
| 106 |
< |
and its potential energy, |
| 100 |
> |
different parts are derivable from a potential, the Lagrangian |
| 101 |
> |
function $L$ can be defined as the difference between the kinetic |
| 102 |
> |
energy of the system and its potential energy, |
| 103 |
|
\begin{equation} |
| 104 |
|
L \equiv K - U = L(q_i ,\dot q_i ) , |
| 105 |
|
\label{introEquation:lagrangianDef} |
| 110 |
|
\label{introEquation:halmitonianPrinciple2} |
| 111 |
|
\end{equation} |
| 112 |
|
|
| 113 |
< |
\subsubsection{\label{introSection:equationOfMotionLagrangian}The |
| 114 |
< |
Equations of Motion in Lagrangian Mechanics} |
| 113 |
> |
\subsubsection{\label{introSection:equationOfMotionLagrangian}\textbf{The |
| 114 |
> |
Equations of Motion in Lagrangian Mechanics}} |
| 115 |
|
|
| 116 |
< |
For a holonomic system of $f$ degrees of freedom, the equations of |
| 117 |
< |
motion in the Lagrangian form is |
| 116 |
> |
For a system of $f$ degrees of freedom, the equations of motion in |
| 117 |
> |
the Lagrangian form is |
| 118 |
|
\begin{equation} |
| 119 |
|
\frac{d}{{dt}}\frac{{\partial L}}{{\partial \dot q_i }} - |
| 120 |
|
\frac{{\partial L}}{{\partial q_i }} = 0,{\rm{ }}i = 1, \ldots,f |
| 128 |
|
Arising from Lagrangian Mechanics, Hamiltonian Mechanics was |
| 129 |
|
introduced by William Rowan Hamilton in 1833 as a re-formulation of |
| 130 |
|
classical mechanics. If the potential energy of a system is |
| 131 |
< |
independent of generalized velocities, the generalized momenta can |
| 136 |
< |
be defined as |
| 131 |
> |
independent of velocities, the momenta can be defined as |
| 132 |
|
\begin{equation} |
| 133 |
|
p_i = \frac{\partial L}{\partial \dot q_i} |
| 134 |
|
\label{introEquation:generalizedMomenta} |
| 167 |
|
By identifying the coefficients of $dq_k$, $dp_k$ and dt, we can |
| 168 |
|
find |
| 169 |
|
\begin{equation} |
| 170 |
< |
\frac{{\partial H}}{{\partial p_k }} = q_k |
| 170 |
> |
\frac{{\partial H}}{{\partial p_k }} = \dot {q_k} |
| 171 |
|
\label{introEquation:motionHamiltonianCoordinate} |
| 172 |
|
\end{equation} |
| 173 |
|
\begin{equation} |
| 174 |
< |
\frac{{\partial H}}{{\partial q_k }} = - p_k |
| 174 |
> |
\frac{{\partial H}}{{\partial q_k }} = - \dot {p_k} |
| 175 |
|
\label{introEquation:motionHamiltonianMomentum} |
| 176 |
|
\end{equation} |
| 177 |
|
and |
| 188 |
|
|
| 189 |
|
An important difference between Lagrangian approach and the |
| 190 |
|
Hamiltonian approach is that the Lagrangian is considered to be a |
| 191 |
< |
function of the generalized velocities $\dot q_i$ and the |
| 192 |
< |
generalized coordinates $q_i$, while the Hamiltonian is considered |
| 193 |
< |
to be a function of the generalized momenta $p_i$ and the conjugate |
| 194 |
< |
generalized coordinate $q_i$. Hamiltonian Mechanics is more |
| 195 |
< |
appropriate for application to statistical mechanics and quantum |
| 196 |
< |
mechanics, since it treats the coordinate and its time derivative as |
| 197 |
< |
independent variables and it only works with 1st-order differential |
| 203 |
< |
equations\cite{Marion1990}. |
| 191 |
> |
function of the generalized velocities $\dot q_i$ and coordinates |
| 192 |
> |
$q_i$, while the Hamiltonian is considered to be a function of the |
| 193 |
> |
generalized momenta $p_i$ and the conjugate coordinates $q_i$. |
| 194 |
> |
Hamiltonian Mechanics is more appropriate for application to |
| 195 |
> |
statistical mechanics and quantum mechanics, since it treats the |
| 196 |
> |
coordinate and its time derivative as independent variables and it |
| 197 |
> |
only works with 1st-order differential equations\cite{Marion1990}. |
| 198 |
|
|
| 199 |
|
In Newtonian Mechanics, a system described by conservative forces |
| 200 |
|
conserves the total energy \ref{introEquation:energyConservation}. |
| 224 |
|
possible states. Each possible state of the system corresponds to |
| 225 |
|
one unique point in the phase space. For mechanical systems, the |
| 226 |
|
phase space usually consists of all possible values of position and |
| 227 |
< |
momentum variables. Consider a dynamic system in a cartesian space, |
| 228 |
< |
where each of the $6f$ coordinates and momenta is assigned to one of |
| 229 |
< |
$6f$ mutually orthogonal axes, the phase space of this system is a |
| 230 |
< |
$6f$ dimensional space. A point, $x = (q_1 , \ldots ,q_f ,p_1 , |
| 231 |
< |
\ldots ,p_f )$, with a unique set of values of $6f$ coordinates and |
| 232 |
< |
momenta is a phase space vector. |
| 227 |
> |
momentum variables. Consider a dynamic system of $f$ particles in a |
| 228 |
> |
cartesian space, where each of the $6f$ coordinates and momenta is |
| 229 |
> |
assigned to one of $6f$ mutually orthogonal axes, the phase space of |
| 230 |
> |
this system is a $6f$ dimensional space. A point, $x = (q_1 , \ldots |
| 231 |
> |
,q_f ,p_1 , \ldots ,p_f )$, with a unique set of values of $6f$ |
| 232 |
> |
coordinates and momenta is a phase space vector. |
| 233 |
|
|
| 234 |
+ |
%%%fix me |
| 235 |
|
A microscopic state or microstate of a classical system is |
| 236 |
|
specification of the complete phase space vector of a system at any |
| 237 |
|
instant in time. An ensemble is defined as a collection of systems |
| 252 |
|
regions of the phase space. The condition of an ensemble at any time |
| 253 |
|
can be regarded as appropriately specified by the density $\rho$ |
| 254 |
|
with which representative points are distributed over the phase |
| 255 |
< |
space. The density of distribution for an ensemble with $f$ degrees |
| 256 |
< |
of freedom is defined as, |
| 255 |
> |
space. The density distribution for an ensemble with $f$ degrees of |
| 256 |
> |
freedom is defined as, |
| 257 |
|
\begin{equation} |
| 258 |
|
\rho = \rho (q_1 , \ldots ,q_f ,p_1 , \ldots ,p_f ,t). |
| 259 |
|
\label{introEquation:densityDistribution} |
| 260 |
|
\end{equation} |
| 261 |
|
Governed by the principles of mechanics, the phase points change |
| 262 |
< |
their value which would change the density at any time at phase |
| 263 |
< |
space. Hence, the density of distribution is also to be taken as a |
| 262 |
> |
their locations which would change the density at any time at phase |
| 263 |
> |
space. Hence, the density distribution is also to be taken as a |
| 264 |
|
function of the time. |
| 265 |
|
|
| 266 |
|
The number of systems $\delta N$ at time $t$ can be determined by, |
| 268 |
|
\delta N = \rho (q,p,t)dq_1 \ldots dq_f dp_1 \ldots dp_f. |
| 269 |
|
\label{introEquation:deltaN} |
| 270 |
|
\end{equation} |
| 271 |
< |
Assuming a large enough population of systems are exploited, we can |
| 272 |
< |
sufficiently approximate $\delta N$ without introducing |
| 273 |
< |
discontinuity when we go from one region in the phase space to |
| 274 |
< |
another. By integrating over the whole phase space, |
| 271 |
> |
Assuming a large enough population of systems, we can sufficiently |
| 272 |
> |
approximate $\delta N$ without introducing discontinuity when we go |
| 273 |
> |
from one region in the phase space to another. By integrating over |
| 274 |
> |
the whole phase space, |
| 275 |
|
\begin{equation} |
| 276 |
|
N = \int { \ldots \int {\rho (q,p,t)dq_1 } ...dq_f dp_1 } ...dp_f |
| 277 |
|
\label{introEquation:totalNumberSystem} |
| 283 |
|
{\rho (q,p,t)dq_1 } ...dq_f dp_1 } ...dp_f }}. |
| 284 |
|
\label{introEquation:unitProbability} |
| 285 |
|
\end{equation} |
| 286 |
< |
With the help of Equation(\ref{introEquation:unitProbability}) and |
| 287 |
< |
the knowledge of the system, it is possible to calculate the average |
| 286 |
> |
With the help of Eq.~\ref{introEquation:unitProbability} and the |
| 287 |
> |
knowledge of the system, it is possible to calculate the average |
| 288 |
|
value of any desired quantity which depends on the coordinates and |
| 289 |
|
momenta of the system. Even when the dynamics of the real system is |
| 290 |
|
complex, or stochastic, or even discontinuous, the average |
| 291 |
< |
properties of the ensemble of possibilities as a whole may still |
| 292 |
< |
remain well defined. For a classical system in thermal equilibrium |
| 293 |
< |
with its environment, the ensemble average of a mechanical quantity, |
| 294 |
< |
$\langle A(q , p) \rangle_t$, takes the form of an integral over the |
| 295 |
< |
phase space of the system, |
| 291 |
> |
properties of the ensemble of possibilities as a whole remaining |
| 292 |
> |
well defined. For a classical system in thermal equilibrium with its |
| 293 |
> |
environment, the ensemble average of a mechanical quantity, $\langle |
| 294 |
> |
A(q , p) \rangle_t$, takes the form of an integral over the phase |
| 295 |
> |
space of the system, |
| 296 |
|
\begin{equation} |
| 297 |
|
\langle A(q , p) \rangle_t = \frac{{\int { \ldots \int {A(q,p)\rho |
| 298 |
|
(q,p,t)dq_1 } ...dq_f dp_1 } ...dp_f }}{{\int { \ldots \int {\rho |
| 302 |
|
|
| 303 |
|
There are several different types of ensembles with different |
| 304 |
|
statistical characteristics. As a function of macroscopic |
| 305 |
< |
parameters, such as temperature \textit{etc}, partition function can |
| 306 |
< |
be used to describe the statistical properties of a system in |
| 305 |
> |
parameters, such as temperature \textit{etc}, the partition function |
| 306 |
> |
can be used to describe the statistical properties of a system in |
| 307 |
|
thermodynamic equilibrium. |
| 308 |
|
|
| 309 |
|
As an ensemble of systems, each of which is known to be thermally |
| 310 |
< |
isolated and conserve energy, Microcanonical ensemble(NVE) has a |
| 311 |
< |
partition function like, |
| 310 |
> |
isolated and conserve energy, the Microcanonical ensemble (NVE) has |
| 311 |
> |
a partition function like, |
| 312 |
|
\begin{equation} |
| 313 |
|
\Omega (N,V,E) = e^{\beta TS} \label{introEquation:NVEPartition}. |
| 314 |
|
\end{equation} |
| 315 |
< |
A canonical ensemble(NVT)is an ensemble of systems, each of which |
| 315 |
> |
A canonical ensemble (NVT)is an ensemble of systems, each of which |
| 316 |
|
can share its energy with a large heat reservoir. The distribution |
| 317 |
|
of the total energy amongst the possible dynamical states is given |
| 318 |
|
by the partition function, |
| 321 |
|
\label{introEquation:NVTPartition} |
| 322 |
|
\end{equation} |
| 323 |
|
Here, $A$ is the Helmholtz free energy which is defined as $ A = U - |
| 324 |
< |
TS$. Since most experiment are carried out under constant pressure |
| 325 |
< |
condition, isothermal-isobaric ensemble(NPT) play a very important |
| 326 |
< |
role in molecular simulation. The isothermal-isobaric ensemble allow |
| 327 |
< |
the system to exchange energy with a heat bath of temperature $T$ |
| 328 |
< |
and to change the volume as well. Its partition function is given as |
| 324 |
> |
TS$. Since most experiments are carried out under constant pressure |
| 325 |
> |
condition, the isothermal-isobaric ensemble (NPT) plays a very |
| 326 |
> |
important role in molecular simulations. The isothermal-isobaric |
| 327 |
> |
ensemble allow the system to exchange energy with a heat bath of |
| 328 |
> |
temperature $T$ and to change the volume as well. Its partition |
| 329 |
> |
function is given as |
| 330 |
|
\begin{equation} |
| 331 |
|
\Delta (N,P,T) = - e^{\beta G}. |
| 332 |
|
\label{introEquation:NPTPartition} |
| 335 |
|
|
| 336 |
|
\subsection{\label{introSection:liouville}Liouville's theorem} |
| 337 |
|
|
| 338 |
< |
The Liouville's theorem is the foundation on which statistical |
| 339 |
< |
mechanics rests. It describes the time evolution of phase space |
| 338 |
> |
Liouville's theorem is the foundation on which statistical mechanics |
| 339 |
> |
rests. It describes the time evolution of the phase space |
| 340 |
|
distribution function. In order to calculate the rate of change of |
| 341 |
< |
$\rho$, we begin from Equation(\ref{introEquation:deltaN}). If we |
| 342 |
< |
consider the two faces perpendicular to the $q_1$ axis, which are |
| 343 |
< |
located at $q_1$ and $q_1 + \delta q_1$, the number of phase points |
| 344 |
< |
leaving the opposite face is given by the expression, |
| 341 |
> |
$\rho$, we begin from Eq.~\ref{introEquation:deltaN}. If we consider |
| 342 |
> |
the two faces perpendicular to the $q_1$ axis, which are located at |
| 343 |
> |
$q_1$ and $q_1 + \delta q_1$, the number of phase points leaving the |
| 344 |
> |
opposite face is given by the expression, |
| 345 |
|
\begin{equation} |
| 346 |
|
\left( {\rho + \frac{{\partial \rho }}{{\partial q_1 }}\delta q_1 } |
| 347 |
|
\right)\left( {\dot q_1 + \frac{{\partial \dot q_1 }}{{\partial q_1 |
| 365 |
|
+ \frac{{\partial \dot p_i }}{{\partial p_i }}} \right)} = 0 , |
| 366 |
|
\end{equation} |
| 367 |
|
which cancels the first terms of the right hand side. Furthermore, |
| 368 |
< |
divining $ \delta q_1 \ldots \delta q_f \delta p_1 \ldots \delta |
| 368 |
> |
dividing $ \delta q_1 \ldots \delta q_f \delta p_1 \ldots \delta |
| 369 |
|
p_f $ in both sides, we can write out Liouville's theorem in a |
| 370 |
|
simple form, |
| 371 |
|
\begin{equation} |
| 377 |
|
|
| 378 |
|
Liouville's theorem states that the distribution function is |
| 379 |
|
constant along any trajectory in phase space. In classical |
| 380 |
< |
statistical mechanics, since the number of particles in the system |
| 381 |
< |
is huge, we may be able to believe the system is stationary, |
| 380 |
> |
statistical mechanics, since the number of members in an ensemble is |
| 381 |
> |
huge and constant, we can assume the local density has no reason |
| 382 |
> |
(other than classical mechanics) to change, |
| 383 |
|
\begin{equation} |
| 384 |
|
\frac{{\partial \rho }}{{\partial t}} = 0. |
| 385 |
|
\label{introEquation:stationary} |
| 392 |
|
\label{introEquation:densityAndHamiltonian} |
| 393 |
|
\end{equation} |
| 394 |
|
|
| 395 |
< |
\subsubsection{\label{introSection:phaseSpaceConservation}Conservation of Phase Space} |
| 395 |
> |
\subsubsection{\label{introSection:phaseSpaceConservation}\textbf{Conservation of Phase Space}} |
| 396 |
|
Lets consider a region in the phase space, |
| 397 |
|
\begin{equation} |
| 398 |
|
\delta v = \int { \ldots \int {dq_1 } ...dq_f dp_1 } ..dp_f . |
| 399 |
|
\end{equation} |
| 400 |
|
If this region is small enough, the density $\rho$ can be regarded |
| 401 |
< |
as uniform over the whole phase space. Thus, the number of phase |
| 402 |
< |
points inside this region is given by, |
| 401 |
> |
as uniform over the whole integral. Thus, the number of phase points |
| 402 |
> |
inside this region is given by, |
| 403 |
|
\begin{equation} |
| 404 |
|
\delta N = \rho \delta v = \rho \int { \ldots \int {dq_1 } ...dq_f |
| 405 |
|
dp_1 } ..dp_f. |
| 411 |
|
\end{equation} |
| 412 |
|
With the help of stationary assumption |
| 413 |
|
(\ref{introEquation:stationary}), we obtain the principle of the |
| 414 |
< |
\emph{conservation of extension in phase space}, |
| 414 |
> |
\emph{conservation of volume in phase space}, |
| 415 |
|
\begin{equation} |
| 416 |
|
\frac{d}{{dt}}(\delta v) = \frac{d}{{dt}}\int { \ldots \int {dq_1 } |
| 417 |
|
...dq_f dp_1 } ..dp_f = 0. |
| 418 |
|
\label{introEquation:volumePreserving} |
| 419 |
|
\end{equation} |
| 420 |
|
|
| 421 |
< |
\subsubsection{\label{introSection:liouvilleInOtherForms}Liouville's Theorem in Other Forms} |
| 421 |
> |
\subsubsection{\label{introSection:liouvilleInOtherForms}\textbf{Liouville's Theorem in Other Forms}} |
| 422 |
|
|
| 423 |
|
Liouville's theorem can be expresses in a variety of different forms |
| 424 |
|
which are convenient within different contexts. For any two function |
| 432 |
|
\label{introEquation:poissonBracket} |
| 433 |
|
\end{equation} |
| 434 |
|
Substituting equations of motion in Hamiltonian formalism( |
| 435 |
< |
\ref{introEquation:motionHamiltonianCoordinate} , |
| 436 |
< |
\ref{introEquation:motionHamiltonianMomentum} ) into |
| 437 |
< |
(\ref{introEquation:liouvilleTheorem}), we can rewrite Liouville's |
| 438 |
< |
theorem using Poisson bracket notion, |
| 435 |
> |
Eq.~\ref{introEquation:motionHamiltonianCoordinate} , |
| 436 |
> |
Eq.~\ref{introEquation:motionHamiltonianMomentum} ) into |
| 437 |
> |
(Eq.~\ref{introEquation:liouvilleTheorem}), we can rewrite |
| 438 |
> |
Liouville's theorem using Poisson bracket notion, |
| 439 |
|
\begin{equation} |
| 440 |
|
\left( {\frac{{\partial \rho }}{{\partial t}}} \right) = - \left\{ |
| 441 |
|
{\rho ,H} \right\}. |
| 460 |
|
Various thermodynamic properties can be calculated from Molecular |
| 461 |
|
Dynamics simulation. By comparing experimental values with the |
| 462 |
|
calculated properties, one can determine the accuracy of the |
| 463 |
< |
simulation and the quality of the underlying model. However, both of |
| 464 |
< |
experiment and computer simulation are usually performed during a |
| 463 |
> |
simulation and the quality of the underlying model. However, both |
| 464 |
> |
experiments and computer simulations are usually performed during a |
| 465 |
|
certain time interval and the measurements are averaged over a |
| 466 |
|
period of them which is different from the average behavior of |
| 467 |
< |
many-body system in Statistical Mechanics. Fortunately, Ergodic |
| 468 |
< |
Hypothesis is proposed to make a connection between time average and |
| 469 |
< |
ensemble average. It states that time average and average over the |
| 467 |
> |
many-body system in Statistical Mechanics. Fortunately, the Ergodic |
| 468 |
> |
Hypothesis makes a connection between time average and the ensemble |
| 469 |
> |
average. It states that the time average and average over the |
| 470 |
|
statistical ensemble are identical \cite{Frenkel1996, Leach2001}. |
| 471 |
|
\begin{equation} |
| 472 |
|
\langle A(q , p) \rangle_t = \mathop {\lim }\limits_{t \to \infty } |
| 488 |
|
choice\cite{Frenkel1996}. |
| 489 |
|
|
| 490 |
|
\section{\label{introSection:geometricIntegratos}Geometric Integrators} |
| 491 |
< |
A variety of numerical integrators were proposed to simulate the |
| 492 |
< |
motions. They usually begin with an initial conditionals and move |
| 493 |
< |
the objects in the direction governed by the differential equations. |
| 494 |
< |
However, most of them ignore the hidden physical law contained |
| 495 |
< |
within the equations. Since 1990, geometric integrators, which |
| 496 |
< |
preserve various phase-flow invariants such as symplectic structure, |
| 497 |
< |
volume and time reversal symmetry, are developed to address this |
| 498 |
< |
issue\cite{Dullweber1997, McLachlan1998, Leimkuhler1999}. The |
| 499 |
< |
velocity verlet method, which happens to be a simple example of |
| 500 |
< |
symplectic integrator, continues to gain its popularity in molecular |
| 501 |
< |
dynamics community. This fact can be partly explained by its |
| 502 |
< |
geometric nature. |
| 491 |
> |
A variety of numerical integrators have been proposed to simulate |
| 492 |
> |
the motions of atoms in MD simulation. They usually begin with |
| 493 |
> |
initial conditionals and move the objects in the direction governed |
| 494 |
> |
by the differential equations. However, most of them ignore the |
| 495 |
> |
hidden physical laws contained within the equations. Since 1990, |
| 496 |
> |
geometric integrators, which preserve various phase-flow invariants |
| 497 |
> |
such as symplectic structure, volume and time reversal symmetry, are |
| 498 |
> |
developed to address this issue\cite{Dullweber1997, McLachlan1998, |
| 499 |
> |
Leimkuhler1999}. The velocity Verlet method, which happens to be a |
| 500 |
> |
simple example of symplectic integrator, continues to gain |
| 501 |
> |
popularity in the molecular dynamics community. This fact can be |
| 502 |
> |
partly explained by its geometric nature. |
| 503 |
|
|
| 504 |
< |
\subsection{\label{introSection:symplecticManifold}Symplectic Manifold} |
| 505 |
< |
A \emph{manifold} is an abstract mathematical space. It locally |
| 506 |
< |
looks like Euclidean space, but when viewed globally, it may have |
| 507 |
< |
more complicate structure. A good example of manifold is the surface |
| 508 |
< |
of Earth. It seems to be flat locally, but it is round if viewed as |
| 509 |
< |
a whole. A \emph{differentiable manifold} (also known as |
| 510 |
< |
\emph{smooth manifold}) is a manifold with an open cover in which |
| 511 |
< |
the covering neighborhoods are all smoothly isomorphic to one |
| 512 |
< |
another. In other words,it is possible to apply calculus on |
| 516 |
< |
\emph{differentiable manifold}. A \emph{symplectic manifold} is |
| 517 |
< |
defined as a pair $(M, \omega)$ which consisting of a |
| 504 |
> |
\subsection{\label{introSection:symplecticManifold}Symplectic Manifolds} |
| 505 |
> |
A \emph{manifold} is an abstract mathematical space. It looks |
| 506 |
> |
locally like Euclidean space, but when viewed globally, it may have |
| 507 |
> |
more complicated structure. A good example of manifold is the |
| 508 |
> |
surface of Earth. It seems to be flat locally, but it is round if |
| 509 |
> |
viewed as a whole. A \emph{differentiable manifold} (also known as |
| 510 |
> |
\emph{smooth manifold}) is a manifold on which it is possible to |
| 511 |
> |
apply calculus on \emph{differentiable manifold}. A \emph{symplectic |
| 512 |
> |
manifold} is defined as a pair $(M, \omega)$ which consists of a |
| 513 |
|
\emph{differentiable manifold} $M$ and a close, non-degenerated, |
| 514 |
|
bilinear symplectic form, $\omega$. A symplectic form on a vector |
| 515 |
|
space $V$ is a function $\omega(x, y)$ which satisfies |
| 516 |
|
$\omega(\lambda_1x_1+\lambda_2x_2, y) = \lambda_1\omega(x_1, y)+ |
| 517 |
|
\lambda_2\omega(x_2, y)$, $\omega(x, y) = - \omega(y, x)$ and |
| 518 |
< |
$\omega(x, x) = 0$. Cross product operation in vector field is an |
| 519 |
< |
example of symplectic form. |
| 518 |
> |
$\omega(x, x) = 0$. The cross product operation in vector field is |
| 519 |
> |
an example of symplectic form. |
| 520 |
|
|
| 521 |
< |
One of the motivations to study \emph{symplectic manifold} in |
| 521 |
> |
One of the motivations to study \emph{symplectic manifolds} in |
| 522 |
|
Hamiltonian Mechanics is that a symplectic manifold can represent |
| 523 |
|
all possible configurations of the system and the phase space of the |
| 524 |
|
system can be described by it's cotangent bundle. Every symplectic |
| 525 |
|
manifold is even dimensional. For instance, in Hamilton equations, |
| 526 |
|
coordinate and momentum always appear in pairs. |
| 527 |
|
|
| 533 |
– |
Let $(M,\omega)$ and $(N, \eta)$ be symplectic manifolds. A map |
| 534 |
– |
\[ |
| 535 |
– |
f : M \rightarrow N |
| 536 |
– |
\] |
| 537 |
– |
is a \emph{symplectomorphism} if it is a \emph{diffeomorphims} and |
| 538 |
– |
the \emph{pullback} of $\eta$ under f is equal to $\omega$. |
| 539 |
– |
Canonical transformation is an example of symplectomorphism in |
| 540 |
– |
classical mechanics. |
| 541 |
– |
|
| 528 |
|
\subsection{\label{introSection:ODE}Ordinary Differential Equations} |
| 529 |
|
|
| 530 |
< |
For a ordinary differential system defined as |
| 530 |
> |
For an ordinary differential system defined as |
| 531 |
|
\begin{equation} |
| 532 |
|
\dot x = f(x) |
| 533 |
|
\end{equation} |
| 534 |
< |
where $x = x(q,p)^T$, this system is canonical Hamiltonian, if |
| 534 |
> |
where $x = x(q,p)^T$, this system is a canonical Hamiltonian, if |
| 535 |
|
\begin{equation} |
| 536 |
|
f(r) = J\nabla _x H(r). |
| 537 |
|
\end{equation} |
| 591 |
|
\end{equation} |
| 592 |
|
|
| 593 |
|
In most cases, it is not easy to find the exact flow $\varphi_\tau$. |
| 594 |
< |
Instead, we use a approximate map, $\psi_\tau$, which is usually |
| 594 |
> |
Instead, we use an approximate map, $\psi_\tau$, which is usually |
| 595 |
|
called integrator. The order of an integrator $\psi_\tau$ is $p$, if |
| 596 |
|
the Taylor series of $\psi_\tau$ agree to order $p$, |
| 597 |
|
\begin{equation} |
| 598 |
< |
\psi_tau(x) = x + \tau f(x) + O(\tau^{p+1}) |
| 598 |
> |
\psi_\tau(x) = x + \tau f(x) + O(\tau^{p+1}) |
| 599 |
|
\end{equation} |
| 600 |
|
|
| 601 |
|
\subsection{\label{introSection:geometricProperties}Geometric Properties} |
| 602 |
|
|
| 603 |
< |
The hidden geometric properties\cite{Budd1999, Marsden1998} of ODE |
| 604 |
< |
and its flow play important roles in numerical studies. Many of them |
| 605 |
< |
can be found in systems which occur naturally in applications. |
| 603 |
> |
The hidden geometric properties\cite{Budd1999, Marsden1998} of an |
| 604 |
> |
ODE and its flow play important roles in numerical studies. Many of |
| 605 |
> |
them can be found in systems which occur naturally in applications. |
| 606 |
|
|
| 607 |
|
Let $\varphi$ be the flow of Hamiltonian vector field, $\varphi$ is |
| 608 |
|
a \emph{symplectic} flow if it satisfies, |
| 617 |
|
\begin{equation} |
| 618 |
|
{\varphi '}^T J \varphi ' = J \circ \varphi |
| 619 |
|
\end{equation} |
| 620 |
< |
is the property must be preserved by the integrator. |
| 620 |
> |
is the property that must be preserved by the integrator. |
| 621 |
|
|
| 622 |
|
It is possible to construct a \emph{volume-preserving} flow for a |
| 623 |
< |
source free($ \nabla \cdot f = 0 $) ODE, if the flow satisfies $ |
| 623 |
> |
source free ODE ($ \nabla \cdot f = 0 $), if the flow satisfies $ |
| 624 |
|
\det d\varphi = 1$. One can show easily that a symplectic flow will |
| 625 |
|
be volume-preserving. |
| 626 |
|
|
| 627 |
< |
Changing the variables $y = h(x)$ in a ODE\ref{introEquation:ODE} |
| 628 |
< |
will result in a new system, |
| 627 |
> |
Changing the variables $y = h(x)$ in an ODE |
| 628 |
> |
(Eq.~\ref{introEquation:ODE}) will result in a new system, |
| 629 |
|
\[ |
| 630 |
|
\dot y = \tilde f(y) = ((dh \cdot f)h^{ - 1} )(y). |
| 631 |
|
\] |
| 675 |
|
A lot of well established and very effective numerical methods have |
| 676 |
|
been successful precisely because of their symplecticities even |
| 677 |
|
though this fact was not recognized when they were first |
| 678 |
< |
constructed. The most famous example is leapfrog methods in |
| 679 |
< |
molecular dynamics. In general, symplectic integrators can be |
| 678 |
> |
constructed. The most famous example is the Verlet-leapfrog method |
| 679 |
> |
in molecular dynamics. In general, symplectic integrators can be |
| 680 |
|
constructed using one of four different methods. |
| 681 |
|
\begin{enumerate} |
| 682 |
|
\item Generating functions |
| 694 |
|
high-order explicit Runge-Kutta methods |
| 695 |
|
\cite{Owren1992,Chen2003}have been developed to overcome this |
| 696 |
|
instability. However, due to computational penalty involved in |
| 697 |
< |
implementing the Runge-Kutta methods, they do not attract too much |
| 698 |
< |
attention from Molecular Dynamics community. Instead, splitting have |
| 699 |
< |
been widely accepted since they exploit natural decompositions of |
| 700 |
< |
the system\cite{Tuckerman1992, McLachlan1998}. |
| 697 |
> |
implementing the Runge-Kutta methods, they have not attracted much |
| 698 |
> |
attention from the Molecular Dynamics community. Instead, splitting |
| 699 |
> |
methods have been widely accepted since they exploit natural |
| 700 |
> |
decompositions of the system\cite{Tuckerman1992, McLachlan1998}. |
| 701 |
|
|
| 702 |
< |
\subsubsection{\label{introSection:splittingMethod}Splitting Method} |
| 702 |
> |
\subsubsection{\label{introSection:splittingMethod}\textbf{Splitting Methods}} |
| 703 |
|
|
| 704 |
|
The main idea behind splitting methods is to decompose the discrete |
| 705 |
|
$\varphi_h$ as a composition of simpler flows, |
| 720 |
|
energy respectively, which is a natural decomposition of the |
| 721 |
|
problem. If $H_1$ and $H_2$ can be integrated using exact flows |
| 722 |
|
$\varphi_1(t)$ and $\varphi_2(t)$, respectively, a simple first |
| 723 |
< |
order is then given by the Lie-Trotter formula |
| 723 |
> |
order expression is then given by the Lie-Trotter formula |
| 724 |
|
\begin{equation} |
| 725 |
|
\varphi _h = \varphi _{1,h} \circ \varphi _{2,h}, |
| 726 |
|
\label{introEquation:firstOrderSplitting} |
| 746 |
|
\varphi _h = \varphi _{1,h/2} \circ \varphi _{2,h} \circ \varphi |
| 747 |
|
_{1,h/2} , \label{introEquation:secondOrderSplitting} |
| 748 |
|
\end{equation} |
| 749 |
< |
which has a local error proportional to $h^3$. Sprang splitting's |
| 750 |
< |
popularity in molecular simulation community attribute to its |
| 751 |
< |
symmetric property, |
| 749 |
> |
which has a local error proportional to $h^3$. The Sprang |
| 750 |
> |
splitting's popularity in molecular simulation community attribute |
| 751 |
> |
to its symmetric property, |
| 752 |
|
\begin{equation} |
| 753 |
|
\varphi _h^{ - 1} = \varphi _{ - h}. |
| 754 |
|
\label{introEquation:timeReversible} |
| 755 |
|
\end{equation} |
| 756 |
|
|
| 757 |
< |
\subsubsection{\label{introSection:exampleSplittingMethod}Example of Splitting Method} |
| 757 |
> |
\subsubsection{\label{introSection:exampleSplittingMethod}\textbf{Examples of the Splitting Method}} |
| 758 |
|
The classical equation for a system consisting of interacting |
| 759 |
|
particles can be written in Hamiltonian form, |
| 760 |
|
\[ |
| 761 |
|
H = T + V |
| 762 |
|
\] |
| 763 |
|
where $T$ is the kinetic energy and $V$ is the potential energy. |
| 764 |
< |
Setting $H_1 = T, H_2 = V$ and applying Strang splitting, one |
| 764 |
> |
Setting $H_1 = T, H_2 = V$ and applying the Strang splitting, one |
| 765 |
|
obtains the following: |
| 766 |
|
\begin{align} |
| 767 |
|
q(\Delta t) &= q(0) + \dot{q}(0)\Delta t + |
| 788 |
|
\label{introEquation:Lp9b}\\% |
| 789 |
|
% |
| 790 |
|
\dot{q}(\Delta t) &= \dot{q}\biggl (\frac{\Delta t}{2}\biggr ) + |
| 791 |
< |
\frac{\Delta t}{2m}\, F[q(0)]. \label{introEquation:Lp9c} |
| 791 |
> |
\frac{\Delta t}{2m}\, F[q(t)]. \label{introEquation:Lp9c} |
| 792 |
|
\end{align} |
| 793 |
|
From the preceding splitting, one can see that the integration of |
| 794 |
|
the equations of motion would follow: |
| 797 |
|
|
| 798 |
|
\item Use the half step velocities to move positions one whole step, $\Delta t$. |
| 799 |
|
|
| 800 |
< |
\item Evaluate the forces at the new positions, $\mathbf{r}(\Delta t)$, and use the new forces to complete the velocity move. |
| 800 |
> |
\item Evaluate the forces at the new positions, $\mathbf{q}(\Delta t)$, and use the new forces to complete the velocity move. |
| 801 |
|
|
| 802 |
|
\item Repeat from step 1 with the new position, velocities, and forces assuming the roles of the initial values. |
| 803 |
|
\end{enumerate} |
| 804 |
|
|
| 805 |
< |
Simply switching the order of splitting and composing, a new |
| 806 |
< |
integrator, the \emph{position verlet} integrator, can be generated, |
| 805 |
> |
By simply switching the order of the propagators in the splitting |
| 806 |
> |
and composing a new integrator, the \emph{position verlet} |
| 807 |
> |
integrator, can be generated, |
| 808 |
|
\begin{align} |
| 809 |
|
\dot q(\Delta t) &= \dot q(0) + \Delta tF(q(0))\left[ {q(0) + |
| 810 |
|
\frac{{\Delta t}}{{2m}}\dot q(0)} \right], % |
| 815 |
|
\label{introEquation:positionVerlet2} |
| 816 |
|
\end{align} |
| 817 |
|
|
| 818 |
< |
\subsubsection{\label{introSection:errorAnalysis}Error Analysis and Higher Order Methods} |
| 818 |
> |
\subsubsection{\label{introSection:errorAnalysis}\textbf{Error Analysis and Higher Order Methods}} |
| 819 |
|
|
| 820 |
< |
Baker-Campbell-Hausdorff formula can be used to determine the local |
| 821 |
< |
error of splitting method in terms of commutator of the |
| 820 |
> |
The Baker-Campbell-Hausdorff formula can be used to determine the |
| 821 |
> |
local error of splitting method in terms of the commutator of the |
| 822 |
|
operators(\ref{introEquation:exponentialOperator}) associated with |
| 823 |
< |
the sub-flow. For operators $hX$ and $hY$ which are associate to |
| 823 |
> |
the sub-flow. For operators $hX$ and $hY$ which are associated with |
| 824 |
|
$\varphi_1(t)$ and $\varphi_2(t)$ respectively , we have |
| 825 |
|
\begin{equation} |
| 826 |
|
\exp (hX + hY) = \exp (hZ) |
| 834 |
|
\[ |
| 835 |
|
[X,Y] = XY - YX . |
| 836 |
|
\] |
| 837 |
< |
Applying Baker-Campbell-Hausdorff formula\cite{Varadarajan1974} to |
| 838 |
< |
Sprang splitting, we can obtain |
| 837 |
> |
Applying the Baker-Campbell-Hausdorff formula\cite{Varadarajan1974} |
| 838 |
> |
to the Sprang splitting, we can obtain |
| 839 |
|
\begin{eqnarray*} |
| 840 |
|
\exp (h X/2)\exp (h Y)\exp (h X/2) & = & \exp (h X + h Y + h^2 [X,Y]/4 + h^2 [Y,X]/4 \\ |
| 841 |
|
& & \mbox{} + h^2 [X,X]/8 + h^2 [Y,Y]/8 \\ |
| 842 |
|
& & \mbox{} + h^3 [Y,[Y,X]]/12 - h^3[X,[X,Y]]/24 + \ldots ) |
| 843 |
|
\end{eqnarray*} |
| 844 |
< |
Since \[ [X,Y] + [Y,X] = 0\] and \[ [X,X] = 0\], the dominant local |
| 844 |
> |
Since \[ [X,Y] + [Y,X] = 0\] and \[ [X,X] = 0,\] the dominant local |
| 845 |
|
error of Spring splitting is proportional to $h^3$. The same |
| 846 |
< |
procedure can be applied to general splitting, of the form |
| 846 |
> |
procedure can be applied to a general splitting, of the form |
| 847 |
|
\begin{equation} |
| 848 |
|
\varphi _{b_m h}^2 \circ \varphi _{a_m h}^1 \circ \varphi _{b_{m - |
| 849 |
|
1} h}^2 \circ \ldots \circ \varphi _{a_1 h}^1 . |
| 850 |
|
\end{equation} |
| 851 |
< |
Careful choice of coefficient $a_1 \ldot b_m$ will lead to higher |
| 852 |
< |
order method. Yoshida proposed an elegant way to compose higher |
| 851 |
> |
A careful choice of coefficient $a_1 \ldots b_m$ will lead to higher |
| 852 |
> |
order methods. Yoshida proposed an elegant way to compose higher |
| 853 |
|
order methods based on symmetric splitting\cite{Yoshida1990}. Given |
| 854 |
|
a symmetric second order base method $ \varphi _h^{(2)} $, a |
| 855 |
|
fourth-order symmetric method can be constructed by composing, |
| 862 |
|
integrator $ \varphi _h^{(2n + 2)}$ can be composed by |
| 863 |
|
\begin{equation} |
| 864 |
|
\varphi _h^{(2n + 2)} = \varphi _{\alpha h}^{(2n)} \circ \varphi |
| 865 |
< |
_{\beta h}^{(2n)} \circ \varphi _{\alpha h}^{(2n)} |
| 865 |
> |
_{\beta h}^{(2n)} \circ \varphi _{\alpha h}^{(2n)}, |
| 866 |
|
\end{equation} |
| 867 |
< |
, if the weights are chosen as |
| 867 |
> |
if the weights are chosen as |
| 868 |
|
\[ |
| 869 |
|
\alpha = - \frac{{2^{1/(2n + 1)} }}{{2 - 2^{1/(2n + 1)} }},\beta = |
| 870 |
|
\frac{{2^{1/(2n + 1)} }}{{2 - 2^{1/(2n + 1)} }} . |
| 901 |
|
\end{enumerate} |
| 902 |
|
These three individual steps will be covered in the following |
| 903 |
|
sections. Sec.~\ref{introSec:initialSystemSettings} deals with the |
| 904 |
< |
initialization of a simulation. Sec.~\ref{introSec:production} will |
| 905 |
< |
discusses issues in production run. Sec.~\ref{introSection:Analysis} |
| 906 |
< |
provides the theoretical tools for trajectory analysis. |
| 904 |
> |
initialization of a simulation. Sec.~\ref{introSection:production} |
| 905 |
> |
will discusse issues in production run. |
| 906 |
> |
Sec.~\ref{introSection:Analysis} provides the theoretical tools for |
| 907 |
> |
trajectory analysis. |
| 908 |
|
|
| 909 |
|
\subsection{\label{introSec:initialSystemSettings}Initialization} |
| 910 |
|
|
| 911 |
< |
\subsubsection{Preliminary preparation} |
| 911 |
> |
\subsubsection{\textbf{Preliminary preparation}} |
| 912 |
|
|
| 913 |
|
When selecting the starting structure of a molecule for molecular |
| 914 |
|
simulation, one may retrieve its Cartesian coordinates from public |
| 915 |
|
databases, such as RCSB Protein Data Bank \textit{etc}. Although |
| 916 |
|
thousands of crystal structures of molecules are discovered every |
| 917 |
|
year, many more remain unknown due to the difficulties of |
| 918 |
< |
purification and crystallization. Even for the molecule with known |
| 919 |
< |
structure, some important information is missing. For example, the |
| 918 |
> |
purification and crystallization. Even for molecules with known |
| 919 |
> |
structure, some important information is missing. For example, a |
| 920 |
|
missing hydrogen atom which acts as donor in hydrogen bonding must |
| 921 |
|
be added. Moreover, in order to include electrostatic interaction, |
| 922 |
|
one may need to specify the partial charges for individual atoms. |
| 923 |
|
Under some circumstances, we may even need to prepare the system in |
| 924 |
< |
a special setup. For instance, when studying transport phenomenon in |
| 925 |
< |
membrane system, we may prepare the lipids in bilayer structure |
| 926 |
< |
instead of placing lipids randomly in solvent, since we are not |
| 927 |
< |
interested in self-aggregation and it takes a long time to happen. |
| 924 |
> |
a special configuration. For instance, when studying transport |
| 925 |
> |
phenomenon in membrane systems, we may prepare the lipids in a |
| 926 |
> |
bilayer structure instead of placing lipids randomly in solvent, |
| 927 |
> |
since we are not interested in the slow self-aggregation process. |
| 928 |
|
|
| 929 |
< |
\subsubsection{Minimization} |
| 929 |
> |
\subsubsection{\textbf{Minimization}} |
| 930 |
|
|
| 931 |
|
It is quite possible that some of molecules in the system from |
| 932 |
< |
preliminary preparation may be overlapped with each other. This |
| 933 |
< |
close proximity leads to high potential energy which consequently |
| 934 |
< |
jeopardizes any molecular dynamics simulations. To remove these |
| 935 |
< |
steric overlaps, one typically performs energy minimization to find |
| 936 |
< |
a more reasonable conformation. Several energy minimization methods |
| 937 |
< |
have been developed to exploit the energy surface and to locate the |
| 938 |
< |
local minimum. While converging slowly near the minimum, steepest |
| 939 |
< |
descent method is extremely robust when systems are far from |
| 940 |
< |
harmonic. Thus, it is often used to refine structure from |
| 941 |
< |
crystallographic data. Relied on the gradient or hessian, advanced |
| 942 |
< |
methods like conjugate gradient and Newton-Raphson converge rapidly |
| 943 |
< |
to a local minimum, while become unstable if the energy surface is |
| 944 |
< |
far from quadratic. Another factor must be taken into account, when |
| 932 |
> |
preliminary preparation may be overlapping with each other. This |
| 933 |
> |
close proximity leads to high initial potential energy which |
| 934 |
> |
consequently jeopardizes any molecular dynamics simulations. To |
| 935 |
> |
remove these steric overlaps, one typically performs energy |
| 936 |
> |
minimization to find a more reasonable conformation. Several energy |
| 937 |
> |
minimization methods have been developed to exploit the energy |
| 938 |
> |
surface and to locate the local minimum. While converging slowly |
| 939 |
> |
near the minimum, steepest descent method is extremely robust when |
| 940 |
> |
systems are strongly anharmonic. Thus, it is often used to refine |
| 941 |
> |
structure from crystallographic data. Relied on the gradient or |
| 942 |
> |
hessian, advanced methods like Newton-Raphson converge rapidly to a |
| 943 |
> |
local minimum, but become unstable if the energy surface is far from |
| 944 |
> |
quadratic. Another factor that must be taken into account, when |
| 945 |
|
choosing energy minimization method, is the size of the system. |
| 946 |
|
Steepest descent and conjugate gradient can deal with models of any |
| 947 |
< |
size. Because of the limit of computation power to calculate hessian |
| 948 |
< |
matrix and insufficient storage capacity to store them, most |
| 949 |
< |
Newton-Raphson methods can not be used with very large models. |
| 947 |
> |
size. Because of the limits on computer memory to store the hessian |
| 948 |
> |
matrix and the computing power needed to diagonalized these |
| 949 |
> |
matrices, most Newton-Raphson methods can not be used with very |
| 950 |
> |
large systems. |
| 951 |
|
|
| 952 |
< |
\subsubsection{Heating} |
| 952 |
> |
\subsubsection{\textbf{Heating}} |
| 953 |
|
|
| 954 |
|
Typically, Heating is performed by assigning random velocities |
| 955 |
< |
according to a Gaussian distribution for a temperature. Beginning at |
| 956 |
< |
a lower temperature and gradually increasing the temperature by |
| 957 |
< |
assigning greater random velocities, we end up with setting the |
| 958 |
< |
temperature of the system to a final temperature at which the |
| 959 |
< |
simulation will be conducted. In heating phase, we should also keep |
| 960 |
< |
the system from drifting or rotating as a whole. Equivalently, the |
| 961 |
< |
net linear momentum and angular momentum of the system should be |
| 962 |
< |
shifted to zero. |
| 955 |
> |
according to a Maxwell-Boltzman distribution for a desired |
| 956 |
> |
temperature. Beginning at a lower temperature and gradually |
| 957 |
> |
increasing the temperature by assigning larger random velocities, we |
| 958 |
> |
end up with setting the temperature of the system to a final |
| 959 |
> |
temperature at which the simulation will be conducted. In heating |
| 960 |
> |
phase, we should also keep the system from drifting or rotating as a |
| 961 |
> |
whole. To do this, the net linear momentum and angular momentum of |
| 962 |
> |
the system is shifted to zero after each resampling from the Maxwell |
| 963 |
> |
-Boltzman distribution. |
| 964 |
|
|
| 965 |
< |
\subsubsection{Equilibration} |
| 965 |
> |
\subsubsection{\textbf{Equilibration}} |
| 966 |
|
|
| 967 |
|
The purpose of equilibration is to allow the system to evolve |
| 968 |
|
spontaneously for a period of time and reach equilibrium. The |
| 976 |
|
|
| 977 |
|
\subsection{\label{introSection:production}Production} |
| 978 |
|
|
| 979 |
< |
Production run is the most important step of the simulation, in |
| 979 |
> |
The production run is the most important step of the simulation, in |
| 980 |
|
which the equilibrated structure is used as a starting point and the |
| 981 |
|
motions of the molecules are collected for later analysis. In order |
| 982 |
|
to capture the macroscopic properties of the system, the molecular |
| 983 |
< |
dynamics simulation must be performed in correct and efficient way. |
| 983 |
> |
dynamics simulation must be performed by sampling correctly and |
| 984 |
> |
efficiently from the relevant thermodynamic ensemble. |
| 985 |
|
|
| 986 |
|
The most expensive part of a molecular dynamics simulation is the |
| 987 |
|
calculation of non-bonded forces, such as van der Waals force and |
| 988 |
|
Coulombic forces \textit{etc}. For a system of $N$ particles, the |
| 989 |
|
complexity of the algorithm for pair-wise interactions is $O(N^2 )$, |
| 990 |
|
which making large simulations prohibitive in the absence of any |
| 991 |
< |
computation saving techniques. |
| 991 |
> |
algorithmic tricks. |
| 992 |
|
|
| 993 |
< |
A natural approach to avoid system size issue is to represent the |
| 993 |
> |
A natural approach to avoid system size issues is to represent the |
| 994 |
|
bulk behavior by a finite number of the particles. However, this |
| 995 |
< |
approach will suffer from the surface effect. To offset this, |
| 996 |
< |
\textit{Periodic boundary condition} (see Fig.~\ref{introFig:pbc}) |
| 997 |
< |
is developed to simulate bulk properties with a relatively small |
| 998 |
< |
number of particles. In this method, the simulation box is |
| 999 |
< |
replicated throughout space to form an infinite lattice. During the |
| 1000 |
< |
simulation, when a particle moves in the primary cell, its image in |
| 1001 |
< |
other cells move in exactly the same direction with exactly the same |
| 1002 |
< |
orientation. Thus, as a particle leaves the primary cell, one of its |
| 1003 |
< |
images will enter through the opposite face. |
| 995 |
> |
approach will suffer from the surface effect at the edges of the |
| 996 |
> |
simulation. To offset this, \textit{Periodic boundary conditions} |
| 997 |
> |
(see Fig.~\ref{introFig:pbc}) is developed to simulate bulk |
| 998 |
> |
properties with a relatively small number of particles. In this |
| 999 |
> |
method, the simulation box is replicated throughout space to form an |
| 1000 |
> |
infinite lattice. During the simulation, when a particle moves in |
| 1001 |
> |
the primary cell, its image in other cells move in exactly the same |
| 1002 |
> |
direction with exactly the same orientation. Thus, as a particle |
| 1003 |
> |
leaves the primary cell, one of its images will enter through the |
| 1004 |
> |
opposite face. |
| 1005 |
|
\begin{figure} |
| 1006 |
|
\centering |
| 1007 |
|
\includegraphics[width=\linewidth]{pbc.eps} |
| 1013 |
|
|
| 1014 |
|
%cutoff and minimum image convention |
| 1015 |
|
Another important technique to improve the efficiency of force |
| 1016 |
< |
evaluation is to apply cutoff where particles farther than a |
| 1017 |
< |
predetermined distance, are not included in the calculation |
| 1016 |
> |
evaluation is to apply spherical cutoff where particles farther than |
| 1017 |
> |
a predetermined distance are not included in the calculation |
| 1018 |
|
\cite{Frenkel1996}. The use of a cutoff radius will cause a |
| 1019 |
|
discontinuity in the potential energy curve. Fortunately, one can |
| 1020 |
< |
shift the potential to ensure the potential curve go smoothly to |
| 1021 |
< |
zero at the cutoff radius. Cutoff strategy works pretty well for |
| 1022 |
< |
Lennard-Jones interaction because of its short range nature. |
| 1023 |
< |
However, simply truncating the electrostatic interaction with the |
| 1024 |
< |
use of cutoff has been shown to lead to severe artifacts in |
| 1025 |
< |
simulations. Ewald summation, in which the slowly conditionally |
| 1026 |
< |
convergent Coulomb potential is transformed into direct and |
| 1027 |
< |
reciprocal sums with rapid and absolute convergence, has proved to |
| 1028 |
< |
minimize the periodicity artifacts in liquid simulations. Taking the |
| 1029 |
< |
advantages of the fast Fourier transform (FFT) for calculating |
| 1030 |
< |
discrete Fourier transforms, the particle mesh-based |
| 1020 |
> |
shift simple radial potential to ensure the potential curve go |
| 1021 |
> |
smoothly to zero at the cutoff radius. The cutoff strategy works |
| 1022 |
> |
well for Lennard-Jones interaction because of its short range |
| 1023 |
> |
nature. However, simply truncating the electrostatic interaction |
| 1024 |
> |
with the use of cutoffs has been shown to lead to severe artifacts |
| 1025 |
> |
in simulations. The Ewald summation, in which the slowly decaying |
| 1026 |
> |
Coulomb potential is transformed into direct and reciprocal sums |
| 1027 |
> |
with rapid and absolute convergence, has proved to minimize the |
| 1028 |
> |
periodicity artifacts in liquid simulations. Taking the advantages |
| 1029 |
> |
of the fast Fourier transform (FFT) for calculating discrete Fourier |
| 1030 |
> |
transforms, the particle mesh-based |
| 1031 |
|
methods\cite{Hockney1981,Shimada1993, Luty1994} are accelerated from |
| 1032 |
< |
$O(N^{3/2})$ to $O(N logN)$. An alternative approach is \emph{fast |
| 1033 |
< |
multipole method}\cite{Greengard1987, Greengard1994}, which treats |
| 1034 |
< |
Coulombic interaction exactly at short range, and approximate the |
| 1035 |
< |
potential at long range through multipolar expansion. In spite of |
| 1036 |
< |
their wide acceptances at the molecular simulation community, these |
| 1037 |
< |
two methods are hard to be implemented correctly and efficiently. |
| 1038 |
< |
Instead, we use a damped and charge-neutralized Coulomb potential |
| 1039 |
< |
method developed by Wolf and his coworkers\cite{Wolf1999}. The |
| 1040 |
< |
shifted Coulomb potential for particle $i$ and particle $j$ at |
| 1041 |
< |
distance $r_{rj}$ is given by: |
| 1032 |
> |
$O(N^{3/2})$ to $O(N logN)$. An alternative approach is the |
| 1033 |
> |
\emph{fast multipole method}\cite{Greengard1987, Greengard1994}, |
| 1034 |
> |
which treats Coulombic interactions exactly at short range, and |
| 1035 |
> |
approximate the potential at long range through multipolar |
| 1036 |
> |
expansion. In spite of their wide acceptance at the molecular |
| 1037 |
> |
simulation community, these two methods are difficult to implement |
| 1038 |
> |
correctly and efficiently. Instead, we use a damped and |
| 1039 |
> |
charge-neutralized Coulomb potential method developed by Wolf and |
| 1040 |
> |
his coworkers\cite{Wolf1999}. The shifted Coulomb potential for |
| 1041 |
> |
particle $i$ and particle $j$ at distance $r_{rj}$ is given by: |
| 1042 |
|
\begin{equation} |
| 1043 |
|
V(r_{ij})= \frac{q_i q_j \textrm{erfc}(\alpha |
| 1044 |
|
r_{ij})}{r_{ij}}-\lim_{r_{ij}\rightarrow |
| 1060 |
|
|
| 1061 |
|
\subsection{\label{introSection:Analysis} Analysis} |
| 1062 |
|
|
| 1063 |
< |
Recently, advanced visualization technique are widely applied to |
| 1063 |
> |
Recently, advanced visualization technique have become applied to |
| 1064 |
|
monitor the motions of molecules. Although the dynamics of the |
| 1065 |
|
system can be described qualitatively from animation, quantitative |
| 1066 |
< |
trajectory analysis are more appreciable. According to the |
| 1067 |
< |
principles of Statistical Mechanics, |
| 1068 |
< |
Sec.~\ref{introSection:statisticalMechanics}, one can compute |
| 1069 |
< |
thermodynamics properties, analyze fluctuations of structural |
| 1070 |
< |
parameters, and investigate time-dependent processes of the molecule |
| 1079 |
< |
from the trajectories. |
| 1066 |
> |
trajectory analysis are more useful. According to the principles of |
| 1067 |
> |
Statistical Mechanics, Sec.~\ref{introSection:statisticalMechanics}, |
| 1068 |
> |
one can compute thermodynamic properties, analyze fluctuations of |
| 1069 |
> |
structural parameters, and investigate time-dependent processes of |
| 1070 |
> |
the molecule from the trajectories. |
| 1071 |
|
|
| 1072 |
< |
\subsubsection{\label{introSection:thermodynamicsProperties}Thermodynamics Properties} |
| 1072 |
> |
\subsubsection{\label{introSection:thermodynamicsProperties}\textbf{Thermodynamic Properties}} |
| 1073 |
|
|
| 1074 |
< |
Thermodynamics properties, which can be expressed in terms of some |
| 1074 |
> |
Thermodynamic properties, which can be expressed in terms of some |
| 1075 |
|
function of the coordinates and momenta of all particles in the |
| 1076 |
|
system, can be directly computed from molecular dynamics. The usual |
| 1077 |
|
way to measure the pressure is based on virial theorem of Clausius |
| 1091 |
|
< j} {r{}_{ij} \cdot f_{ij} } } \right\rangle |
| 1092 |
|
\end{equation} |
| 1093 |
|
|
| 1094 |
< |
\subsubsection{\label{introSection:structuralProperties}Structural Properties} |
| 1094 |
> |
\subsubsection{\label{introSection:structuralProperties}\textbf{Structural Properties}} |
| 1095 |
|
|
| 1096 |
|
Structural Properties of a simple fluid can be described by a set of |
| 1097 |
< |
distribution functions. Among these functions,\emph{pair |
| 1097 |
> |
distribution functions. Among these functions,the \emph{pair |
| 1098 |
|
distribution function}, also known as \emph{radial distribution |
| 1099 |
< |
function}, is of most fundamental importance to liquid-state theory. |
| 1100 |
< |
Pair distribution function can be gathered by Fourier transforming |
| 1101 |
< |
raw data from a series of neutron diffraction experiments and |
| 1102 |
< |
integrating over the surface factor \cite{Powles1973}. The |
| 1103 |
< |
experiment result can serve as a criterion to justify the |
| 1104 |
< |
correctness of the theory. Moreover, various equilibrium |
| 1105 |
< |
thermodynamic and structural properties can also be expressed in |
| 1106 |
< |
terms of radial distribution function \cite{Allen1987}. |
| 1099 |
> |
function}, is of most fundamental importance to liquid theory. |
| 1100 |
> |
Experimentally, pair distribution function can be gathered by |
| 1101 |
> |
Fourier transforming raw data from a series of neutron diffraction |
| 1102 |
> |
experiments and integrating over the surface factor |
| 1103 |
> |
\cite{Powles1973}. The experimental results can serve as a criterion |
| 1104 |
> |
to justify the correctness of a liquid model. Moreover, various |
| 1105 |
> |
equilibrium thermodynamic and structural properties can also be |
| 1106 |
> |
expressed in terms of radial distribution function \cite{Allen1987}. |
| 1107 |
|
|
| 1108 |
< |
A pair distribution functions $g(r)$ gives the probability that a |
| 1108 |
> |
The pair distribution functions $g(r)$ gives the probability that a |
| 1109 |
|
particle $i$ will be located at a distance $r$ from a another |
| 1110 |
|
particle $j$ in the system |
| 1111 |
|
\[ |
| 1112 |
|
g(r) = \frac{V}{{N^2 }}\left\langle {\sum\limits_i {\sum\limits_{j |
| 1113 |
< |
\ne i} {\delta (r - r_{ij} )} } } \right\rangle. |
| 1113 |
> |
\ne i} {\delta (r - r_{ij} )} } } \right\rangle = \frac{\rho |
| 1114 |
> |
(r)}{\rho}. |
| 1115 |
|
\] |
| 1116 |
|
Note that the delta function can be replaced by a histogram in |
| 1117 |
< |
computer simulation. Figure |
| 1118 |
< |
\ref{introFigure:pairDistributionFunction} shows a typical pair |
| 1119 |
< |
distribution function for the liquid argon system. The occurrence of |
| 1128 |
< |
several peaks in the plot of $g(r)$ suggests that it is more likely |
| 1129 |
< |
to find particles at certain radial values than at others. This is a |
| 1130 |
< |
result of the attractive interaction at such distances. Because of |
| 1131 |
< |
the strong repulsive forces at short distance, the probability of |
| 1132 |
< |
locating particles at distances less than about 2.5{\AA} from each |
| 1133 |
< |
other is essentially zero. |
| 1117 |
> |
computer simulation. Peaks in $g(r)$ represent solvent shells, and |
| 1118 |
> |
the height of these peaks gradually decreases to 1 as the liquid of |
| 1119 |
> |
large distance approaches the bulk density. |
| 1120 |
|
|
| 1135 |
– |
%\begin{figure} |
| 1136 |
– |
%\centering |
| 1137 |
– |
%\includegraphics[width=\linewidth]{pdf.eps} |
| 1138 |
– |
%\caption[Pair distribution function for the liquid argon |
| 1139 |
– |
%]{Pair distribution function for the liquid argon} |
| 1140 |
– |
%\label{introFigure:pairDistributionFunction} |
| 1141 |
– |
%\end{figure} |
| 1121 |
|
|
| 1122 |
< |
\subsubsection{\label{introSection:timeDependentProperties}Time-dependent |
| 1123 |
< |
Properties} |
| 1122 |
> |
\subsubsection{\label{introSection:timeDependentProperties}\textbf{Time-dependent |
| 1123 |
> |
Properties}} |
| 1124 |
|
|
| 1125 |
|
Time-dependent properties are usually calculated using \emph{time |
| 1126 |
< |
correlation function}, which correlates random variables $A$ and $B$ |
| 1127 |
< |
at two different time |
| 1126 |
> |
correlation functions}, which correlate random variables $A$ and $B$ |
| 1127 |
> |
at two different times, |
| 1128 |
|
\begin{equation} |
| 1129 |
|
C_{AB} (t) = \left\langle {A(t)B(0)} \right\rangle. |
| 1130 |
|
\label{introEquation:timeCorrelationFunction} |
| 1131 |
|
\end{equation} |
| 1132 |
|
If $A$ and $B$ refer to same variable, this kind of correlation |
| 1133 |
< |
function is called \emph{auto correlation function}. One example of |
| 1134 |
< |
auto correlation function is velocity auto-correlation function |
| 1135 |
< |
which is directly related to transport properties of molecular |
| 1136 |
< |
liquids: |
| 1133 |
> |
function is called an \emph{autocorrelation function}. One example |
| 1134 |
> |
of an auto correlation function is the velocity auto-correlation |
| 1135 |
> |
function which is directly related to transport properties of |
| 1136 |
> |
molecular liquids: |
| 1137 |
|
\[ |
| 1138 |
|
D = \frac{1}{3}\int\limits_0^\infty {\left\langle {v(t) \cdot v(0)} |
| 1139 |
|
\right\rangle } dt |
| 1140 |
|
\] |
| 1141 |
< |
where $D$ is diffusion constant. Unlike velocity autocorrelation |
| 1142 |
< |
function which is averaging over time origins and over all the |
| 1143 |
< |
atoms, dipole autocorrelation are calculated for the entire system. |
| 1144 |
< |
The dipole autocorrelation function is given by: |
| 1141 |
> |
where $D$ is diffusion constant. Unlike the velocity autocorrelation |
| 1142 |
> |
function, which is averaging over time origins and over all the |
| 1143 |
> |
atoms, the dipole autocorrelation functions are calculated for the |
| 1144 |
> |
entire system. The dipole autocorrelation function is given by: |
| 1145 |
|
\[ |
| 1146 |
|
c_{dipole} = \left\langle {u_{tot} (t) \cdot u_{tot} (t)} |
| 1147 |
|
\right\rangle |
| 1167 |
|
areas, from engineering, physics, to chemistry. For example, |
| 1168 |
|
missiles and vehicle are usually modeled by rigid bodies. The |
| 1169 |
|
movement of the objects in 3D gaming engine or other physics |
| 1170 |
< |
simulator is governed by the rigid body dynamics. In molecular |
| 1171 |
< |
simulation, rigid body is used to simplify the model in |
| 1172 |
< |
protein-protein docking study\cite{Gray2003}. |
| 1170 |
> |
simulator is governed by rigid body dynamics. In molecular |
| 1171 |
> |
simulations, rigid bodies are used to simplify protein-protein |
| 1172 |
> |
docking studies\cite{Gray2003}. |
| 1173 |
|
|
| 1174 |
|
It is very important to develop stable and efficient methods to |
| 1175 |
< |
integrate the equations of motion of orientational degrees of |
| 1176 |
< |
freedom. Euler angles are the nature choice to describe the |
| 1177 |
< |
rotational degrees of freedom. However, due to its singularity, the |
| 1178 |
< |
numerical integration of corresponding equations of motion is very |
| 1179 |
< |
inefficient and inaccurate. Although an alternative integrator using |
| 1180 |
< |
different sets of Euler angles can overcome this |
| 1181 |
< |
difficulty\cite{Barojas1973}, the computational penalty and the lost |
| 1182 |
< |
of angular momentum conservation still remain. A singularity free |
| 1183 |
< |
representation utilizing quaternions was developed by Evans in |
| 1184 |
< |
1977\cite{Evans1977}. Unfortunately, this approach suffer from the |
| 1185 |
< |
nonseparable Hamiltonian resulted from quaternion representation, |
| 1186 |
< |
which prevents the symplectic algorithm to be utilized. Another |
| 1187 |
< |
different approach is to apply holonomic constraints to the atoms |
| 1188 |
< |
belonging to the rigid body. Each atom moves independently under the |
| 1189 |
< |
normal forces deriving from potential energy and constraint forces |
| 1190 |
< |
which are used to guarantee the rigidness. However, due to their |
| 1191 |
< |
iterative nature, SHAKE and Rattle algorithm converge very slowly |
| 1192 |
< |
when the number of constraint increases\cite{Ryckaert1977, |
| 1193 |
< |
Andersen1983}. |
| 1175 |
> |
integrate the equations of motion for orientational degrees of |
| 1176 |
> |
freedom. Euler angles are the natural choice to describe the |
| 1177 |
> |
rotational degrees of freedom. However, due to $\frac {1}{sin |
| 1178 |
> |
\theta}$ singularities, the numerical integration of corresponding |
| 1179 |
> |
equations of motion is very inefficient and inaccurate. Although an |
| 1180 |
> |
alternative integrator using multiple sets of Euler angles can |
| 1181 |
> |
overcome this difficulty\cite{Barojas1973}, the computational |
| 1182 |
> |
penalty and the loss of angular momentum conservation still remain. |
| 1183 |
> |
A singularity-free representation utilizing quaternions was |
| 1184 |
> |
developed by Evans in 1977\cite{Evans1977}. Unfortunately, this |
| 1185 |
> |
approach uses a nonseparable Hamiltonian resulting from the |
| 1186 |
> |
quaternion representation, which prevents the symplectic algorithm |
| 1187 |
> |
to be utilized. Another different approach is to apply holonomic |
| 1188 |
> |
constraints to the atoms belonging to the rigid body. Each atom |
| 1189 |
> |
moves independently under the normal forces deriving from potential |
| 1190 |
> |
energy and constraint forces which are used to guarantee the |
| 1191 |
> |
rigidness. However, due to their iterative nature, the SHAKE and |
| 1192 |
> |
Rattle algorithms also converge very slowly when the number of |
| 1193 |
> |
constraints increases\cite{Ryckaert1977, Andersen1983}. |
| 1194 |
|
|
| 1195 |
< |
The break through in geometric literature suggests that, in order to |
| 1195 |
> |
A break-through in geometric literature suggests that, in order to |
| 1196 |
|
develop a long-term integration scheme, one should preserve the |
| 1197 |
< |
symplectic structure of the flow. Introducing conjugate momentum to |
| 1198 |
< |
rotation matrix $Q$ and re-formulating Hamiltonian's equation, a |
| 1199 |
< |
symplectic integrator, RSHAKE\cite{Kol1997}, was proposed to evolve |
| 1200 |
< |
the Hamiltonian system in a constraint manifold by iteratively |
| 1201 |
< |
satisfying the orthogonality constraint $Q_T Q = 1$. An alternative |
| 1202 |
< |
method using quaternion representation was developed by |
| 1203 |
< |
Omelyan\cite{Omelyan1998}. However, both of these methods are |
| 1204 |
< |
iterative and inefficient. In this section, we will present a |
| 1197 |
> |
symplectic structure of the flow. By introducing a conjugate |
| 1198 |
> |
momentum to the rotation matrix $Q$ and re-formulating Hamiltonian's |
| 1199 |
> |
equation, a symplectic integrator, RSHAKE\cite{Kol1997}, was |
| 1200 |
> |
proposed to evolve the Hamiltonian system in a constraint manifold |
| 1201 |
> |
by iteratively satisfying the orthogonality constraint $Q^T Q = 1$. |
| 1202 |
> |
An alternative method using the quaternion representation was |
| 1203 |
> |
developed by Omelyan\cite{Omelyan1998}. However, both of these |
| 1204 |
> |
methods are iterative and inefficient. In this section, we descibe a |
| 1205 |
|
symplectic Lie-Poisson integrator for rigid body developed by |
| 1206 |
|
Dullweber and his coworkers\cite{Dullweber1997} in depth. |
| 1207 |
|
|
| 1208 |
< |
\subsection{\label{introSection:constrainedHamiltonianRB}Constrained Hamiltonian for Rigid Body} |
| 1209 |
< |
The motion of the rigid body is Hamiltonian with the Hamiltonian |
| 1208 |
> |
\subsection{\label{introSection:constrainedHamiltonianRB}Constrained Hamiltonian for Rigid Bodies} |
| 1209 |
> |
The motion of a rigid body is Hamiltonian with the Hamiltonian |
| 1210 |
|
function |
| 1211 |
|
\begin{equation} |
| 1212 |
|
H = \frac{1}{2}(p^T m^{ - 1} p) + \frac{1}{2}tr(PJ^{ - 1} P) + |
| 1220 |
|
I_{ii}^{ - 1} = \frac{1}{2}\sum\limits_{i \ne j} {J_{jj}^{ - 1} } |
| 1221 |
|
\] |
| 1222 |
|
where $I_{ii}$ is the diagonal element of the inertia tensor. This |
| 1223 |
< |
constrained Hamiltonian equation subjects to a holonomic constraint, |
| 1223 |
> |
constrained Hamiltonian equation is subjected to a holonomic |
| 1224 |
> |
constraint, |
| 1225 |
|
\begin{equation} |
| 1226 |
|
Q^T Q = 1, \label{introEquation:orthogonalConstraint} |
| 1227 |
|
\end{equation} |
| 1228 |
< |
which is used to ensure rotation matrix's orthogonality. |
| 1229 |
< |
Differentiating \ref{introEquation:orthogonalConstraint} and using |
| 1230 |
< |
Equation \ref{introEquation:RBMotionMomentum}, one may obtain, |
| 1228 |
> |
which is used to ensure rotation matrix's unitarity. Differentiating |
| 1229 |
> |
\ref{introEquation:orthogonalConstraint} and using Equation |
| 1230 |
> |
\ref{introEquation:RBMotionMomentum}, one may obtain, |
| 1231 |
|
\begin{equation} |
| 1232 |
|
Q^T PJ^{ - 1} + J^{ - 1} P^T Q = 0 . \\ |
| 1233 |
|
\label{introEquation:RBFirstOrderConstraint} |
| 1236 |
|
Using Equation (\ref{introEquation:motionHamiltonianCoordinate}, |
| 1237 |
|
\ref{introEquation:motionHamiltonianMomentum}), one can write down |
| 1238 |
|
the equations of motion, |
| 1259 |
– |
\[ |
| 1260 |
– |
\begin{array}{c} |
| 1261 |
– |
\frac{{dq}}{{dt}} = \frac{p}{m} \label{introEquation:RBMotionPosition}\\ |
| 1262 |
– |
\frac{{dp}}{{dt}} = - \nabla _q V(q,Q) \label{introEquation:RBMotionMomentum}\\ |
| 1263 |
– |
\frac{{dQ}}{{dt}} = PJ^{ - 1} \label{introEquation:RBMotionRotation}\\ |
| 1264 |
– |
\frac{{dP}}{{dt}} = - \nabla _Q V(q,Q) - 2Q\Lambda . \label{introEquation:RBMotionP}\\ |
| 1265 |
– |
\end{array} |
| 1266 |
– |
\] |
| 1239 |
|
|
| 1240 |
+ |
\begin{eqnarray} |
| 1241 |
+ |
\frac{{dq}}{{dt}} & = & \frac{p}{m} \label{introEquation:RBMotionPosition}\\ |
| 1242 |
+ |
\frac{{dp}}{{dt}} & = & - \nabla _q V(q,Q) \label{introEquation:RBMotionMomentum}\\ |
| 1243 |
+ |
\frac{{dQ}}{{dt}} & = & PJ^{ - 1} \label{introEquation:RBMotionRotation}\\ |
| 1244 |
+ |
\frac{{dP}}{{dt}} & = & - \nabla _Q V(q,Q) - 2Q\Lambda . \label{introEquation:RBMotionP} |
| 1245 |
+ |
\end{eqnarray} |
| 1246 |
+ |
|
| 1247 |
|
In general, there are two ways to satisfy the holonomic constraints. |
| 1248 |
< |
We can use constraint force provided by lagrange multiplier on the |
| 1249 |
< |
normal manifold to keep the motion on constraint space. Or we can |
| 1250 |
< |
simply evolve the system in constraint manifold. These two methods |
| 1251 |
< |
are proved to be equivalent. The holonomic constraint and equations |
| 1252 |
< |
of motions define a constraint manifold for rigid body |
| 1248 |
> |
We can use a constraint force provided by a Lagrange multiplier on |
| 1249 |
> |
the normal manifold to keep the motion on constraint space. Or we |
| 1250 |
> |
can simply evolve the system on the constraint manifold. These two |
| 1251 |
> |
methods have been proved to be equivalent. The holonomic constraint |
| 1252 |
> |
and equations of motions define a constraint manifold for rigid |
| 1253 |
> |
bodies |
| 1254 |
|
\[ |
| 1255 |
|
M = \left\{ {(Q,P):Q^T Q = 1,Q^T PJ^{ - 1} + J^{ - 1} P^T Q = 0} |
| 1256 |
|
\right\}. |
| 1259 |
|
Unfortunately, this constraint manifold is not the cotangent bundle |
| 1260 |
|
$T_{\star}SO(3)$. However, it turns out that under symplectic |
| 1261 |
|
transformation, the cotangent space and the phase space are |
| 1262 |
< |
diffeomorphic. Introducing |
| 1262 |
> |
diffeomorphic. By introducing |
| 1263 |
|
\[ |
| 1264 |
|
\tilde Q = Q,\tilde P = \frac{1}{2}\left( {P - QP^T Q} \right), |
| 1265 |
|
\] |
| 1291 |
|
respectively. |
| 1292 |
|
|
| 1293 |
|
As a common choice to describe the rotation dynamics of the rigid |
| 1294 |
< |
body, angular momentum on body frame $\Pi = Q^t P$ is introduced to |
| 1295 |
< |
rewrite the equations of motion, |
| 1294 |
> |
body, the angular momentum on the body fixed frame $\Pi = Q^t P$ is |
| 1295 |
> |
introduced to rewrite the equations of motion, |
| 1296 |
|
\begin{equation} |
| 1297 |
|
\begin{array}{l} |
| 1298 |
|
\mathop \Pi \limits^ \bullet = J^{ - 1} \Pi ^T \Pi + Q^T \sum\limits_i {F_i (q,Q)X_i^T } - \Lambda \\ |
| 1324 |
|
\[ |
| 1325 |
|
\hat vu = v \times u |
| 1326 |
|
\] |
| 1347 |
– |
|
| 1327 |
|
Using \ref{introEqaution:RBMotionPI}, one can construct a skew |
| 1328 |
|
matrix, |
| 1329 |
|
\begin{equation} |
| 1330 |
< |
(\mathop \Pi \limits^ \bullet - \mathop \Pi \limits^ \bullet ^T |
| 1330 |
> |
(\mathop \Pi \limits^ \bullet - \mathop \Pi \limits^ {\bullet ^T} |
| 1331 |
|
){\rm{ }} = {\rm{ }}(\Pi - \Pi ^T ){\rm{ }}(J^{ - 1} \Pi + \Pi J^{ |
| 1332 |
|
- 1} ) + \sum\limits_i {[Q^T F_i (r,Q)X_i^T - X_i F_i (r,Q)^T Q]} - |
| 1333 |
|
(\Lambda - \Lambda ^T ) . \label{introEquation:skewMatrixPI} |
| 1335 |
|
Since $\Lambda$ is symmetric, the last term of Equation |
| 1336 |
|
\ref{introEquation:skewMatrixPI} is zero, which implies the Lagrange |
| 1337 |
|
multiplier $\Lambda$ is absent from the equations of motion. This |
| 1338 |
< |
unique property eliminate the requirement of iterations which can |
| 1338 |
> |
unique property eliminates the requirement of iterations which can |
| 1339 |
|
not be avoided in other methods\cite{Kol1997, Omelyan1998}. |
| 1340 |
|
|
| 1341 |
< |
Applying hat-map isomorphism, we obtain the equation of motion for |
| 1342 |
< |
angular momentum on body frame |
| 1341 |
> |
Applying the hat-map isomorphism, we obtain the equation of motion |
| 1342 |
> |
for angular momentum on body frame |
| 1343 |
|
\begin{equation} |
| 1344 |
|
\dot \pi = \pi \times I^{ - 1} \pi + \sum\limits_i {\left( {Q^T |
| 1345 |
|
F_i (r,Q)} \right) \times X_i }. |
| 1354 |
|
\subsection{\label{introSection:SymplecticFreeRB}Symplectic |
| 1355 |
|
Lie-Poisson Integrator for Free Rigid Body} |
| 1356 |
|
|
| 1357 |
< |
If there is not external forces exerted on the rigid body, the only |
| 1358 |
< |
contribution to the rotational is from the kinetic potential (the |
| 1359 |
< |
first term of \ref{ introEquation:bodyAngularMotion}). The free |
| 1360 |
< |
rigid body is an example of Lie-Poisson system with Hamiltonian |
| 1357 |
> |
If there are no external forces exerted on the rigid body, the only |
| 1358 |
> |
contribution to the rotational motion is from the kinetic energy |
| 1359 |
> |
(the first term of \ref{introEquation:bodyAngularMotion}). The free |
| 1360 |
> |
rigid body is an example of a Lie-Poisson system with Hamiltonian |
| 1361 |
|
function |
| 1362 |
|
\begin{equation} |
| 1363 |
|
T^r (\pi ) = T_1 ^r (\pi _1 ) + T_2^r (\pi _2 ) + T_3^r (\pi _3 ) |
| 1405 |
|
\end{array}} \right),\theta _1 = \frac{{\pi _1 }}{{I_1 }}\Delta t. |
| 1406 |
|
\] |
| 1407 |
|
To reduce the cost of computing expensive functions in $e^{\Delta |
| 1408 |
< |
tR_1 }$, we can use Cayley transformation, |
| 1408 |
> |
tR_1 }$, we can use Cayley transformation to obtain a single-aixs |
| 1409 |
> |
propagator, |
| 1410 |
|
\[ |
| 1411 |
|
e^{\Delta tR_1 } \approx (1 - \Delta tR_1 )^{ - 1} (1 + \Delta tR_1 |
| 1412 |
|
) |
| 1413 |
|
\] |
| 1414 |
|
The flow maps for $T_2^r$ and $T_3^r$ can be found in the same |
| 1415 |
< |
manner. |
| 1416 |
< |
|
| 1437 |
< |
In order to construct a second-order symplectic method, we split the |
| 1438 |
< |
angular kinetic Hamiltonian function can into five terms |
| 1415 |
> |
manner. In order to construct a second-order symplectic method, we |
| 1416 |
> |
split the angular kinetic Hamiltonian function can into five terms |
| 1417 |
|
\[ |
| 1418 |
|
T^r (\pi ) = \frac{1}{2}T_1 ^r (\pi _1 ) + \frac{1}{2}T_2^r (\pi _2 |
| 1419 |
|
) + T_3^r (\pi _3 ) + \frac{1}{2}T_2^r (\pi _2 ) + \frac{1}{2}T_1 ^r |
| 1420 |
< |
(\pi _1 ) |
| 1421 |
< |
\]. |
| 1422 |
< |
Concatenating flows corresponding to these five terms, we can obtain |
| 1423 |
< |
an symplectic integrator, |
| 1420 |
> |
(\pi _1 ). |
| 1421 |
> |
\] |
| 1422 |
> |
By concatenating the propagators corresponding to these five terms, |
| 1423 |
> |
we can obtain an symplectic integrator, |
| 1424 |
|
\[ |
| 1425 |
|
\varphi _{\Delta t,T^r } = \varphi _{\Delta t/2,\pi _1 } \circ |
| 1426 |
|
\varphi _{\Delta t/2,\pi _2 } \circ \varphi _{\Delta t,\pi _3 } |
| 1447 |
|
\] |
| 1448 |
|
Thus $ [\nabla _\pi F(\pi )]^T J(\pi ) = - S'(\frac{{\parallel \pi |
| 1449 |
|
\parallel ^2 }}{2})\pi \times \pi = 0 $. This explicit |
| 1450 |
< |
Lie-Poisson integrator is found to be extremely efficient and stable |
| 1451 |
< |
which can be explained by the fact the small angle approximation is |
| 1452 |
< |
used and the norm of the angular momentum is conserved. |
| 1450 |
> |
Lie-Poisson integrator is found to be both extremely efficient and |
| 1451 |
> |
stable. These properties can be explained by the fact the small |
| 1452 |
> |
angle approximation is used and the norm of the angular momentum is |
| 1453 |
> |
conserved. |
| 1454 |
|
|
| 1455 |
|
\subsection{\label{introSection:RBHamiltonianSplitting} Hamiltonian |
| 1456 |
|
Splitting for Rigid Body} |
| 1477 |
|
\end{tabular} |
| 1478 |
|
\end{center} |
| 1479 |
|
\end{table} |
| 1480 |
< |
A second-order symplectic method is now obtained by the |
| 1481 |
< |
composition of the flow maps, |
| 1480 |
> |
A second-order symplectic method is now obtained by the composition |
| 1481 |
> |
of the position and velocity propagators, |
| 1482 |
|
\[ |
| 1483 |
|
\varphi _{\Delta t} = \varphi _{\Delta t/2,V} \circ \varphi |
| 1484 |
|
_{\Delta t,T} \circ \varphi _{\Delta t/2,V}. |
| 1485 |
|
\] |
| 1486 |
|
Moreover, $\varphi _{\Delta t/2,V}$ can be divided into two |
| 1487 |
< |
sub-flows which corresponding to force and torque respectively, |
| 1487 |
> |
sub-propagators which corresponding to force and torque |
| 1488 |
> |
respectively, |
| 1489 |
|
\[ |
| 1490 |
|
\varphi _{\Delta t/2,V} = \varphi _{\Delta t/2,F} \circ \varphi |
| 1491 |
|
_{\Delta t/2,\tau }. |
| 1492 |
|
\] |
| 1493 |
|
Since the associated operators of $\varphi _{\Delta t/2,F} $ and |
| 1494 |
< |
$\circ \varphi _{\Delta t/2,\tau }$ are commuted, the composition |
| 1495 |
< |
order inside $\varphi _{\Delta t/2,V}$ does not matter. |
| 1496 |
< |
|
| 1497 |
< |
Furthermore, kinetic potential can be separated to translational |
| 1518 |
< |
kinetic term, $T^t (p)$, and rotational kinetic term, $T^r (\pi )$, |
| 1494 |
> |
$\circ \varphi _{\Delta t/2,\tau }$ commute, the composition order |
| 1495 |
> |
inside $\varphi _{\Delta t/2,V}$ does not matter. Furthermore, the |
| 1496 |
> |
kinetic energy can be separated to translational kinetic term, $T^t |
| 1497 |
> |
(p)$, and rotational kinetic term, $T^r (\pi )$, |
| 1498 |
|
\begin{equation} |
| 1499 |
|
T(p,\pi ) =T^t (p) + T^r (\pi ). |
| 1500 |
|
\end{equation} |
| 1501 |
|
where $ T^t (p) = \frac{1}{2}p^T m^{ - 1} p $ and $T^r (\pi )$ is |
| 1502 |
|
defined by \ref{introEquation:rotationalKineticRB}. Therefore, the |
| 1503 |
< |
corresponding flow maps are given by |
| 1503 |
> |
corresponding propagators are given by |
| 1504 |
|
\[ |
| 1505 |
|
\varphi _{\Delta t,T} = \varphi _{\Delta t,T^t } \circ \varphi |
| 1506 |
|
_{\Delta t,T^r }. |
| 1507 |
|
\] |
| 1508 |
< |
Finally, we obtain the overall symplectic flow maps for free moving |
| 1509 |
< |
rigid body |
| 1508 |
> |
Finally, we obtain the overall symplectic propagators for freely |
| 1509 |
> |
moving rigid bodies |
| 1510 |
|
\begin{equation} |
| 1511 |
|
\begin{array}{c} |
| 1512 |
|
\varphi _{\Delta t} = \varphi _{\Delta t/2,F} \circ \varphi _{\Delta t/2,\tau } \\ |
| 1520 |
|
As an alternative to newtonian dynamics, Langevin dynamics, which |
| 1521 |
|
mimics a simple heat bath with stochastic and dissipative forces, |
| 1522 |
|
has been applied in a variety of studies. This section will review |
| 1523 |
< |
the theory of Langevin dynamics simulation. A brief derivation of |
| 1524 |
< |
generalized Langevin equation will be given first. Follow that, we |
| 1525 |
< |
will discuss the physical meaning of the terms appearing in the |
| 1526 |
< |
equation as well as the calculation of friction tensor from |
| 1527 |
< |
hydrodynamics theory. |
| 1523 |
> |
the theory of Langevin dynamics. A brief derivation of generalized |
| 1524 |
> |
Langevin equation will be given first. Following that, we will |
| 1525 |
> |
discuss the physical meaning of the terms appearing in the equation |
| 1526 |
> |
as well as the calculation of friction tensor from hydrodynamics |
| 1527 |
> |
theory. |
| 1528 |
|
|
| 1529 |
|
\subsection{\label{introSection:generalizedLangevinDynamics}Derivation of Generalized Langevin Equation} |
| 1530 |
|
|
| 1531 |
< |
Harmonic bath model, in which an effective set of harmonic |
| 1531 |
> |
A harmonic bath model, in which an effective set of harmonic |
| 1532 |
|
oscillators are used to mimic the effect of a linearly responding |
| 1533 |
|
environment, has been widely used in quantum chemistry and |
| 1534 |
|
statistical mechanics. One of the successful applications of |
| 1535 |
< |
Harmonic bath model is the derivation of Deriving Generalized |
| 1536 |
< |
Langevin Dynamics. Lets consider a system, in which the degree of |
| 1535 |
> |
Harmonic bath model is the derivation of the Generalized Langevin |
| 1536 |
> |
Dynamics (GLE). Lets consider a system, in which the degree of |
| 1537 |
|
freedom $x$ is assumed to couple to the bath linearly, giving a |
| 1538 |
|
Hamiltonian of the form |
| 1539 |
|
\begin{equation} |
| 1540 |
|
H = \frac{{p^2 }}{{2m}} + U(x) + H_B + \Delta U(x,x_1 , \ldots x_N) |
| 1541 |
|
\label{introEquation:bathGLE}. |
| 1542 |
|
\end{equation} |
| 1543 |
< |
Here $p$ is a momentum conjugate to $q$, $m$ is the mass associated |
| 1544 |
< |
with this degree of freedom, $H_B$ is harmonic bath Hamiltonian, |
| 1543 |
> |
Here $p$ is a momentum conjugate to $x$, $m$ is the mass associated |
| 1544 |
> |
with this degree of freedom, $H_B$ is a harmonic bath Hamiltonian, |
| 1545 |
|
\[ |
| 1546 |
|
H_B = \sum\limits_{\alpha = 1}^N {\left\{ {\frac{{p_\alpha ^2 |
| 1547 |
|
}}{{2m_\alpha }} + \frac{1}{2}m_\alpha \omega _\alpha ^2 } |
| 1549 |
|
\] |
| 1550 |
|
where the index $\alpha$ runs over all the bath degrees of freedom, |
| 1551 |
|
$\omega _\alpha$ are the harmonic bath frequencies, $m_\alpha$ are |
| 1552 |
< |
the harmonic bath masses, and $\Delta U$ is bilinear system-bath |
| 1552 |
> |
the harmonic bath masses, and $\Delta U$ is a bilinear system-bath |
| 1553 |
|
coupling, |
| 1554 |
|
\[ |
| 1555 |
|
\Delta U = - \sum\limits_{\alpha = 1}^N {g_\alpha x_\alpha x} |
| 1556 |
|
\] |
| 1557 |
< |
where $g_\alpha$ are the coupling constants between the bath and the |
| 1558 |
< |
coordinate $x$. Introducing |
| 1557 |
> |
where $g_\alpha$ are the coupling constants between the bath |
| 1558 |
> |
coordinates ($x_ \alpha$) and the system coordinate ($x$). |
| 1559 |
> |
Introducing |
| 1560 |
|
\[ |
| 1561 |
|
W(x) = U(x) - \sum\limits_{\alpha = 1}^N {\frac{{g_\alpha ^2 |
| 1562 |
|
}}{{2m_\alpha w_\alpha ^2 }}} x^2 |
| 1571 |
|
\] |
| 1572 |
|
Since the first two terms of the new Hamiltonian depend only on the |
| 1573 |
|
system coordinates, we can get the equations of motion for |
| 1574 |
< |
Generalized Langevin Dynamics by Hamilton's equations |
| 1595 |
< |
\ref{introEquation:motionHamiltonianCoordinate, |
| 1596 |
< |
introEquation:motionHamiltonianMomentum}, |
| 1574 |
> |
Generalized Langevin Dynamics by Hamilton's equations, |
| 1575 |
|
\begin{equation} |
| 1576 |
|
m\ddot x = - \frac{{\partial W(x)}}{{\partial x}} - |
| 1577 |
|
\sum\limits_{\alpha = 1}^N {g_\alpha \left( {x_\alpha - |
| 1588 |
|
In order to derive an equation for $x$, the dynamics of the bath |
| 1589 |
|
variables $x_\alpha$ must be solved exactly first. As an integral |
| 1590 |
|
transform which is particularly useful in solving linear ordinary |
| 1591 |
< |
differential equations, Laplace transform is the appropriate tool to |
| 1592 |
< |
solve this problem. The basic idea is to transform the difficult |
| 1591 |
> |
differential equations,the Laplace transform is the appropriate tool |
| 1592 |
> |
to solve this problem. The basic idea is to transform the difficult |
| 1593 |
|
differential equations into simple algebra problems which can be |
| 1594 |
< |
solved easily. Then applying inverse Laplace transform, also known |
| 1595 |
< |
as the Bromwich integral, we can retrieve the solutions of the |
| 1594 |
> |
solved easily. Then, by applying the inverse Laplace transform, also |
| 1595 |
> |
known as the Bromwich integral, we can retrieve the solutions of the |
| 1596 |
|
original problems. |
| 1597 |
|
|
| 1598 |
|
Let $f(t)$ be a function defined on $ [0,\infty ) $. The Laplace |
| 1612 |
|
\end{eqnarray*} |
| 1613 |
|
|
| 1614 |
|
|
| 1615 |
< |
Applying Laplace transform to the bath coordinates, we obtain |
| 1615 |
> |
Applying the Laplace transform to the bath coordinates, we obtain |
| 1616 |
|
\begin{eqnarray*} |
| 1617 |
|
p^2 L(x_\alpha ) - px_\alpha (0) - \dot x_\alpha (0) & = & - \omega _\alpha ^2 L(x_\alpha ) + \frac{{g_\alpha }}{{\omega _\alpha }}L(x) \\ |
| 1618 |
|
L(x_\alpha ) & = & \frac{{\frac{{g_\alpha }}{{\omega _\alpha }}L(x) + px_\alpha (0) + \dot x_\alpha (0)}}{{p^2 + \omega _\alpha ^2 }} \\ |
| 1635 |
|
\] |
| 1636 |
|
, we obtain |
| 1637 |
|
\begin{eqnarray*} |
| 1638 |
< |
m\ddot x & = & - \frac{{\partial W(x)}}{{\partial x}} - |
| 1638 |
> |
m\ddot x & = & - \frac{{\partial W(x)}}{{\partial x}} - |
| 1639 |
|
\sum\limits_{\alpha = 1}^N {\left\{ {\left( { - \frac{{g_\alpha ^2 |
| 1640 |
|
}}{{m_\alpha \omega _\alpha ^2 }}} \right)\int_0^t {\cos (\omega |
| 1641 |
< |
_\alpha t)\dot x(t - \tau )d\tau - \left[ {g_\alpha x_\alpha (0) |
| 1642 |
< |
- \frac{{g_\alpha }}{{m_\alpha \omega _\alpha }}} \right]\cos |
| 1643 |
< |
(\omega _\alpha t) - \frac{{g_\alpha \dot x_\alpha (0)}}{{\omega |
| 1644 |
< |
_\alpha }}\sin (\omega _\alpha t)} } \right\}} |
| 1645 |
< |
% |
| 1646 |
< |
& = & - \frac{{\partial W(x)}}{{\partial x}} - \int_0^t |
| 1641 |
> |
_\alpha t)\dot x(t - \tau )d\tau } } \right\}} \\ |
| 1642 |
> |
& & + \sum\limits_{\alpha = 1}^N {\left\{ {\left[ {g_\alpha |
| 1643 |
> |
x_\alpha (0) - \frac{{g_\alpha }}{{m_\alpha \omega _\alpha }}} |
| 1644 |
> |
\right]\cos (\omega _\alpha t) + \frac{{g_\alpha \dot x_\alpha |
| 1645 |
> |
(0)}}{{\omega _\alpha }}\sin (\omega _\alpha t)} \right\}} |
| 1646 |
> |
\end{eqnarray*} |
| 1647 |
> |
\begin{eqnarray*} |
| 1648 |
> |
m\ddot x & = & - \frac{{\partial W(x)}}{{\partial x}} - \int_0^t |
| 1649 |
|
{\sum\limits_{\alpha = 1}^N {\left( { - \frac{{g_\alpha ^2 |
| 1650 |
|
}}{{m_\alpha \omega _\alpha ^2 }}} \right)\cos (\omega _\alpha |
| 1651 |
< |
t)\dot x(t - \tau )d} \tau } + \sum\limits_{\alpha = 1}^N {\left\{ |
| 1652 |
< |
{\left[ {g_\alpha x_\alpha (0) - \frac{{g_\alpha }}{{m_\alpha |
| 1653 |
< |
\omega _\alpha }}} \right]\cos (\omega _\alpha t) + |
| 1654 |
< |
\frac{{g_\alpha \dot x_\alpha (0)}}{{\omega _\alpha }}\sin |
| 1655 |
< |
(\omega _\alpha t)} \right\}} |
| 1651 |
> |
t)\dot x(t - \tau )d} \tau } \\ |
| 1652 |
> |
& & + \sum\limits_{\alpha = 1}^N {\left\{ {\left[ {g_\alpha |
| 1653 |
> |
x_\alpha (0) - \frac{{g_\alpha }}{{m_\alpha \omega _\alpha }}} |
| 1654 |
> |
\right]\cos (\omega _\alpha t) + \frac{{g_\alpha \dot x_\alpha |
| 1655 |
> |
(0)}}{{\omega _\alpha }}\sin (\omega _\alpha t)} \right\}} |
| 1656 |
|
\end{eqnarray*} |
| 1657 |
|
Introducing a \emph{dynamic friction kernel} |
| 1658 |
|
\begin{equation} |
| 1676 |
|
\end{equation} |
| 1677 |
|
which is known as the \emph{generalized Langevin equation}. |
| 1678 |
|
|
| 1679 |
< |
\subsubsection{\label{introSection:randomForceDynamicFrictionKernel}Random Force and Dynamic Friction Kernel} |
| 1679 |
> |
\subsubsection{\label{introSection:randomForceDynamicFrictionKernel}\textbf{Random Force and Dynamic Friction Kernel}} |
| 1680 |
|
|
| 1681 |
|
One may notice that $R(t)$ depends only on initial conditions, which |
| 1682 |
|
implies it is completely deterministic within the context of a |
| 1689 |
|
\end{array} |
| 1690 |
|
\] |
| 1691 |
|
This property is what we expect from a truly random process. As long |
| 1692 |
< |
as the model, which is gaussian distribution in general, chosen for |
| 1693 |
< |
$R(t)$ is a truly random process, the stochastic nature of the GLE |
| 1714 |
< |
still remains. |
| 1692 |
> |
as the model chosen for $R(t)$ was a gaussian distribution in |
| 1693 |
> |
general, the stochastic nature of the GLE still remains. |
| 1694 |
|
|
| 1695 |
|
%dynamic friction kernel |
| 1696 |
|
The convolution integral |
| 1711 |
|
m\ddot x = - \frac{\partial }{{\partial x}}\left( {W(x) + |
| 1712 |
|
\frac{1}{2}\xi _0 (x - x_0 )^2 } \right) + R(t), |
| 1713 |
|
\] |
| 1714 |
< |
which can be used to describe dynamic caging effect. The other |
| 1715 |
< |
extreme is the bath that responds infinitely quickly to motions in |
| 1716 |
< |
the system. Thus, $\xi (t)$ can be taken as a $delta$ function in |
| 1717 |
< |
time: |
| 1714 |
> |
which can be used to describe the effect of dynamic caging in |
| 1715 |
> |
viscous solvents. The other extreme is the bath that responds |
| 1716 |
> |
infinitely quickly to motions in the system. Thus, $\xi (t)$ can be |
| 1717 |
> |
taken as a $delta$ function in time: |
| 1718 |
|
\[ |
| 1719 |
|
\xi (t) = 2\xi _0 \delta (t) |
| 1720 |
|
\] |
| 1730 |
|
\end{equation} |
| 1731 |
|
which is known as the Langevin equation. The static friction |
| 1732 |
|
coefficient $\xi _0$ can either be calculated from spectral density |
| 1733 |
< |
or be determined by Stokes' law for regular shaped particles.A |
| 1733 |
> |
or be determined by Stokes' law for regular shaped particles. A |
| 1734 |
|
briefly review on calculating friction tensor for arbitrary shaped |
| 1735 |
|
particles is given in Sec.~\ref{introSection:frictionTensor}. |
| 1736 |
|
|
| 1737 |
< |
\subsubsection{\label{introSection:secondFluctuationDissipation}The Second Fluctuation Dissipation Theorem} |
| 1737 |
> |
\subsubsection{\label{introSection:secondFluctuationDissipation}\textbf{The Second Fluctuation Dissipation Theorem}} |
| 1738 |
|
|
| 1739 |
|
Defining a new set of coordinates, |
| 1740 |
|
\[ |
| 1763 |
|
\end{equation} |
| 1764 |
|
In effect, it acts as a constraint on the possible ways in which one |
| 1765 |
|
can model the random force and friction kernel. |
| 1787 |
– |
|
| 1788 |
– |
\subsection{\label{introSection:frictionTensor} Friction Tensor} |
| 1789 |
– |
Theoretically, the friction kernel can be determined using velocity |
| 1790 |
– |
autocorrelation function. However, this approach become impractical |
| 1791 |
– |
when the system become more and more complicate. Instead, various |
| 1792 |
– |
approaches based on hydrodynamics have been developed to calculate |
| 1793 |
– |
the friction coefficients. The friction effect is isotropic in |
| 1794 |
– |
Equation, $\zeta$ can be taken as a scalar. In general, friction |
| 1795 |
– |
tensor $\Xi$ is a $6\times 6$ matrix given by |
| 1796 |
– |
\[ |
| 1797 |
– |
\Xi = \left( {\begin{array}{*{20}c} |
| 1798 |
– |
{\Xi _{}^{tt} } & {\Xi _{}^{rt} } \\ |
| 1799 |
– |
{\Xi _{}^{tr} } & {\Xi _{}^{rr} } \\ |
| 1800 |
– |
\end{array}} \right). |
| 1801 |
– |
\] |
| 1802 |
– |
Here, $ {\Xi^{tt} }$ and $ {\Xi^{rr} }$ are translational friction |
| 1803 |
– |
tensor and rotational resistance (friction) tensor respectively, |
| 1804 |
– |
while ${\Xi^{tr} }$ is translation-rotation coupling tensor and $ |
| 1805 |
– |
{\Xi^{rt} }$ is rotation-translation coupling tensor. When a |
| 1806 |
– |
particle moves in a fluid, it may experience friction force or |
| 1807 |
– |
torque along the opposite direction of the velocity or angular |
| 1808 |
– |
velocity, |
| 1809 |
– |
\[ |
| 1810 |
– |
\left( \begin{array}{l} |
| 1811 |
– |
F_R \\ |
| 1812 |
– |
\tau _R \\ |
| 1813 |
– |
\end{array} \right) = - \left( {\begin{array}{*{20}c} |
| 1814 |
– |
{\Xi ^{tt} } & {\Xi ^{rt} } \\ |
| 1815 |
– |
{\Xi ^{tr} } & {\Xi ^{rr} } \\ |
| 1816 |
– |
\end{array}} \right)\left( \begin{array}{l} |
| 1817 |
– |
v \\ |
| 1818 |
– |
w \\ |
| 1819 |
– |
\end{array} \right) |
| 1820 |
– |
\] |
| 1821 |
– |
where $F_r$ is the friction force and $\tau _R$ is the friction |
| 1822 |
– |
toque. |
| 1823 |
– |
|
| 1824 |
– |
\subsubsection{\label{introSection:resistanceTensorRegular}The Resistance Tensor for Regular Shape} |
| 1825 |
– |
|
| 1826 |
– |
For a spherical particle, the translational and rotational friction |
| 1827 |
– |
constant can be calculated from Stoke's law, |
| 1828 |
– |
\[ |
| 1829 |
– |
\Xi ^{tt} = \left( {\begin{array}{*{20}c} |
| 1830 |
– |
{6\pi \eta R} & 0 & 0 \\ |
| 1831 |
– |
0 & {6\pi \eta R} & 0 \\ |
| 1832 |
– |
0 & 0 & {6\pi \eta R} \\ |
| 1833 |
– |
\end{array}} \right) |
| 1834 |
– |
\] |
| 1835 |
– |
and |
| 1836 |
– |
\[ |
| 1837 |
– |
\Xi ^{rr} = \left( {\begin{array}{*{20}c} |
| 1838 |
– |
{8\pi \eta R^3 } & 0 & 0 \\ |
| 1839 |
– |
0 & {8\pi \eta R^3 } & 0 \\ |
| 1840 |
– |
0 & 0 & {8\pi \eta R^3 } \\ |
| 1841 |
– |
\end{array}} \right) |
| 1842 |
– |
\] |
| 1843 |
– |
where $\eta$ is the viscosity of the solvent and $R$ is the |
| 1844 |
– |
hydrodynamics radius. |
| 1845 |
– |
|
| 1846 |
– |
Other non-spherical shape, such as cylinder and ellipsoid |
| 1847 |
– |
\textit{etc}, are widely used as reference for developing new |
| 1848 |
– |
hydrodynamics theory, because their properties can be calculated |
| 1849 |
– |
exactly. In 1936, Perrin extended Stokes's law to general ellipsoid, |
| 1850 |
– |
also called a triaxial ellipsoid, which is given in Cartesian |
| 1851 |
– |
coordinates by\cite{Perrin1934, Perrin1936} |
| 1852 |
– |
\[ |
| 1853 |
– |
\frac{{x^2 }}{{a^2 }} + \frac{{y^2 }}{{b^2 }} + \frac{{z^2 }}{{c^2 |
| 1854 |
– |
}} = 1 |
| 1855 |
– |
\] |
| 1856 |
– |
where the semi-axes are of lengths $a$, $b$, and $c$. Unfortunately, |
| 1857 |
– |
due to the complexity of the elliptic integral, only the ellipsoid |
| 1858 |
– |
with the restriction of two axes having to be equal, \textit{i.e.} |
| 1859 |
– |
prolate($ a \ge b = c$) and oblate ($ a < b = c $), can be solved |
| 1860 |
– |
exactly. Introducing an elliptic integral parameter $S$ for prolate, |
| 1861 |
– |
\[ |
| 1862 |
– |
S = \frac{2}{{\sqrt {a^2 - b^2 } }}\ln \frac{{a + \sqrt {a^2 - b^2 |
| 1863 |
– |
} }}{b}, |
| 1864 |
– |
\] |
| 1865 |
– |
and oblate, |
| 1866 |
– |
\[ |
| 1867 |
– |
S = \frac{2}{{\sqrt {b^2 - a^2 } }}arctg\frac{{\sqrt {b^2 - a^2 } |
| 1868 |
– |
}}{a} |
| 1869 |
– |
\], |
| 1870 |
– |
one can write down the translational and rotational resistance |
| 1871 |
– |
tensors |
| 1872 |
– |
\[ |
| 1873 |
– |
\begin{array}{l} |
| 1874 |
– |
\Xi _a^{tt} = 16\pi \eta \frac{{a^2 - b^2 }}{{(2a^2 - b^2 )S - 2a}} \\ |
| 1875 |
– |
\Xi _b^{tt} = \Xi _c^{tt} = 32\pi \eta \frac{{a^2 - b^2 }}{{(2a^2 - 3b^2 )S + 2a}} \\ |
| 1876 |
– |
\end{array}, |
| 1877 |
– |
\] |
| 1878 |
– |
and |
| 1879 |
– |
\[ |
| 1880 |
– |
\begin{array}{l} |
| 1881 |
– |
\Xi _a^{rr} = \frac{{32\pi }}{3}\eta \frac{{(a^2 - b^2 )b^2 }}{{2a - b^2 S}} \\ |
| 1882 |
– |
\Xi _b^{rr} = \Xi _c^{rr} = \frac{{32\pi }}{3}\eta \frac{{(a^4 - b^4 )}}{{(2a^2 - b^2 )S - 2a}} \\ |
| 1883 |
– |
\end{array}. |
| 1884 |
– |
\] |
| 1885 |
– |
|
| 1886 |
– |
\subsubsection{\label{introSection:resistanceTensorRegularArbitrary}The Resistance Tensor for Arbitrary Shape} |
| 1887 |
– |
|
| 1888 |
– |
Unlike spherical and other regular shaped molecules, there is not |
| 1889 |
– |
analytical solution for friction tensor of any arbitrary shaped |
| 1890 |
– |
rigid molecules. The ellipsoid of revolution model and general |
| 1891 |
– |
triaxial ellipsoid model have been used to approximate the |
| 1892 |
– |
hydrodynamic properties of rigid bodies. However, since the mapping |
| 1893 |
– |
from all possible ellipsoidal space, $r$-space, to all possible |
| 1894 |
– |
combination of rotational diffusion coefficients, $D$-space is not |
| 1895 |
– |
unique\cite{Wegener1979} as well as the intrinsic coupling between |
| 1896 |
– |
translational and rotational motion of rigid body, general ellipsoid |
| 1897 |
– |
is not always suitable for modeling arbitrarily shaped rigid |
| 1898 |
– |
molecule. A number of studies have been devoted to determine the |
| 1899 |
– |
friction tensor for irregularly shaped rigid bodies using more |
| 1900 |
– |
advanced method where the molecule of interest was modeled by |
| 1901 |
– |
combinations of spheres(beads)\cite{Carrasco1999} and the |
| 1902 |
– |
hydrodynamics properties of the molecule can be calculated using the |
| 1903 |
– |
hydrodynamic interaction tensor. Let us consider a rigid assembly of |
| 1904 |
– |
$N$ beads immersed in a continuous medium. Due to hydrodynamics |
| 1905 |
– |
interaction, the ``net'' velocity of $i$th bead, $v'_i$ is different |
| 1906 |
– |
than its unperturbed velocity $v_i$, |
| 1907 |
– |
\[ |
| 1908 |
– |
v'_i = v_i - \sum\limits_{j \ne i} {T_{ij} F_j } |
| 1909 |
– |
\] |
| 1910 |
– |
where $F_i$ is the frictional force, and $T_{ij}$ is the |
| 1911 |
– |
hydrodynamic interaction tensor. The friction force of $i$th bead is |
| 1912 |
– |
proportional to its ``net'' velocity |
| 1913 |
– |
\begin{equation} |
| 1914 |
– |
F_i = \zeta _i v_i - \zeta _i \sum\limits_{j \ne i} {T_{ij} F_j }. |
| 1915 |
– |
\label{introEquation:tensorExpression} |
| 1916 |
– |
\end{equation} |
| 1917 |
– |
This equation is the basis for deriving the hydrodynamic tensor. In |
| 1918 |
– |
1930, Oseen and Burgers gave a simple solution to Equation |
| 1919 |
– |
\ref{introEquation:tensorExpression} |
| 1920 |
– |
\begin{equation} |
| 1921 |
– |
T_{ij} = \frac{1}{{8\pi \eta r_{ij} }}\left( {I + \frac{{R_{ij} |
| 1922 |
– |
R_{ij}^T }}{{R_{ij}^2 }}} \right). |
| 1923 |
– |
\label{introEquation:oseenTensor} |
| 1924 |
– |
\end{equation} |
| 1925 |
– |
Here $R_{ij}$ is the distance vector between bead $i$ and bead $j$. |
| 1926 |
– |
A second order expression for element of different size was |
| 1927 |
– |
introduced by Rotne and Prager\cite{Rotne1969} and improved by |
| 1928 |
– |
Garc\'{i}a de la Torre and Bloomfield\cite{Torre1977}, |
| 1929 |
– |
\begin{equation} |
| 1930 |
– |
T_{ij} = \frac{1}{{8\pi \eta R_{ij} }}\left[ {\left( {I + |
| 1931 |
– |
\frac{{R_{ij} R_{ij}^T }}{{R_{ij}^2 }}} \right) + R\frac{{\sigma |
| 1932 |
– |
_i^2 + \sigma _j^2 }}{{r_{ij}^2 }}\left( {\frac{I}{3} - |
| 1933 |
– |
\frac{{R_{ij} R_{ij}^T }}{{R_{ij}^2 }}} \right)} \right]. |
| 1934 |
– |
\label{introEquation:RPTensorNonOverlapped} |
| 1935 |
– |
\end{equation} |
| 1936 |
– |
Both of the Equation \ref{introEquation:oseenTensor} and Equation |
| 1937 |
– |
\ref{introEquation:RPTensorNonOverlapped} have an assumption $R_{ij} |
| 1938 |
– |
\ge \sigma _i + \sigma _j$. An alternative expression for |
| 1939 |
– |
overlapping beads with the same radius, $\sigma$, is given by |
| 1940 |
– |
\begin{equation} |
| 1941 |
– |
T_{ij} = \frac{1}{{6\pi \eta R_{ij} }}\left[ {\left( {1 - |
| 1942 |
– |
\frac{2}{{32}}\frac{{R_{ij} }}{\sigma }} \right)I + |
| 1943 |
– |
\frac{2}{{32}}\frac{{R_{ij} R_{ij}^T }}{{R_{ij} \sigma }}} \right] |
| 1944 |
– |
\label{introEquation:RPTensorOverlapped} |
| 1945 |
– |
\end{equation} |
| 1946 |
– |
|
| 1947 |
– |
To calculate the resistance tensor at an arbitrary origin $O$, we |
| 1948 |
– |
construct a $3N \times 3N$ matrix consisting of $N \times N$ |
| 1949 |
– |
$B_{ij}$ blocks |
| 1950 |
– |
\begin{equation} |
| 1951 |
– |
B = \left( {\begin{array}{*{20}c} |
| 1952 |
– |
{B_{11} } & \ldots & {B_{1N} } \\ |
| 1953 |
– |
\vdots & \ddots & \vdots \\ |
| 1954 |
– |
{B_{N1} } & \cdots & {B_{NN} } \\ |
| 1955 |
– |
\end{array}} \right), |
| 1956 |
– |
\end{equation} |
| 1957 |
– |
where $B_{ij}$ is given by |
| 1958 |
– |
\[ |
| 1959 |
– |
B_{ij} = \delta _{ij} \frac{I}{{6\pi \eta R}} + (1 - \delta _{ij} |
| 1960 |
– |
)T_{ij} |
| 1961 |
– |
\] |
| 1962 |
– |
where $\delta _{ij}$ is Kronecker delta function. Inverting matrix |
| 1963 |
– |
$B$, we obtain |
| 1964 |
– |
|
| 1965 |
– |
\[ |
| 1966 |
– |
C = B^{ - 1} = \left( {\begin{array}{*{20}c} |
| 1967 |
– |
{C_{11} } & \ldots & {C_{1N} } \\ |
| 1968 |
– |
\vdots & \ddots & \vdots \\ |
| 1969 |
– |
{C_{N1} } & \cdots & {C_{NN} } \\ |
| 1970 |
– |
\end{array}} \right) |
| 1971 |
– |
\] |
| 1972 |
– |
, which can be partitioned into $N \times N$ $3 \times 3$ block |
| 1973 |
– |
$C_{ij}$. With the help of $C_{ij}$ and skew matrix $U_i$ |
| 1974 |
– |
\[ |
| 1975 |
– |
U_i = \left( {\begin{array}{*{20}c} |
| 1976 |
– |
0 & { - z_i } & {y_i } \\ |
| 1977 |
– |
{z_i } & 0 & { - x_i } \\ |
| 1978 |
– |
{ - y_i } & {x_i } & 0 \\ |
| 1979 |
– |
\end{array}} \right) |
| 1980 |
– |
\] |
| 1981 |
– |
where $x_i$, $y_i$, $z_i$ are the components of the vector joining |
| 1982 |
– |
bead $i$ and origin $O$. Hence, the elements of resistance tensor at |
| 1983 |
– |
arbitrary origin $O$ can be written as |
| 1984 |
– |
\begin{equation} |
| 1985 |
– |
\begin{array}{l} |
| 1986 |
– |
\Xi _{}^{tt} = \sum\limits_i {\sum\limits_j {C_{ij} } } , \\ |
| 1987 |
– |
\Xi _{}^{tr} = \Xi _{}^{rt} = \sum\limits_i {\sum\limits_j {U_i C_{ij} } } , \\ |
| 1988 |
– |
\Xi _{}^{rr} = - \sum\limits_i {\sum\limits_j {U_i C_{ij} } } U_j \\ |
| 1989 |
– |
\end{array} |
| 1990 |
– |
\label{introEquation:ResistanceTensorArbitraryOrigin} |
| 1991 |
– |
\end{equation} |
| 1992 |
– |
|
| 1993 |
– |
The resistance tensor depends on the origin to which they refer. The |
| 1994 |
– |
proper location for applying friction force is the center of |
| 1995 |
– |
resistance (reaction), at which the trace of rotational resistance |
| 1996 |
– |
tensor, $ \Xi ^{rr}$ reaches minimum. Mathematically, the center of |
| 1997 |
– |
resistance is defined as an unique point of the rigid body at which |
| 1998 |
– |
the translation-rotation coupling tensor are symmetric, |
| 1999 |
– |
\begin{equation} |
| 2000 |
– |
\Xi^{tr} = \left( {\Xi^{tr} } \right)^T |
| 2001 |
– |
\label{introEquation:definitionCR} |
| 2002 |
– |
\end{equation} |
| 2003 |
– |
Form Equation \ref{introEquation:ResistanceTensorArbitraryOrigin}, |
| 2004 |
– |
we can easily find out that the translational resistance tensor is |
| 2005 |
– |
origin independent, while the rotational resistance tensor and |
| 2006 |
– |
translation-rotation coupling resistance tensor depend on the |
| 2007 |
– |
origin. Given resistance tensor at an arbitrary origin $O$, and a |
| 2008 |
– |
vector ,$r_{OP}(x_{OP}, y_{OP}, z_{OP})$, from $O$ to $P$, we can |
| 2009 |
– |
obtain the resistance tensor at $P$ by |
| 2010 |
– |
\begin{equation} |
| 2011 |
– |
\begin{array}{l} |
| 2012 |
– |
\Xi _P^{tt} = \Xi _O^{tt} \\ |
| 2013 |
– |
\Xi _P^{tr} = \Xi _P^{rt} = \Xi _O^{tr} - U_{OP} \Xi _O^{tt} \\ |
| 2014 |
– |
\Xi _P^{rr} = \Xi _O^{rr} - U_{OP} \Xi _O^{tt} U_{OP} + \Xi _O^{tr} U_{OP} - U_{OP} \Xi _O^{tr} ^{^T } \\ |
| 2015 |
– |
\end{array} |
| 2016 |
– |
\label{introEquation:resistanceTensorTransformation} |
| 2017 |
– |
\end{equation} |
| 2018 |
– |
where |
| 2019 |
– |
\[ |
| 2020 |
– |
U_{OP} = \left( {\begin{array}{*{20}c} |
| 2021 |
– |
0 & { - z_{OP} } & {y_{OP} } \\ |
| 2022 |
– |
{z_i } & 0 & { - x_{OP} } \\ |
| 2023 |
– |
{ - y_{OP} } & {x_{OP} } & 0 \\ |
| 2024 |
– |
\end{array}} \right) |
| 2025 |
– |
\] |
| 2026 |
– |
Using Equations \ref{introEquation:definitionCR} and |
| 2027 |
– |
\ref{introEquation:resistanceTensorTransformation}, one can locate |
| 2028 |
– |
the position of center of resistance, |
| 2029 |
– |
\begin{eqnarray*} |
| 2030 |
– |
\left( \begin{array}{l} |
| 2031 |
– |
x_{OR} \\ |
| 2032 |
– |
y_{OR} \\ |
| 2033 |
– |
z_{OR} \\ |
| 2034 |
– |
\end{array} \right) & = &\left( {\begin{array}{*{20}c} |
| 2035 |
– |
{(\Xi _O^{rr} )_{yy} + (\Xi _O^{rr} )_{zz} } & { - (\Xi _O^{rr} )_{xy} } & { - (\Xi _O^{rr} )_{xz} } \\ |
| 2036 |
– |
{ - (\Xi _O^{rr} )_{xy} } & {(\Xi _O^{rr} )_{zz} + (\Xi _O^{rr} )_{xx} } & { - (\Xi _O^{rr} )_{yz} } \\ |
| 2037 |
– |
{ - (\Xi _O^{rr} )_{xz} } & { - (\Xi _O^{rr} )_{yz} } & {(\Xi _O^{rr} )_{xx} + (\Xi _O^{rr} )_{yy} } \\ |
| 2038 |
– |
\end{array}} \right)^{ - 1} \\ |
| 2039 |
– |
& & \left( \begin{array}{l} |
| 2040 |
– |
(\Xi _O^{tr} )_{yz} - (\Xi _O^{tr} )_{zy} \\ |
| 2041 |
– |
(\Xi _O^{tr} )_{zx} - (\Xi _O^{tr} )_{xz} \\ |
| 2042 |
– |
(\Xi _O^{tr} )_{xy} - (\Xi _O^{tr} )_{yx} \\ |
| 2043 |
– |
\end{array} \right) \\ |
| 2044 |
– |
\end{eqnarray*} |
| 2045 |
– |
|
| 2046 |
– |
|
| 2047 |
– |
|
| 2048 |
– |
where $x_OR$, $y_OR$, $z_OR$ are the components of the vector |
| 2049 |
– |
joining center of resistance $R$ and origin $O$. |
