2 |
|
|
3 |
|
\section{\label{methodSection:rigidBodyIntegrators}Integrators for Rigid Body Motion in Molecular Dynamics} |
4 |
|
|
5 |
< |
In order to mimic the experiments, which are usually performed under |
5 |
> |
In order to mimic experiments which are usually performed under |
6 |
|
constant temperature and/or pressure, extended Hamiltonian system |
7 |
|
methods have been developed to generate statistical ensembles, such |
8 |
< |
as canonical ensemble and isobaric-isothermal ensemble \textit{etc}. |
9 |
< |
In addition to the standard ensemble, specific ensembles have been |
10 |
< |
developed to account for the anisotropy between the lateral and |
11 |
< |
normal directions of membranes. The $NPAT$ ensemble, in which the |
12 |
< |
normal pressure and the lateral surface area of the membrane are |
13 |
< |
kept constant, and the $NP\gamma T$ ensemble, in which the normal |
14 |
< |
pressure and the lateral surface tension are kept constant were |
15 |
< |
proposed to address this issue. |
8 |
> |
as the canonical and isobaric-isothermal ensembles. In addition to |
9 |
> |
the standard ensemble, specific ensembles have been developed to |
10 |
> |
account for the anisotropy between the lateral and normal directions |
11 |
> |
of membranes. The $NPAT$ ensemble, in which the normal pressure and |
12 |
> |
the lateral surface area of the membrane are kept constant, and the |
13 |
> |
$NP\gamma T$ ensemble, in which the normal pressure and the lateral |
14 |
> |
surface tension are kept constant were proposed to address the |
15 |
> |
issues. |
16 |
|
|
17 |
< |
Integration schemes for rotational motion of the rigid molecules in |
18 |
< |
microcanonical ensemble have been extensively studied in the last |
19 |
< |
two decades. Matubayasi developed a time-reversible integrator for |
20 |
< |
rigid bodies in quaternion representation. Although it is not |
21 |
< |
symplectic, this integrator still demonstrates a better long-time |
22 |
< |
energy conservation than traditional methods because of the |
23 |
< |
time-reversible nature. Extending Trotter-Suzuki to general system |
24 |
< |
with a flat phase space, Miller and his colleagues devised an novel |
25 |
< |
symplectic, time-reversible and volume-preserving integrator in |
26 |
< |
quaternion representation, which was shown to be superior to the |
27 |
< |
Matubayasi's time-reversible integrator. However, all of the |
28 |
< |
integrators in quaternion representation suffer from the |
29 |
< |
computational penalty of constructing a rotation matrix from |
30 |
< |
quaternions to evolve coordinates and velocities at every time step. |
31 |
< |
An alternative integration scheme utilizing rotation matrix directly |
32 |
< |
proposed by Dullweber, Leimkuhler and McLachlan (DLM) also preserved |
33 |
< |
the same structural properties of the Hamiltonian flow. In this |
34 |
< |
section, the integration scheme of DLM method will be reviewed and |
35 |
< |
extended to other ensembles. |
17 |
> |
Integration schemes for the rotational motion of the rigid molecules |
18 |
> |
in the microcanonical ensemble have been extensively studied over |
19 |
> |
the last two decades. Matubayasi developed a time-reversible |
20 |
> |
integrator for rigid bodies in quaternion representation. Although |
21 |
> |
it is not symplectic, this integrator still demonstrates a better |
22 |
> |
long-time energy conservation than Euler angle methods because of |
23 |
> |
the time-reversible nature. Extending the Trotter-Suzuki |
24 |
> |
factorization to general system with a flat phase space, Miller and |
25 |
> |
his colleagues devised a novel symplectic, time-reversible and |
26 |
> |
volume-preserving integrator in the quaternion representation, which |
27 |
> |
was shown to be superior to the Matubayasi's time-reversible |
28 |
> |
integrator. However, all of the integrators in the quaternion |
29 |
> |
representation suffer from the computational penalty of constructing |
30 |
> |
a rotation matrix from quaternions to evolve coordinates and |
31 |
> |
velocities at every time step. An alternative integration scheme |
32 |
> |
utilizing the rotation matrix directly proposed by Dullweber, |
33 |
> |
Leimkuhler and McLachlan (DLM) also preserved the same structural |
34 |
> |
properties of the Hamiltonian flow. In this section, the integration |
35 |
> |
scheme of DLM method will be reviewed and extended to other |
36 |
> |
ensembles. |
37 |
|
|
38 |
|
\subsection{\label{methodSection:DLM}Integrating the Equations of Motion: the |
39 |
|
DLM method} |
48 |
|
\item the error for a single time step is of order $\mathcal{O}\left(h^4\right)$ |
49 |
|
for timesteps of length $h$. |
50 |
|
\end{enumerate} |
50 |
– |
|
51 |
|
The integration of the equations of motion is carried out in a |
52 |
|
velocity-Verlet style 2-part algorithm, where $h= \delta t$: |
53 |
|
|
65 |
|
\mathsf{A}(t + h) &\leftarrow \mathrm{rotate}\left( h {\bf j} |
66 |
|
(t + h / 2) \cdot \overleftrightarrow{\mathsf{I}}^{-1} \right). |
67 |
|
\end{align*} |
68 |
– |
|
68 |
|
In this context, the $\mathrm{rotate}$ function is the reversible |
69 |
|
product of the three body-fixed rotations, |
70 |
|
\begin{equation} |
99 |
|
\end{array} |
100 |
|
\right). |
101 |
|
\end{equation} |
102 |
< |
All other rotations follow in a straightforward manner. |
103 |
< |
|
104 |
< |
After the first part of the propagation, the forces and body-fixed |
106 |
< |
torques are calculated at the new positions and orientations |
102 |
> |
All other rotations follow in a straightforward manner. After the |
103 |
> |
first part of the propagation, the forces and body-fixed torques are |
104 |
> |
calculated at the new positions and orientations |
105 |
|
|
106 |
|
{\tt doForces:} |
107 |
|
\begin{align*} |
109 |
|
- \left(\frac{\partial V}{\partial {\bf r}}\right)_{{\bf r}(t + h)}, \\ |
110 |
|
% |
111 |
|
{\bf \tau}^{s}(t + h) &\leftarrow {\bf u}(t + h) |
112 |
< |
\times \frac{\partial V}{\partial {\bf u}}, \\ |
112 |
> |
\times (\frac{\partial V}{\partial {\bf u}})_{u(t+h)}, \\ |
113 |
|
% |
114 |
|
{\bf \tau}^{b}(t + h) &\leftarrow \mathsf{A}(t + h) |
115 |
|
\cdot {\bf \tau}^s(t + h). |
116 |
|
\end{align*} |
117 |
< |
|
120 |
< |
{\sc oopse} automatically updates ${\bf u}$ when the rotation matrix |
117 |
> |
${\bf u}$ is automatically updated when the rotation matrix |
118 |
|
$\mathsf{A}$ is calculated in {\tt moveA}. Once the forces and |
119 |
|
torques have been obtained at the new time step, the velocities can |
120 |
|
be advanced to the same time value. |
129 |
|
\right) |
130 |
|
+ \frac{h}{2} {\bf \tau}^b(t + h) . |
131 |
|
\end{align*} |
135 |
– |
|
132 |
|
The matrix rotations used in the DLM method end up being more costly |
133 |
|
computationally than the simpler arithmetic quaternion propagation. |
134 |
|
With the same time step, a 1000-molecule water simulation shows an |
135 |
|
average 7\% increase in computation time using the DLM method in |
136 |
|
place of quaternions. This cost is more than justified when |
137 |
|
comparing the energy conservation of the two methods as illustrated |
138 |
< |
in Fig.~\ref{methodFig:timestep}. |
138 |
> |
in Fig.~\ref{methodFig:timestep} where the resulting energy drift at |
139 |
> |
various time steps for both the DLM and quaternion integration |
140 |
> |
schemes is compared. All of the 1000 molecule water simulations |
141 |
> |
started with the same configuration, and the only difference was the |
142 |
> |
method for handling rotational motion. At time steps of 0.1 and 0.5 |
143 |
> |
fs, both methods for propagating molecule rotation conserve energy |
144 |
> |
fairly well, with the quaternion method showing a slight energy |
145 |
> |
drift over time in the 0.5 fs time step simulation. At time steps of |
146 |
> |
1 and 2 fs, the energy conservation benefits of the DLM method are |
147 |
> |
clearly demonstrated. Thus, while maintaining the same degree of |
148 |
> |
energy conservation, one can take considerably longer time steps, |
149 |
> |
leading to an overall reduction in computation time. |
150 |
|
|
151 |
|
\begin{figure} |
152 |
|
\centering |
161 |
|
\label{methodFig:timestep} |
162 |
|
\end{figure} |
163 |
|
|
157 |
– |
In Fig.~\ref{methodFig:timestep}, the resulting energy drift at |
158 |
– |
various time steps for both the DLM and quaternion integration |
159 |
– |
schemes is compared. All of the 1000 molecule water simulations |
160 |
– |
started with the same configuration, and the only difference was the |
161 |
– |
method for handling rotational motion. At time steps of 0.1 and 0.5 |
162 |
– |
fs, both methods for propagating molecule rotation conserve energy |
163 |
– |
fairly well, with the quaternion method showing a slight energy |
164 |
– |
drift over time in the 0.5 fs time step simulation. At time steps of |
165 |
– |
1 and 2 fs, the energy conservation benefits of the DLM method are |
166 |
– |
clearly demonstrated. Thus, while maintaining the same degree of |
167 |
– |
energy conservation, one can take considerably longer time steps, |
168 |
– |
leading to an overall reduction in computation time. |
169 |
– |
|
164 |
|
\subsection{\label{methodSection:NVT}Nos\'{e}-Hoover Thermostatting} |
165 |
|
|
166 |
|
The Nos\'e-Hoover equations of motion are given by\cite{Hoover1985} |
174 |
|
rot}\left(\mathsf{A}^{T} \cdot \frac{\partial V}{\partial |
175 |
|
\mathsf{A}} \right) - \chi {\bf j}. \label{eq:nosehoovereom} |
176 |
|
\end{eqnarray} |
183 |
– |
|
177 |
|
$\chi$ is an ``extra'' variable included in the extended system, and |
178 |
|
it is propagated using the first order equation of motion |
179 |
|
\begin{equation} |
180 |
|
\dot{\chi} = \frac{1}{\tau_{T}^2} \left( |
181 |
|
\frac{T}{T_{\mathrm{target}}} - 1 \right). \label{eq:nosehooverext} |
182 |
|
\end{equation} |
190 |
– |
|
183 |
|
The instantaneous temperature $T$ is proportional to the total |
184 |
|
kinetic energy (both translational and orientational) and is given |
185 |
|
by |
186 |
|
\begin{equation} |
187 |
< |
T = \frac{2 K}{f k_B} |
187 |
> |
T = \frac{2 K}{f k_B}. |
188 |
|
\end{equation} |
189 |
|
Here, $f$ is the total number of degrees of freedom in the system, |
190 |
|
\begin{equation} |
191 |
|
f = 3 N + 3 N_{\mathrm{orient}} - N_{\mathrm{constraints}}, |
192 |
|
\end{equation} |
193 |
< |
and $K$ is the total kinetic energy, |
193 |
> |
where $N_{\mathrm{orient}}$ is the number of molecules with |
194 |
> |
orientational degrees of freedom, and $K$ is the total kinetic |
195 |
> |
energy, |
196 |
|
\begin{equation} |
197 |
|
K = \sum_{i=1}^{N} \frac{1}{2} m_i {\bf v}_i^T \cdot {\bf v}_i + |
198 |
|
\sum_{i=1}^{N_{\mathrm{orient}}} \frac{1}{2} {\bf j}_i^T \cdot |
199 |
|
\overleftrightarrow{\mathsf{I}}_i^{-1} \cdot {\bf j}_i. |
200 |
|
\end{equation} |
201 |
+ |
In Eq.~\ref{eq:nosehooverext}, $\tau_T$ is the time constant for |
202 |
+ |
relaxation of the temperature to the target value. The integration |
203 |
+ |
of the equations of motion is carried out in a velocity-Verlet style |
204 |
+ |
2 part algorithm: |
205 |
|
|
208 |
– |
In eq.(\ref{eq:nosehooverext}), $\tau_T$ is the time constant for |
209 |
– |
relaxation of the temperature to the target value. To set values |
210 |
– |
for $\tau_T$ or $T_{\mathrm{target}}$ in a simulation, one would use |
211 |
– |
the {\tt tauThermostat} and {\tt targetTemperature} keywords in the |
212 |
– |
{\tt .bass} file. The units for {\tt tauThermostat} are fs, and the |
213 |
– |
units for the {\tt targetTemperature} are degrees K. The |
214 |
– |
integration of the equations of motion is carried out in a |
215 |
– |
velocity-Verlet style 2 part algorithm: |
216 |
– |
|
206 |
|
{\tt moveA:} |
207 |
|
\begin{align*} |
208 |
|
T(t) &\leftarrow \left\{{\bf v}(t)\right\}, \left\{{\bf j}(t)\right\} ,\\ |
226 |
|
+ \frac{h}{2 \tau_T^2} \left( \frac{T(t)} |
227 |
|
{T_{\mathrm{target}}} - 1 \right) . |
228 |
|
\end{align*} |
240 |
– |
|
229 |
|
Here $\mathrm{rotate}(h * {\bf j} |
230 |
|
\overleftrightarrow{\mathsf{I}}^{-1})$ is the same symplectic |
231 |
|
Trotter factorization of the three rotation operations that was |
236 |
|
step. The new positions (and orientations) are then used to |
237 |
|
calculate a new set of forces and torques in exactly the same way |
238 |
|
they are calculated in the {\tt doForces} portion of the DLM |
239 |
< |
integrator. |
239 |
> |
integrator. Once the forces and torques have been obtained at the |
240 |
> |
new time step, the temperature, velocities, and the extended system |
241 |
> |
variable can be advanced to the same time value. |
242 |
|
|
253 |
– |
Once the forces and torques have been obtained at the new time step, |
254 |
– |
the temperature, velocities, and the extended system variable can be |
255 |
– |
advanced to the same time value. |
256 |
– |
|
243 |
|
{\tt moveB:} |
244 |
|
\begin{align*} |
245 |
|
T(t + h) &\leftarrow \left\{{\bf v}(t + h)\right\}, |
259 |
|
\left( {\bf \tau}^b(t + h) - {\bf j}(t + h) |
260 |
|
\chi(t + h) \right) . |
261 |
|
\end{align*} |
276 |
– |
|
262 |
|
Since ${\bf v}(t + h)$ and ${\bf j}(t + h)$ are required to |
263 |
|
caclculate $T(t + h)$ as well as $\chi(t + h)$, they indirectly |
264 |
|
depend on their own values at time $t + h$. {\tt moveB} is |
265 |
|
therefore done in an iterative fashion until $\chi(t + h)$ becomes |
266 |
< |
self-consistent. The relative tolerance for the self-consistency |
267 |
< |
check defaults to a value of $\mbox{10}^{-6}$, but {\sc oopse} will |
268 |
< |
terminate the iteration after 4 loops even if the consistency check |
284 |
< |
has not been satisfied. |
285 |
< |
|
286 |
< |
The Nos\'e-Hoover algorithm is known to conserve a Hamiltonian for |
287 |
< |
the extended system that is, to within a constant, identical to the |
288 |
< |
Helmholtz free energy,\cite{Melchionna1993} |
266 |
> |
self-consistent. The Nos\'e-Hoover algorithm is known to conserve a |
267 |
> |
Hamiltonian for the extended system that is, to within a constant, |
268 |
> |
identical to the Helmholtz free energy,\cite{Melchionna1993} |
269 |
|
\begin{equation} |
270 |
|
H_{\mathrm{NVT}} = V + K + f k_B T_{\mathrm{target}} \left( |
271 |
|
\frac{\tau_{T}^2 \chi^2(t)}{2} + \int_{0}^{t} \chi(t^\prime) |
277 |
|
of the integration. |
278 |
|
|
279 |
|
\subsection{\label{methodSection:NPTi}Constant-pressure integration with |
280 |
< |
isotropic box deformations (NPTi)} |
280 |
> |
isotropic box (NPTi)} |
281 |
|
|
282 |
< |
To carry out isobaric-isothermal ensemble calculations {\sc oopse} |
283 |
< |
implements the Melchionna modifications to the |
284 |
< |
Nos\'e-Hoover-Andersen equations of motion,\cite{Melchionna1993} |
305 |
< |
|
282 |
> |
We can used an isobaric-isothermal ensemble integrator which is |
283 |
> |
implemented using the Melchionna modifications to the |
284 |
> |
Nos\'e-Hoover-Andersen equations of motion\cite{Melchionna1993} |
285 |
|
\begin{eqnarray} |
286 |
|
\dot{{\bf r}} & = & {\bf v} + \eta \left( {\bf r} - {\bf R}_0 \right), \\ |
287 |
|
\dot{{\bf v}} & = & \frac{{\bf f}}{m} - (\eta + \chi) {\bf v}, \\ |
298 |
|
P_{\mathrm{target}} \right), \\ |
299 |
|
\dot{\mathcal{V}} & = & 3 \mathcal{V} \eta . \label{eq:melchionna1} |
300 |
|
\end{eqnarray} |
322 |
– |
|
301 |
|
$\chi$ and $\eta$ are the ``extra'' degrees of freedom in the |
302 |
|
extended system. $\chi$ is a thermostat, and it has the same |
303 |
|
function as it does in the Nos\'e-Hoover NVT integrator. $\eta$ is |
330 |
|
the Pressure tensor, |
331 |
|
\begin{equation} |
332 |
|
P(t) = \frac{1}{3} \mathrm{Tr} \left( |
333 |
< |
\overleftrightarrow{\mathsf{P}}(t). \right) |
333 |
> |
\overleftrightarrow{\mathsf{P}}(t) \right) . |
334 |
|
\end{equation} |
335 |
< |
|
358 |
< |
In eq.(\ref{eq:melchionna1}), $\tau_B$ is the time constant for |
335 |
> |
In Eq.~\ref{eq:melchionna1}, $\tau_B$ is the time constant for |
336 |
|
relaxation of the pressure to the target value. Like in the NVT |
337 |
|
integrator, the integration of the equations of motion is carried |
338 |
|
out in a velocity-Verlet style 2 part algorithm: |
371 |
|
\mathsf{H}(t + h) &\leftarrow e^{-h \eta(t + h / 2)} |
372 |
|
\mathsf{H}(t). |
373 |
|
\end{align*} |
397 |
– |
|
374 |
|
Most of these equations are identical to their counterparts in the |
375 |
|
NVT integrator, but the propagation of positions to time $t + h$ |
376 |
< |
depends on the positions at the same time. {\sc oopse} carries out |
377 |
< |
this step iteratively (with a limit of 5 passes through the |
378 |
< |
iterative loop). Also, the simulation box $\mathsf{H}$ is scaled |
379 |
< |
uniformly for one full time step by an exponential factor that |
380 |
< |
depends on the value of $\eta$ at time $t + h / 2$. Reshaping the |
405 |
< |
box uniformly also scales the volume of the box by |
376 |
> |
depends on the positions at the same time. The simulation box |
377 |
> |
$\mathsf{H}$ is scaled uniformly for one full time step by an |
378 |
> |
exponential factor that depends on the value of $\eta$ at time $t + |
379 |
> |
h / 2$. Reshaping the box uniformly also scales the volume of the |
380 |
> |
box by |
381 |
|
\begin{equation} |
382 |
|
\mathcal{V}(t + h) \leftarrow e^{ - 3 h \eta(t + h /2)}. |
383 |
|
\mathcal{V}(t) |
384 |
|
\end{equation} |
410 |
– |
|
385 |
|
The {\tt doForces} step for the NPTi integrator is exactly the same |
386 |
|
as in both the DLM and NVT integrators. Once the forces and torques |
387 |
|
have been obtained at the new time step, the velocities can be |
413 |
|
\tau}^b(t + h) - {\bf j}(t + h) |
414 |
|
\chi(t + h) \right) . |
415 |
|
\end{align*} |
442 |
– |
|
416 |
|
Once again, since ${\bf v}(t + h)$ and ${\bf j}(t + h)$ are required |
417 |
|
to caclculate $T(t + h)$, $P(t + h)$, $\chi(t + h)$, and $\eta(t + |
418 |
|
h)$, they indirectly depend on their own values at time $t + h$. |
419 |
|
{\tt moveB} is therefore done in an iterative fashion until $\chi(t |
420 |
< |
+ h)$ and $\eta(t + h)$ become self-consistent. The relative |
448 |
< |
tolerance for the self-consistency check defaults to a value of |
449 |
< |
$\mbox{10}^{-6}$, but {\sc oopse} will terminate the iteration after |
450 |
< |
4 loops even if the consistency check has not been satisfied. |
420 |
> |
+ h)$ and $\eta(t + h)$ become self-consistent. |
421 |
|
|
422 |
|
The Melchionna modification of the Nos\'e-Hoover-Andersen algorithm |
423 |
|
is known to conserve a Hamiltonian for the extended system that is, |
512 |
|
\mathsf{H}(t + h) &\leftarrow \mathsf{H}(t) \cdot e^{-h |
513 |
|
\overleftrightarrow{\eta}(t + h / 2)} . |
514 |
|
\end{align*} |
515 |
< |
{\sc oopse} uses a power series expansion truncated at second order |
516 |
< |
for the exponential operation which scales the simulation box. |
515 |
> |
Here, a power series expansion truncated at second order for the |
516 |
> |
exponential operation is used to scale the simulation box. The {\tt |
517 |
> |
moveB} portion of the algorithm is largely unchanged from the NPTi |
518 |
> |
integrator: |
519 |
|
|
548 |
– |
The {\tt moveB} portion of the algorithm is largely unchanged from |
549 |
– |
the NPTi integrator: |
550 |
– |
|
520 |
|
{\tt moveB:} |
521 |
|
\begin{align*} |
522 |
|
T(t + h) &\leftarrow \left\{{\bf v}(t + h)\right\}, |
546 |
|
+ h / 2 \right) + \frac{h}{2} \left( {\bf \tau}^b(t |
547 |
|
+ h) - {\bf j}(t + h) \chi(t + h) \right) . |
548 |
|
\end{align*} |
580 |
– |
|
549 |
|
The iterative schemes for both {\tt moveA} and {\tt moveB} are |
550 |
< |
identical to those described for the NPTi integrator. |
551 |
< |
|
552 |
< |
The NPTf integrator is known to conserve the following Hamiltonian: |
553 |
< |
\begin{equation} |
586 |
< |
H_{\mathrm{NPTf}} = V + K + f k_B T_{\mathrm{target}} \left( |
550 |
> |
identical to those described for the NPTi integrator. The NPTf |
551 |
> |
integrator is known to conserve the following Hamiltonian: |
552 |
> |
\begin{eqnarray*} |
553 |
> |
H_{\mathrm{NPTf}} & = & V + K + f k_B T_{\mathrm{target}} \left( |
554 |
|
\frac{\tau_{T}^2 \chi^2(t)}{2} + \int_{0}^{t} \chi(t^\prime) |
555 |
< |
dt^\prime \right) + P_{\mathrm{target}} \mathcal{V}(t) + \frac{f k_B |
555 |
> |
dt^\prime \right) \\ |
556 |
> |
& & + P_{\mathrm{target}} \mathcal{V}(t) + \frac{f k_B |
557 |
|
T_{\mathrm{target}}}{2} |
558 |
|
\mathrm{Tr}\left[\overleftrightarrow{\eta}(t)\right]^2 \tau_B^2. |
559 |
< |
\end{equation} |
592 |
< |
|
559 |
> |
\end{eqnarray*} |
560 |
|
This integrator must be used with care, particularly in liquid |
561 |
|
simulations. Liquids have very small restoring forces in the |
562 |
|
off-diagonal directions, and the simulation box can very quickly |
565 |
|
finds most use in simulating crystals or liquid crystals which |
566 |
|
assume non-orthorhombic geometries. |
567 |
|
|
568 |
< |
\subsection{\label{methodSection:otherSpecialEnsembles}Other Special Ensembles} |
568 |
> |
\subsection{\label{methodSection:NPAT}NPAT Ensemble} |
569 |
|
|
570 |
< |
\subsubsection{\label{methodSection:NPAT}\textbf{NPAT Ensemble}} |
570 |
> |
A comprehensive understanding of relations between structures and |
571 |
> |
functions in biological membrane system ultimately relies on |
572 |
> |
structure and dynamics of lipid bilayers, which are strongly |
573 |
> |
affected by the interfacial interaction between lipid molecules and |
574 |
> |
surrounding media. One quantity to describe the interfacial |
575 |
> |
interaction is so called the average surface area per lipid. |
576 |
> |
Constant area and constant lateral pressure simulations can be |
577 |
> |
achieved by extending the standard NPT ensemble with a different |
578 |
> |
pressure control strategy |
579 |
|
|
605 |
– |
A comprehensive understanding of structure¨Cfunction relations of |
606 |
– |
biological membrane system ultimately relies on structure and |
607 |
– |
dynamics of lipid bilayer, which are strongly affected by the |
608 |
– |
interfacial interaction between lipid molecules and surrounding |
609 |
– |
media. One quantity to describe the interfacial interaction is so |
610 |
– |
called the average surface area per lipid. Constat area and constant |
611 |
– |
lateral pressure simulation can be achieved by extending the |
612 |
– |
standard NPT ensemble with a different pressure control strategy |
613 |
– |
|
580 |
|
\begin{equation} |
581 |
|
\dot {\overleftrightarrow{\eta}} _{\alpha \beta}=\left\{\begin{array}{ll} |
582 |
|
\frac{{V(P_{\alpha \beta } - P_{{\rm{target}}} )}}{{\tau_{\rm{B}}^{\rm{2}} fk_B T_{{\rm{target}}} }} |
589 |
|
Note that the iterative schemes for NPAT are identical to those |
590 |
|
described for the NPTi integrator. |
591 |
|
|
592 |
< |
\subsubsection{\label{methodSection:NPrT}\textbf{NP$\gamma$T Ensemble}} |
592 |
> |
\subsection{\label{methodSection:NPrT}NP$\gamma$T |
593 |
> |
Ensemble} |
594 |
|
|
595 |
|
Theoretically, the surface tension $\gamma$ of a stress free |
596 |
|
membrane system should be zero since its surface free energy $G$ is |
597 |
< |
minimum with respect to surface area $A$ |
598 |
< |
\[ |
599 |
< |
\gamma = \frac{{\partial G}}{{\partial A}}. |
600 |
< |
\] |
601 |
< |
However, a surface tension of zero is not appropriate for relatively |
602 |
< |
small patches of membrane. In order to eliminate the edge effect of |
603 |
< |
the membrane simulation, a special ensemble, NP$\gamma$T, is |
637 |
< |
proposed to maintain the lateral surface tension and normal |
638 |
< |
pressure. The equation of motion for cell size control tensor, |
639 |
< |
$\eta$, in $NP\gamma T$ is |
597 |
> |
minimum with respect to surface area $A$, $\gamma = \frac{{\partial |
598 |
> |
G}}{{\partial A}}.$ However, a surface tension of zero is not |
599 |
> |
appropriate for relatively small patches of membrane. In order to |
600 |
> |
eliminate the edge effect of the membrane simulation, a special |
601 |
> |
ensemble, NP$\gamma$T, has been proposed to maintain the lateral |
602 |
> |
surface tension and normal pressure. The equation of motion for the |
603 |
> |
cell size control tensor, $\eta$, in $NP\gamma T$ is |
604 |
|
\begin{equation} |
605 |
|
\dot {\overleftrightarrow{\eta}} _{\alpha \beta}=\left\{\begin{array}{ll} |
606 |
|
- A_{xy} (\gamma _\alpha - \gamma _{{\rm{target}}} ) & \mbox{$\alpha = \beta = x$ or $\alpha = \beta = y$}\\ |
616 |
|
- P_{{\rm{target}}} ) |
617 |
|
\label{methodEquation:instantaneousSurfaceTensor} |
618 |
|
\end{equation} |
655 |
– |
|
619 |
|
There is one additional extended system integrator (NPTxyz), in |
620 |
|
which each attempt to preserve the target pressure along the box |
621 |
|
walls perpendicular to that particular axis. The lengths of the box |
622 |
|
axes are allowed to fluctuate independently, but the angle between |
623 |
|
the box axes does not change. It should be noted that the NPTxyz |
624 |
|
integrator is a special case of $NP\gamma T$ if the surface tension |
625 |
< |
$\gamma$ is set to zero. |
625 |
> |
$\gamma$ is set to zero, and if $x$ and $y$ can move independently. |
626 |
|
|
627 |
< |
\section{\label{methodSection:zcons}Z-Constraint Method} |
627 |
> |
\section{\label{methodSection:zcons}The Z-Constraint Method} |
628 |
|
|
629 |
|
Based on the fluctuation-dissipation theorem, a force |
630 |
|
auto-correlation method was developed by Roux and Karplus to |
638 |
|
\begin{equation} |
639 |
|
\delta F(z,t)=F(z,t)-\langle F(z,t)\rangle. |
640 |
|
\end{equation} |
678 |
– |
|
641 |
|
If the time-dependent friction decays rapidly, the static friction |
642 |
|
coefficient can be approximated by |
643 |
|
\begin{equation} |
650 |
|
D(z)=\frac{k_{B}T}{\xi_{\text{static}}(z)}=\frac{(k_{B}T)^{2}}{\int_{0}^{\infty |
651 |
|
}\langle\delta F(z,t)\delta F(z,0)\rangle dt}.% |
652 |
|
\end{equation} |
691 |
– |
|
653 |
|
The Z-Constraint method, which fixes the z coordinates of the |
654 |
|
molecules with respect to the center of the mass of the system, has |
655 |
|
been a method suggested to obtain the forces required for the force |
658 |
|
whole system. To avoid this problem, we reset the forces of |
659 |
|
z-constrained molecules as well as subtract the total constraint |
660 |
|
forces from the rest of the system after the force calculation at |
661 |
< |
each time step instead of resetting the coordinate. |
662 |
< |
|
702 |
< |
After the force calculation, define $G_\alpha$ as |
661 |
> |
each time step instead of resetting the coordinate. After the force |
662 |
> |
calculation, we define $G_\alpha$ as |
663 |
|
\begin{equation} |
664 |
|
G_{\alpha} = \sum_i F_{\alpha i}, \label{oopseEq:zc1} |
665 |
|
\end{equation} |
694 |
|
v_{\beta i} = v_{\beta i} + \sum_{\alpha} |
695 |
|
\frac{\sum_i m_{\alpha i} v_{\alpha i}}{\sum_i m_{\alpha i}}. |
696 |
|
\end{equation} |
737 |
– |
|
697 |
|
At the very beginning of the simulation, the molecules may not be at |
698 |
|
their constrained positions. To move a z-constrained molecule to its |
699 |
|
specified position, a simple harmonic potential is used |