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# Line 635 | Line 635 | a \emph{symplectic} flow if it satisfies,
635   Let $\varphi$ be the flow of Hamiltonian vector field, $\varphi$ is
636   a \emph{symplectic} flow if it satisfies,
637   \begin{equation}
638 < '\varphi^T J '\varphi = J.
638 > {\varphi '}^T J \varphi ' = J.
639   \end{equation}
640   According to Liouville's theorem, the symplectic volume is invariant
641   under a Hamiltonian flow, which is the basis for classical
# Line 643 | Line 643 | symplectomorphism. As to the Poisson system,
643   field on a symplectic manifold can be shown to be a
644   symplectomorphism. As to the Poisson system,
645   \begin{equation}
646 < '\varphi ^T J '\varphi  = J \circ \varphi
646 > {\varphi '}^T J \varphi ' = J \circ \varphi
647   \end{equation}
648   is the property must be preserved by the integrator.
649  
# Line 685 | Line 685 | instability \cite{}. However, due to computational pen
685   ordinary implicit Runge-Kutta methods are not suitable for
686   Hamiltonian system. Recently, various high-order explicit
687   Runge--Kutta methods have been developed to overcome this
688 < instability \cite{}. However, due to computational penalty involved
689 < in implementing the Runge-Kutta methods, they do not attract too
690 < much attention from Molecular Dynamics community. Instead, splitting
691 < have been widely accepted since they exploit natural decompositions
692 < of the system\cite{Tuckerman92}.
688 > instability. However, due to computational penalty involved in
689 > implementing the Runge-Kutta methods, they do not attract too much
690 > attention from Molecular Dynamics community. Instead, splitting have
691 > been widely accepted since they exploit natural decompositions of
692 > the system\cite{Tuckerman92}.
693  
694   \subsubsection{\label{introSection:splittingMethod}Splitting Method}
695  
# Line 744 | Line 744 | symmetric property,
744   symmetric property,
745   \begin{equation}
746   \varphi _h^{ - 1} = \varphi _{ - h}.
747 < \lable{introEquation:timeReversible}
747 > \label{introEquation:timeReversible}
748   \end{equation}
749  
750   \subsubsection{\label{introSection:exampleSplittingMethod}Example of Splitting Method}
# Line 802 | Line 802 | q(\Delta t) = q(0) + \frac{{\Delta t}}{2}\left[ {\dot
802   \frac{{\Delta t}}{{2m}}\dot q(0)} \right], %
803   \label{introEquation:positionVerlet1} \\%
804   %
805 < q(\Delta t) = q(0) + \frac{{\Delta t}}{2}\left[ {\dot q(0) + \dot
805 > q(\Delta t) &= q(0) + \frac{{\Delta t}}{2}\left[ {\dot q(0) + \dot
806   q(\Delta t)} \right]. %
807   \label{introEquation:positionVerlet1}
808   \end{align}
# Line 828 | Line 828 | can obtain
828   \]
829   Applying Baker-Campbell-Hausdorff formula to Sprang splitting, we
830   can obtain
831 < \begin{eqnarray}
831 > \begin{eqnarray*}
832   \exp (h X/2)\exp (h Y)\exp (h X/2) & = & \exp (h X + h Y + h^2
833 < [X,Y]/4 + h^2 [Y,X]/4 \\ & & \mbox{} + h^2 [X,X]/8 + h^2 [Y,Y]/8 +
834 < h^3 [Y,[Y,X]]/12 - h^3 [X,[X,Y]]/24 +  \ldots )
835 < \end{eqnarray}
833 > [X,Y]/4 + h^2 [Y,X]/4 \\ & & \mbox{} + h^2 [X,X]/8 + h^2 [Y,Y]/8 \\
834 > & & \mbox{} + h^3 [Y,[Y,X]]/12 - h^3 [X,[X,Y]]/24 & & \mbox{} +
835 > \ldots )
836 > \end{eqnarray*}
837   Since \[ [X,Y] + [Y,X] = 0\] and \[ [X,X] = 0\], the dominant local
838   error of Spring splitting is proportional to $h^3$. The same
839   procedure can be applied to general splitting,  of the form

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