∂u
∂t
= d
u
∆u − kd
dyn
u + k
−
v, in Ω,
∂v
∂t
= d
v
∆v + kd
dyn
u − k
−
v − k
1
v
IxJ
+ k
−1
w
IxJ
|J|
+ c(δ
x
Fi
− δ
x
In
)w
IxJ
|J|
, in Ω,
∂w
∂t
+ c
∂w
∂x
= −k
−1
w + k
1
R
J
vdy, in ]x
In
,x
Fi
[,
(1)
velocity for the transported particle. Dynein concen-
tration is supposed to be constant and is denoted by
[D] = d
dyn
.
Under the previous assumptions the u and v
species satisfy a reaction-diffusion equation, while w
is controlled by a convection equation modeling the
transport along the microtubule with a steady veloc-
ity c. The model we get is equation 1, where δ
x
0
in the equation for v stands for the Dirac mass in
x
0
= x
In
,x
Fi
. The term c(δ
x
Fi
− δ
x
In
)w
IxJ
represents
the contribution due to the outgoing flux of the trans-
ported particles at the end of the MT filament and it
guarantees conservation of the mass. We also impose
the boundary conditions:
∂u
∂n
= 0,
∂v
∂n
= 0, on Γ
4
,
d
u
∂u
∂n
+ p
u
u = 0, d
v
∂v
∂n
+ p
v
v = 0, on Γ
2
,
w(x
In
) = 0.
As said before, the boundary conditions on Γ
1
and Γ
3
for u and v are periodic, i.e. we suppose that for every
t u|
Γ
1
= u|
Γ
3
, respectively v (see figure 2). We as-
sume that proteins cannot cross the membrane layer
on Γ
4
using a Neumann homogeneous boundary con-
dition, but we suppose that on Γ
2
there is an outgoing
flow proportional to the species concentration. For
the transported cargo we suppose that there is not an
upcoming flux at the beginning of the microtubule.
We remark that the two first equations lie in a two
dimensional domain: u = u(x,y,t) and v = v(x,y,t)
represent the species concentration per unit volume
at time t in (x, y) ∈ Ω. The equation for w is one
dimensional and the cargo concentration can move
only in one direction along the filament, positioned
at [x
In
,x
Fi
] × {y
0
} ⊂ Ω.
In our model, to point out the difference in the type
of transport mechanisms, we consider the MT depen-
dent transport to be 1D and describe diffusion as a bi-
dimensional event. With this approach we couple the
two mechanisms considered and model them at two
different levels. In this way we get an interconnected
system that relies on the two processes but empha-
sizes the features of each type of transport.
A concentration gradient that allows diffusion in
the whole domain, and active transport directed to-
wards the nucleus and localized near the microtubule.
3 SCHEME
In this section we will propose a numerical scheme in
order to solve the system presented above.
Let us introduce a space discretization of the x and
y axis. Our domain Ω is the rectangle [0,L
x
] × [0, L
y
]
(fig: 1). We denote by ∆x, ∆y the discretization steps
in the x and y directions respectively and we divide
the intervals [0,L
x
] and [0, L
y
] in N
x
+ 1 and N
y
+ 1
points. The mesh points will be (x
i
,y
j
) = (i∆x, j∆y)
with 0 ≤ i ≤ N
x
+1, 0 ≤ j ≤ N
y
+1. Let ∆t be the time
discretization step and t
n
the n
th
step, i.e. t
n
= n∆t,
n ∈ N. According to these notations u
n
i, j
will be the
approximation of the solution of u in (x
i
,y
j
) at time
t
n
and respectively v
n
i, j
and w
n
i
denote the approxima-
tions of v and w. We remark that w lies in [x
In
,x
Fi
]
so w
n
i
is well defined only for certain values of i, in
particular we need x
In
/∆x ≤ i≤ x
Fi
/∆x.
We first solve the third equation of the system. We
discretize the transport contribution by using an up-
wind scheme enhanced by a TDV flux limiter (Sweby,
1984). The right hand side is made by two parts. The
term −k
−1
w is stiff, and it will be approximated by
an implicit discretization. For the other source term
F :=
R
J
v(x
i
,y)dy
|J|
, we used an upwinding scheme (Roe,
1981), which improve the resolution near the asymp-
totic states, and besides, we approximated the integral
using a trapezoidal rule. Summing up these consid-
erations, we obtain a scheme for w (equation 2). In
this equation ν = c
∆t
∆x
and we put r
i+1/2
=
w
n
i−1
−w
n
i−2
w
n
i
−w
n
i−1
and r
i−1/2
=
w
n
i+1
−w
n
i
w
n
i
−w
n
i−1
, while φ is a flux limiter func-
tion (minmod in our simulations, see again (Sweeby,
1984)).
We use a IMEX midpoint scheme (Briani et al.,
2007), to solve numerically the reaction-diffusion
system (see equations: 3, 4), where
δ
2
x
u
(1)
∆x
2
=
u
(1)
i+1, j
− 2u
(1)
i, j
+ u
(1)
i−1, j
∆x
2
and
motor velocity for the transported particle. Dynein
concentration is supposed to be constant and is de-
noted by [D] = d
dyn
.
Under the previous assumptions the u and v
species satisfy a reaction-diffusion equation, while w
is controlled by a convection equation modeling the
transport along the microtubule with a steady veloc-
ity c. The model we get is equation 1, where δ
x
0
in the equation for v stands for the Dirac mass in
x
0
= x
In
,x
Fi
. The term c(δ
x
Fi
− δ
x
In
)w
IxJ
represents
the contribution due to the outgoing flux of the trans-
ported particles at the end of the MT filament and it
guarantees conservation of the mass. We also impose
the boundary conditions:
∂u
∂n
= 0,
∂v
∂n
= 0, on Γ
4
,
d
u
∂u
∂n
+ p
u
u = 0, d
v
∂v
∂n
+ p
v
v = 0, on Γ
2
,
w(x
In
) = 0.
As said before, the boundary conditions on Γ
1
and Γ
3
for u and v are periodic, i.e. we suppose that for every
t u|
Γ
1
= u|
Γ
3
, respectively v (see figure 2). We as-
sume that proteins cannot cross the membrane layer
on Γ
4
using a Neumann homogeneous boundary con-
dition, but we suppose that on Γ
2
there is an outgoing
flow proportional to the species concentration. For
the transported cargo we suppose that there is not an
upcoming flux at the beginning of the microtubule.
We remark that the two first equations lie in a two
dimensional domain: u = u(x,y,t) and v = v(x,y,t)
represent the species concentration per unit volume
at time t in (x,y) ∈ Ω. The equation for w is one
dimensional and the cargo concentration can move
only in one direction along the filament, positioned
at [x
In
,x
Fi
] × {y
0
} ⊂ Ω.
In our model, to point out the difference in the type
of transport mechanisms, we consider the MT depen-
dent transport to be 1D and describe diffusion as a bi-
dimensional event. With this approach we couple the
two mechanisms considered and model them at two
different levels. In this way we get an interconnected
system that relies on the two processes but empha-
sizes the features of each type of transport.
A concentration gradient that allows diffusion in
the whole domain, and active transport directed to-
wards the nucleus and localized near the microtubule.
3 SCHEME
In this section we will propose a numerical scheme in
order to solve the system presented above.
Let us introduce a space discretization of the x and
y axis. Our domain Ω is the rectangle [0,L
x
] × [0, L
y
]
(fig: 1). We denote by ∆x, ∆y the discretization steps
in the x and y directions respectively and we divide
the intervals [0, L
x
] and [0, L
y
] in N
x
+ 1 and N
y
+ 1
points. The mesh points will be (x
i
,y
j
) = (i∆x, j∆y)
with 0 ≤ i ≤ N
x
+1, 0 ≤ j ≤ N
y
+1. Let ∆t be the time
discretization step and t
n
the n
th
step, i.e. t
n
= n∆t,
n ∈ N. According to these notations u
n
i, j
will be the
approximation of the solution of u in (x
i
,y
j
) at time
t
n
and respectively v
n
i, j
and w
n
i
denote the approxima-
tions of v and w. We remark that w lies in [x
In
,x
Fi
]
so w
n
i
is well defined only for certain values of i, in
particular we need x
In
/∆x ≤ i≤ x
Fi
/∆x.
We first solve the third equation of the system. We
discretize the transport contribution by using an up-
wind scheme enhanced by a TDV flux limiter (Sweby,
1984). The right hand side is made by two parts. The
term −k
−1
w is stiff, and it will be approximated by
an implicit discretization. For the other source term
F :=
R
J
v(x
i
,y)dy
|J|
, we used an upwinding scheme (Roe,
1981), which improve the resolution near the asymp-
totic states, and besides, we approximated the integral
using a trapezoidal rule. Summing up these consid-
erations, we obtain a scheme for w (equation 2). In
this equation ν = c
∆t
∆x
and we put r
i+1/2
=
w
n
i−1
−w
n
i−2
w
n
i
−w
n
i−1
and r
i−1/2
=
w
n
i+1
−w
n
i
w
n
i
−w
n
i−1
, while φ is a flux limiter func-
tion (minmod in our simulations, see again (Sweeby,
1984)).
We use a IMEX midpoint scheme (Briani et al.,
2007), to solve numerically the reaction-diffusion
system (see equations: 3, 4), where
δ
2
x
u
(1)
∆x
2
=
u
(1)
i+1, j
− 2u
(1)
i, j
+ u
(1)
i−1, j
∆x
2
and
BIOINFORMATICS 2011 - International Conference on Bioinformatics Models, Methods and Algorithms
42