402
Figure 1. Grid points of DP to calculate minimum fuel route.
The propeller revolution number is determined so
as to reach the destination point at the desired time
of arrival. We will look for the minimum propeller
revolution number that will allow us to reach the
destination at the desired time of arrival, by doing so
we will find the most practical minimum fuel route
for the desired voyage time.
Ship’s position can be described by the following
equation:
(1)
Where t is the time, x the position of the ship, S the
speed and C the control parameter, which in our case
is dependent only on rudder angle since the propeller
revolution number in kept constant.
The speed of the ship at any instant is function of
ship’s heading and response to the external weather
elements, such as wave, wind and current.
),,,( currentwindwavefS
θ
=
(2)
Knowing the weather elements we can determine the
speed of the ship, and knowing this later allows us to
compute the time needed to travel from one node to
another.
Let the i-th node on the k-th vertex line from P
0
be G(k, i). The ship starts from G(k, i) at time t
k
and
reaches the node G(k-1, j) on the k-1-th vertex line at
time t
k-1
(see fig.1 for more details).
The minimum time route from the departure point
P
0
to the destination Ps is obtained by solving the
following iterative equation:
( )( ) ( ) ( )( ) ( )( ){ }
jkGTikGjkGTMinikGT
j
,1,,,1,
minmin
−+−=
(3)
(k=1,2,…,N+1)
where T
min
(G(k, i)) represents the minimum passage
time from the departure P
0
to the node G(k, i), and
T(G(k-1, j), G(k, i)) represents the passage time from
the previous node G(k-1, j) to the node G(k, i).
Eq.3 means than the minimum passage time from
departure point P
0
to any point G(k, i) can be deter-
mined by finding the minimum of the sum of pas-
sage time from G(k-1, j) to G(k, i) and the minimum
passage time from departure point P
0
to G(k-1, j)
(when k reaches N+1, G(N+1) is Ps ).
If the T
min
obtained by solving (3) is not equal to
the desired voyage time the propeller revolution
number is changed and (3) resolved, we will gradu-
ally adjust the propeller revolution number until we
get a T
min
as close as possible to the desired voyage
time.
The route thus obtained can be considered as the
minimum fuel route for the specified voyage time.
Here after we will refer to this route as MFR.
The MFR obtained by this method is not the true
minimum fuel route from the mathematical point of
view, but it can be regarded as the sub-optimal route
that will allow us to reach destination at the desired
time with a minimum consumption and a fixed pro-
peller revolution number. In this method since the
only control parameter is the ship’s course the
amount of calculation is largely reduced
3 ENVIRONMENTAL DATA
The environmental data used for carrying simulation
with this calculation method are forecasted data of
surface winds, waves, ocean and tidal currents, these
data were used to calculate the ship’s speed trough
the water and over the ground. The forecast data are
available for each 1 hour, extending for a period of
72 hours, the forecast data are updated 8 times a day
(i.e. base time of forecast: 00,03,06,09,12,15,18,21
UTC).
3.1 Wind and wave data
The wind data comprises mean wind direction and
mean wind speed; the wave data comprises the sig-
nificant wave height, predominant wave direction
and significant wave period.
For the forecast period up to 15 hours ahead the
forecasted data are the result of the input of the sur-
face winds from the mesoscale numerical forecast
model of the Japan Meteorological Agency into the
3
rd
generation wave forecast model “WAM” of the
Japan Weather Association, the data are given for
grids of 2 by 2 miles .
For the forecast period from 16 to 72 hours
ahead, the data are from the output of the wave fore-
cast model of the Japan Meteorological Agency, the
data are given for grids of 6 by 6 miles.