
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.