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Fig. 14.5 Situation 2
A, .50
D
B, .25
C, .75
Fig. 14.6 Situation 3
A, .25
D, .50
B, .25
C, .25
Table 14.3 Computational results
Sit./Par.
a
b
c
1
1
1
0
2
1.6498
2.3324
1.9342
3
5.2245
15.6735
0
From the centre of gravity (coordinates x*, y*) one computes for each dimension
k :u k ¼
x*) 2 ,v k ¼
y*) 2 ,z k ¼
(x k
(y k
(x k
x*) (y k
y *); let
u, v, z,
be the
column vectors of those magnitudes, and
X ¼ [u, v, z]
the resulting matrix. One
then constructs
X'X
,a3
3 matrix, and defines a column vector
e
of three
coefficients a, b, c , from which the following program is derived:
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