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                    <text>Item D Number

02374

Author

Belli, G.

Corporate Author
Report/Article Title

Typescript: Statistical Interpolation Model for the
Description of Ground Pollution Due to the TCDD
Produced in the 1976 Chemical Accident at Seveso in
the Heavily Contaminated Zone "A"

Journal/Book Title
Year

1983

Month/Day

November

Color

D

Number of Images

45

Descrtyton Notes

Friday, October 05, 2001

Page 2374 of 2422

�STATISTICAL INTERPOLATION MODEL FOR THE
DESCRIPTION OF GROUND POLLUTION DUE TO
THE TCDD PRODUCED IN THE 1976 CHEMICAL
ACCIDENT AT SEVESO IN THE HEAVILY
CONTAMINATED ZONE "A".
G.Belli

,S.Cerlesi
(3 4)
S.Ratti ' .

,E.Milan!

1) Regione Lombardia - Ufficio Speciale Seveso

and

(Mi)

2) Istituto Tecnico Industrials Pavia
3) Istituto di Pisica Nucleare Universita Pavia
4) Istituto Nazionale di Pisica Nucleare Sezione Pavia

Novembre 1983

IFNUP/RL

14/83

�INDEX
1. INTRODUCTION
2. DEFINITION OF THE DATA SAMPLE
3. THEORY OF THE MATHEMATICAL METHOD
3.1 Introduction
3.2 Approximation of an arbitrary function
by means of a set of given functions
3.3 Conditions on the coefficients a,
3.4 Choice of the functions p^Cx)
3.5 Legendre Functions and Tchebychev
Functions
3.6

Multidimensional parametrization

Pag.

1

"

1

"

4

"
"
"

5
6
8

"

10

"

13

"

14

"
"
"

15
17
19

"
"
"
"

26
26
31
33

"

39

"

40

4. PSEUDOMEASUREMENTS

4.1
4.2
4.3
4.4

Introduction
General Comments on the Interpolated
data
Shepard's Method
Choice of the Weighting functions W(r)

5. GRAPHYCAL REPRESENTATION OF THE RESULTS
5.1
5.2
5.3
5.4

Introduction
Numerical results of the approximation
Graphycal results of the approximation
Concluding remarks.

6. ACKNOWLEDGEMENTS
REFERENCES

�1.
1. INTRODUCTION

Following the results of ref (1) and what anticipated in
the last paragraph of that paper, the present report

is

dealing with the rigorously mathematical and statistical problem
of finding the best methodological procedure to determine in
a

way as unbiased as possible the quantity of TCDD deposited

on the ground within the limits of the so-called "zone-A" around
the Icmesa Factory in Seveso (Italy).
The main features of the problem have been anticipated in
ref. (1) here, in Section 2 we shall define our data sample
while in Section 3 we shall go through all major mathematical
aspects in order to prepare the actual procedure applied in
Section 4. Finally in Section 5 the graphycal result of the
interpolation is presented.
2. DEFINITION OF THE DATA SAMPLE
It is important to qualify and certify the data used in
the integration process: the data used are those obtained in
the 1976

Campaign (December '76) limited, to zone A (for the

reasons given in ref. ( ) .
1)
The topographical distribution of the coordinates belonging

to the points in which the ground sample has been col-

lected is shown in fig. 1.
Zone A has an extention of about IKm

in the East-West

direction and of about 2 Km in the North-South direction and the
collecting points follow an approximately regular grid of
about 50 m x 50 m.
The values of TCDD concentration on the ground vary from
a minimum of 0.75 yg/m
of the analitical
of 5477 yg/m2.

(corresponding to the detectable limit

measurements-denoted as

N.V.) and a maximum

�2.

an
ODD
DODD
D DDD
DDDDDD D
DDD 303
D D D O 3D
DDD D D
D OD DDO _

DDDD D

0 O 3D D D D
0 OD33 C
ODDD03P 3D
D D D D D D D DD
3OODDODD DD3
DDDDDD3DD D D
D D D D D D D D C D DO 3
D D D D C D U D D O D O D3
D D D D D D D D D D D DDDD
D D D D D D D D D 3DD3
D D D D D ODD D ODD
D3DDDC3C
O CO 0
DDDOODODDD DDD3O
DD3DDU3DO33DCDDnO
O p O D D O O D D D ODOQO
_ D Z3 D C D D O O D D O D D O
U
DDDDDODO DDDOD
D O D 3 O D D D C D DD
O DDDDDDD DD
D DD D flDDD D D 3

n a a a DD D
DDD OD 3D D 333
UD D D 3 D D DDDD

D O D D D DD 3C333
D D D 3 Q DDnOD
ODD

Fig. 2.1: Every squares is the thopographycal rapresentation of the
single sample of the 1976 campaign.

�EV./0.5

X =

loss limit

2.34

V = 2.39
40

38O EV.
33 N.V.

30

20

10

I

-3.

-2.

-1.

I

I

O.

1.

I
I . I
3.

t

2.

II
4.

I

5.

I

6.

I

7.

I

I

8.

'

9.

ln

O

(TCDD^g/m )

Fig. 2.2: Histogram of all samples and gaussian curve fitted using only the right part of
data starting from the "loss limit"; numerical results of procedures fit.

�4.

In order to

take into

account the main indications of a

previous analysis of the overall TCDD distribution^

, in the pre

sent report we use as a quantification parameter the logarithm
of the TCDD density

since this is the quantity showing a gaussian

distribution (see fig. 2.2) thus

being the most suitable va-

riable to .be used in an optimization process.
With this variable, the contaminant ranges from a minimum

f
value of - 0.287

iln(yg/m ) and a maximum value of 8.608

ln(yg/m
3. THEORY OF THE MATHEMATICAL

METHOD

3 .1 Introduction
In this Section we define the problem in its general
aspects and propose the algorithms which

have been included

in the program used for the numerical solution of it.
Let D be the quantity of TCDD under consideration which
depends

upon the values directly measured of the location

(?c,y ) which define the coordinate vector(hereafter referred to
as vector x = (x,y)).
Given a set of data providing the values D- of the quantity D(x) in several points X.J, = (x.,y.) in
space, our target will be to find a

a 2-dimensional

explicit function of the

independent vector-coordinate variable

7 = f(x)
To this end a program^ ' will be used to find by means of
a least square fit,a reasonable approximation, of the type

�5.

n
D - E t c. f (x)
1

(3.1.1)

approximating the measured values Di distributed within the
set of measured coordinates (x,y).
In (3.1.1) c. are constant coefficients and f.(x) are
proper polynomial functions of the vector variable x..
The following Sections shall be devoted to the study of
the mathematical functions, to their choice and to the choice
(and definition) of the constant coefficients c..
For sake of semplicity we shall treat the case of a sin
gle independent variable x, which can be easily extended to a mo
re

general multidimensional space x.

3.2 Approximation of an arbitrary function by means of a set
of given functions.
We propose the general problem of representing an arbitra.
ry function f(x), by means of a finite number of functions
chosen with a certain degree of arbitrarity, for instance polynomial of increasing power such as:
po(x), p1(x), P2(x),.....Pn(x)

(3.2.1)

or rather by means of arbitrary linear combinations of the type:
+a

npn(x)

where the coefficients a, can be choosen, within the linear comb_i
nation, in such a way that the difference
dn(x) = f(x)-Sn(x)

(3.2.3)

be "the smallest possible" (in the most general sense still to
be discussed) .

�6.

It is more than clear that the criterion

of "small er

ror" as given by (3.2.3) is largely arbitrary and driven by the
principal interest of using the approximation S (x) instead of
the function f(x) (which

might well be unknown).

Among the most frequently used criteria there is the least-square criterion which requires to minimize the average quadra
tic error

in the range (a,b) for x
d 2

n 'bh | dn°° 2 d x
.

(3 2 4)

''

that is to determine a, by means of a least square fit.
The use of a quadratic form is largely considered an opti^
mal application to the practical calculations.

A least square

fit approximation may give locally large discrepancies but it
gives in general a rather accurate global representation of the
function f(x).
3.3 Conditions on the coefficents a.
_
k

- 2
The most obvious condition to be imposed is that d

be

the minimum possible as a consequence of the choice made on
a, ; being dn a positive polynomial in the variables a o ,ax ..aIT
1}
ic
it indeed admits a minimum.
Thus zeroing the first derivatives with respect to a, we
shall obtain an unique

solution corresponding to a minimum.

Thus:
= 0

k = 0,1,2,..., n

(3.3.1)

From (3.2.4) and (3.2.3) we get, by deriving with respect to

�7.

a, within the integral:
3d

2

n
••
•
3a,
k

—l
b -

=

2a

f

2[f(x)-Sn(x)]^[f(x)-Sn(x)]dx

f»
j -pk(x)[f(x)-Sn(x)]dx

(3.3.2)

k = 0,1 , 2. . . .n

where we take advantage of the fact that the arbitrary function
f(x) is independent of a, , while SXI for the (3.2.2) depends liK.
nearly on ak through

the choosen polynomials pk(x).

Formula (3.3.1) thus becomes:
rb

,b
pk(x)Sn(x)dx = I pk(x)f(x)dx
j
a

|
a

J

k=0,l,2,...n

(3.3.3)

and, given the (3.3.2) for S (x) , formula (3.3.3) assumes the
shape :
fb
fb
r
I pk(x)f(x)dx=aQ| pk(x)pQ(x)dx+a1
*u

J *a

»Q

+ a 11 j| p 1\ ( x ) p II ( x ) d x
,

k=0,l,2,..,n

(3.3.4)

or rather in a compact form, for any k :

fb
n
fb
| pK ( x ) f ( x ) d x = La | i| p, ( x ) p ( x ) d x
i
I
K
j

j

a

o

j

J

J

a

(3.3.5

J

We have thus obtained a linear system of (n+1) equations in the
(n+1) unknowns a..
The solution of such a system is uniquely determined provided the

�9.

M - &lt;-oo »o
£2 = Cj o a 0 + G!! a x

f3

*™

f*
^20

Q - i / ^
** 0
^2 1

Q
** 1

A

/*•
^-22

Q
*2

(3.4.1)

r

=

n

c

no

a2 + c

ni

&amp;i ^ 3. _ f t j * • • • « + c _ a
*
n2
nn n

this selections allows us to add the significant conditions
| p. (x)p.(x)dx = 0
J

j&gt;k,j,k=0,l,2, . . .n

(3.4.2)

J

It is important to note at this point that, as j and k are two
indices restricted

by the relation k&lt;j , but otherwise arbitrary

integers, eq. (3.4.2) must hold also when k and j are interchanged, i.e. k&gt;j so that (3.4.2) implies a more restricted con
dition:

,fb , , , ,,
. . ,,
i p,(x)p (x)dx = 0
j?^k
J
J
a

ORTHOGONALITY

f.

. .
.
(3.4.3)

CONDITIONS

Thus imposing the triangularization of the linear system
we automatically obtain its diagonalyzation*- * this is due to
the fact that the coefficient matrix |C., | (3.3.7) is symmetric
as it immediately appears by inspecting the definition (3.3.6).

If the orthogonality conditions are verified by the system
of the Pv.(x) functions chosen as a basis for the approximation,
then the system (3.3.5) is now reduced to the form, for any k:

�8.

determinant of the coefficient matrix
Ckj =

Pk(x)p..(x)dx

(3.3.6)

3.

be different from zero; i.e.:
Det |Ckj| | ? 0

(3.3.7)

It has to be clear that, if n is large, the expression to solve
the system (3.3.5) which can be rewritten as:

7. C, .a. - F,
L
i ki Ji
k
o

(3.3.8)
J
^

:
where F. = I Pi (x)f(x)dx, may be anything but a simple problem.
i = I K
K
a
In such a case the use of the approximation S (x) would be a

bad and unconfortable choice.f 4)

3.4 Choice of the functions Pi,(x)
In order to overcome the difficulty we have to perform a
suitable choice on all possible functions {p, (x)} in such a way
that the solution of the system (3.3.5) be as simplified as pos_
sible.
Among the most interesting choices is a selection of the
functions pv(x) such that the system (3.3.5) be reduced to a
.K

triangular

form, without lack of generality. That is a selection

on the basis of which in the K-th equation only the unknowns a. with j$k appear,'i.e. :

�10

f P (x) 2 dx = r| p (x)f(x)dx
k I
k
k
\
JQ
JQ
'a

(3.4.4)

since only the integral having j=k turns out to be different
from zero in the left-hand side of (3.3.5).
It follows immediately then that a, is simply given by
a

v

=

~T~

I PvCx)f(x)dx

for any k

(3.4.5)

where

f

p(x)

2

dx

(3.4.6)

is a positive normalization constant; i.e. a positive number
which depends exclusively

upon the functions P^CX) but not

upon the function f(x) to be approximated.
In this subsection we have thus reached the following re
suit: if the functions P^Cx) are orthogonal (and it is

always

possible to select a set of well -known orthogonal functions)
the problem of approximating an arbitrary function f(x) is solved by (3.4.4) .

3.5 Legendre Functions and Tchebychev Functions
In the previous Sections we have introduced the problem
of the least-square approximation and clearly underlined the
need to select a system of functions having the requisite of
obeying the orthogonality conditions since in such a case the
solution of (3.3.5) is particularly simplified.

f
The ortogonalization process suggested by Gram-Schmidt^ 4)
provides

a tool to select from among

a finite or an infinite

set of linearly independent functions defined in the range (a,b)
a set of functions which are orthonormal in (a,b).

�11.

In this section we briefly propose two important and well
known orthogonal systems which will constitute the alternative
basis of our data handling.
The first system is provided by the Legendre polynomial^ '
functions. They are defined by the formula:

-

(2n-l)(2n-3)...1
1
ft

X

n n(n-l) n-2
-2(^l7X +

,. . ^
-5'1)

(3

and alternatively by the recurrence formula
p,

,
*(n+l)-,(x) =n+1 :— *nxp (x)--- p , (x)
n+1 *n-l

(3.5.2)

from which the very first components are easily derived:

P0(x) = 1
PjCx) - x
p(x) =

(3x2-l)

(3.5.3)

= -r(5x -3x)

It is of fundamental importance the result &gt;
1

pm(x)pn(x)dx = 0

m y n

(3.5.4)

which is a consequence of the orthogonality conditions. It implies
that the Legendre Polynomial Functions are orthogonal in the ran
ge ( ! + )
-,!.

�12.

The second example of orthogonal system is provided by the
Tchebychev polynomial functions
which-are defined by the formula
tn(x) = cos (n cos

x)

(3.5.5)

From (3.5.5), by using the De Moivre Theorem and the Theorem on
the binomial's power we can rewrite:
I
T l (x)=xn-fnWn~2fl-x)2+/A.Jtn~4fl-x)4 + •••'
l Aj-A
171
*•
' I
*•
'

(3 S 6)

I.J.O.UJ

and alternatively write the recurrence formula:

X) = 2X

VX) - Vl

(3 5 7)

''

from which the very first components can be easily derived
To(x) - 1

T (x) = x
T2(x) - 2x2-l

(
3 5 8
)

''

T3(x) = 4x3-3x
The Tchebychev polynomial functions are orthogonal in the range
( ! + ) since for
-,!

[

T

m(x)Tn(x) dx = 0

(3.5.9)

As a general matter, in a non-orthogonal model, in order
to estimate the value of a coefficient a^ one has to know all the
other preceeding coefficients a.(j&lt;k) as well as all the following coefficents a.(i&gt;k) as one has to invert the matrix
(3.3.6). In an orthogonal model, on the contrary, all coeffi-

�13.

cients can be separately evaluated since we are dealing with a
diagonal matrix.
However an orthogonal model has to be preferred not only
for a matter of convenience and mathematical
method appears to be very sure
errors which so often become

semplicity; the

against the dangerous

round-off

relevant in computer working.

We conclude this section by stating

that the Tchebychev

polynomal functions are practical to minimize the MAXIMUM ERROR, while the Legendre polynomial functions are practical to
minimize the ERROR OF THE MEAN.

3.6 Multidimensionl parametrization.
In this Section we indicate the most natural procedure to
extend the proceeding algorithm to an

n-dimensional space,

limiting however one computation to the case under consideration which requires a 2-dimensional space.
In our case, then, for the approximation of a two dimensi£
nal function D(x,y) by means of a linear combination of Tchebychev polynomial functions we can write:
D(x,y) = Z
m

1C
T (x)mT_(y)
n mn n

(3.6.1)

Let

n
Then we can write
D(x,y) = I' a (x) T (y)
m
1U
m

(3.6.3)

Clearly in the two dimensional case a strategy for the selection
of the most convenient functions is needed, since all possible

�14.

combinations Tv(x)-T.(y) constitute a very large variety of
J
possibilities.
An obvious procedure, which incidentally

economizes o.n

computer time, suggests to consider first the lower order fun
ctions; in addition, for each given function taken into account
prove if its contribution to the reduction of the squares of the
residuals is large enough (step by step improvement).
To

prove this latter point, even using a non orthogonal

model, it is not strictly necessary to invert the matrix but an
orthogonalization can be reached by applying the Modified
()
4
Gram-Schmidt procedure.
In this way an orthogonal model is easily built in which
the potential reduction in the sum of the squared residuals
AS? is easily evaluated for the different choices of the functions f., in the available

measured values of the represen-

tative function D(x) to be approximated D^(x.,y.)«
In summary we can handle our multidimensional

approxima-

tion problem if we can reduce the large number of possible arbitrary functions to a few dozens and if we can perform an orthogonal transformation able to reduce the approximation to
the one-dimensional case, which implies a single inversion of
a triangular matrix, at the most.

4. PSEUDOMEASUREMENTS.
4.1 Introduction
The data sample is provided by the 1976 campaign during
which carets have been collected every A, 50 m.
However in order to perform a two-dimensional fit the
starting sample has to be increased by producing new pseudo-mea
surements in a much denser grid. In fact for a convergent ap-

�15.

proximation of the function D(x,y) described in Capt. 3 at least
50 measurements per coefficient is desirable.
Then our target here is to construct a new data sample
which preserves the structure and the characteristics of the
original one, by properly interpolating the TCDD values in intermediate points.
The starting experimental data are not sufficient to guarantee the applicability of the model; from them the results
obtainable in a straight forward way are those of Ref. 1.

4.2 General Comments on the Interpolated data.
The interpolation needed to guarantee a sufficient number
of starting measurements in order to perform the approximation
of D(x,y) is based on the following procedure:
given in a limited region of the x,y plane a number of mea
surements D.(x.,y.) in the points (x.,y.)» look for a function
g(x,y) able to designate a reasonable value of D in any arbitra
ry point (x,y).
The domain in which our experimental function is defined
has a non-geometrical form (since the limits of zone

A are i_r

regular as well as the distribution of the original measurement
points (x.,y.)).Then we replace the contour with a rectangle
subdivided into a regular grid both in x and y. The crossing
points of the new grid are the reference points in which we intend to evaluate the new interpolating function g(x,y).
Two basic methods provide a solution of the problem:
- the first one consists in building a function g which interpp_
lates exactly the measured values, i.e.:

�16.

g(xi,yi) = Di

i-1,2,.....n

(4.2.1)

This method gives excellent results only when the values
D. are known with high accuracy;
- The second method consists in building a function g as a
weighted average of the experimental observations and it is
desirable when the starting experimental data are likely to
be subject to inaccuracies and large unavoidable fluctuations.
Due to the nature of our data we choose the weighted interpolation, suggested by D.Shepard
Essentially the weighted

and recently used by others.

''

interpolation of sparse data

irregurarly scattered can be represented by the following for_
mula:

J
"

(4.2.2.)

where :
D,,

is the measured value in the point (x, ,y, )

W(r, )is a proper weighting
r,
K

function

is the distance between the points (x, ,yK ) and (x.,y.)
v
K
1
J

Note that the value g(x.,y.) represents the weighted avera
ge of the observations of the entire sample in the case of a
"global interpolation"; it represents the weighted average value of the sorroundings observations for a "local" interpolation.

�17.

4 . 3 Shepard's Method

f 7a)
The Shepard's interpolation method,
in its general form is
applicable to measurements arbitrarily scattered.
Given in the plane a point (x,y), let r. be the distance
between (x,y) and the n points(x.,y.) in which measurements
have been made, for any i = l,2,...n.
The Shepard's interpolation formula reads:
?. D(x. 7
,y.) W (r .)
^i ^ i 1
r

g(x,y) =

if r^O
V
li W f riJ
w U ^

1
g(x,y) = D (xi,yi)

(4.3.1)
if ri=0

Note that (4.3.1) is defined in all points of the plane
R

and that it interpolates exactly the values D. in the given

points (x.,y.)&gt; while the value g(x,y) in the "new points" is
given as the weighted average of all given measurements. The
contribution of the i-th measurement is weighted as a function
of the distance between the point (x,y) under consideration and
the given points (x.,y.)It is obviously inconvenient to use this method when n is
very large; however in such a case the method would not be
needed.
Furthermore the method increases in selectivity when the
interpolation is performed in local form.
Let us fix a radius R&gt;0 and define a weighting function

�18.

W(r) = W(r)

if r $ R

W(r) = 0

(4.3.2)

if r &gt; R

Thus in the local form formula (4.3.1) becomes:
Zi D(xi&gt;yi)

W (r.)

g(x,y) = ^
Z.
I1

if?i £ R

(4.3.3)

W (r.)

g(x,y) = 0

if r ^ R

Formula (4.3.3) is still defined in every point of the
plane, but now the value

of the function in the point (x,y) is

given by the weighted average of the measurements D(x.,y.) only
in the neighbouring circle of radius R.
Therefore the problems is now lying in a reasonable choice
of the values for the cut-off radius R in such a way that for
any

point (x,y) of the plane there is an adeguate number of

measurements included in a circle of radius R, so as to compensate fluctuations.
This second method opens up the new possibility of choosing
different values of R, in different regions
within

of the

domain

which D(x,y) is defined.

Theoretically the choice of R, in this kind of procedure
depends upon the statistical sample under

consideration.

In our particular case we want to define a variable R depending upon the distance from the ICMESA Factory having in mind
both the topographycal distribution of the measurement points
and the TCDD concentration. Infact maximal TCDD concentration is

�19.

found immediately around ICMESA and, due to the transport
phenomenon caused by the wind, along a maximum concentra(81
tion bound
in the south-east direction, while, perpendicular to such a line and away from it the TCDD concentra_
tion values are significantly decreased.
Therefore the choice for R has been done in order to
maintain these particular characteristics.
4 . 4 Choice of the Weighting functions W(r)
In the practical case with which we are dealing we wish
to introduce weighting factors W(r) able to preserve statistically the same characteristics of the original sample, a
point which has been clearly pointed out from the beginning.
The choice is suggested by the successfull use, (found in
the literature) in metheorology f 71 to solve analogous problems
such as, for instance, the distribution of the ozone concentration in the bay around Los Angeles (U.S.A.). A reference
to the papers by Gustafson, Kortanek, Sweigart
McRae, Seinfeld

and by Glahn

(7b)

, Goodin,

is imperative.

To perform the calculations of Sect. 5 we have selected
three weighting functions.
The first choice is:
W(r) = ^ "
2^

(4.4.1)

R +r

The second is :
W(r) =

i+T(r)~ S2(r)

where
S(r) = i
„

having defined

,

27
4R

if
R-r2

0&lt;r4-|
.. R

(4.4.2)

�20

m
I
T(r)

*-i

(4.4.5)

m

I

S^(r)

in which:
- m is the number of measurement
of radius

points lying within the disk

R

- a is the angle defined by the segment (see fig. 4.1)
(xk,yk)-(xi,y.)

and

(x i ,y )-(x 1 ,
JCMESA

MAXIMUM
CONCENTRATION
LINE

Fig. 4.1

the t h i r d choice is
W(r) = (l+T(r).)S(r)
S(r) =

Fig. 4.2
T(r)

as defined by ( 4 . 4 . 3 )

In the first choice, formula (4.4.1), the weighting factor
depends only on the distance between the point (x,y) in which
we want to construct a pseudo-measurement and the original mea.
surement-points (x.,y.) falling within the disk of radius R.
In the other two methods a directional dependence is also
included by (4.4.5) .
In all 5 methods R is variable in the plane according to
the increase in the width of the contaminating cone in the wind
(8^
direction along the maximum contamination liner (see fig.4.2)
All the three formulae (4.4.1); (4.4.2) and (4.4.4) give
final samples which are well compared in their global characte:
ristics with the real data.

�21.

As an example fig. 4. 3 and fig. 4. 4, obtained with the pro(9)
gram HBOOK
, give the scatter plots of the original data
while fig. 4. 5 and fig. 4. 6 give the scatter plots of the
ched sample using (4.4.2). These are not topographycal maps;
in fig. 4. 3 In(TCDD) is plotted versus x and in fig. 4. 4 In(TCDD)
is plotted versus y for the original data sample.
Comparing fig. 4. 3 with fig. 4. 5 the density of points are
different but the structure of the two data samples is the
same; points with large TCDD values around 5000 yg/m %exp(8.5)
yg/m

are very few and have small abscissa x (see fig. 2. I for

the definition of the reference frame) while the majority of
the points have values between 2.7 yg/m ^exp(T.O) and 150 yg/
m ^exp(5 .0) .
Comparing fig. 4. 4 with fig. 4. 6, the points with large TCDD
values are fewer and located at large y coordinates (close to
the Icmesa Factory in the reference frame of fig. 2. 1). Furthe_r
more one can notice that the granularity of the information is
increased but that in the regions where there was no data in
fig. 4. 4, no pseudo-data have been invented in fig. 4. 6; an observation supporting the adeguateness of the Shepard's method
to our goal.
In conclusion we wish to point out that (4.4.4) contains
the maximum "a priori" information that can be extracted from
the original data sample as a guide-line to the finding of
the approximating function D(x,y).

�22.
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�26.

5. GRAPHICAL REPRESENTATION OF THE RESULTS

5.1 Introduction
In this final Section we shall present the results of our
investigation by showing the quantitative solution of the approximation of the contaminant distribution in zone A by means
of the analytical function built with a number of Tchebychev
polynomials.
Two different presentations of our results will be given:
1 - a quantitative presentation of the coefficient for the dif
ferent polynomials and the confidence parameters
2 - a graphycal drawing of a 3-dimensional surface as seen from
different perspective points describing the TCDD distribution in a rectangle containing zone A, using the program
SURFAC1-10-1 .
We have checked the goodness of the model adopted and compared our results with those obtained in previous investigations
. The model is adequate and several characteristics,
already pointed out by others, are verified.
5.2 Numerical results of the approximation
The data constructed with the interpolation methods described in Sect.4 have been used as input to the program MUDIFI
(Multi-DjLmensional-FJ^tting) . The principal algorithms have
been outlined in Section 3.
The program allows to fix the number of coefficients a,
that we want to introduce in the final form (3.1.1) and gives
the possibility to specify if the approximation has to be pe:r

�27.

formed with functions product of simple monomials

in the two

variables x and y or rather with orthogonal polynomial

forms

such as, for instance, the Tchebychev functions of Sect.3.5.
We have, thanks to the Shepard method, a relevant number
of input points; thus the goal of a rather accurate represen
tation of the unknown function y(x,y) measured in n points
y.=D.(x.y.) can be reached by using as many as 30 free parame_
ters (coefficients a

iC

) to build the approximant function D(x,y).

We show in the present paper only the results obtained by
the use of the Tchebychev orthogonal polynomial (3.5.5) (3.5.6)
(3.5.7) and (3.5.8) mentioned in Sect.3, and on the interpola(1
tion method, mentioned in Sect.4, using only the formula (4.4.4). 4)

The all procedure however has been applied also using the
(14)
Legendre polynomial
Due to the particular nature of the experimental data which
often show large fluctuations even between very close points,
and due to the very large ratio between the "area of zone A"
and the "total area of zone A submitted to the contamination
analysis", the results of our approximation can be considered
as sufficiently good.
In Table 5.1 the values of the residuals for each of the
coefficients are collected and the corresponding reductions
together with the value of the multiple correlation coefficient
C are given.
Table 5.2 collects in the first column the values obtained
for the 30 coefficients a , in the second column the variance
1C

and in the third column the degree of the Tchebychev polynomials
to which they refer.
As an explicative

example, the second line quotes the coe-

fficient a (col.1) = (0.759

±

0.140) related to the combination

�28.

(col.3) 01. This means that a-j^ refers to the product T (x)T..(y). .
The second coefficient (line 3) is related to the combination
20 which means that a 2 refers to the product T£(X) T (y) .
Explicitely:
D(x,y) = (2,61± .183)+(.759± .14)T()(x)T1 (y) -

(5.2.1)

- (0.268* .101)T2(x)To(y)-....+ai.T.(x)T.(y)
and from (3.5.8) :
D(x,y) = (2.61± .183)+(.759± .140)y-(0.268± .101)• (22 -1)+

(5.2.2)

The parameter C of Table 5.1 gives an indication for the
goodness of the approximation. The closer C is to unity, the
better the fit can be considered.
As one can notice in Table 5.1, coium 5, the sum of the
residuals is reduced by about a factor 10 per coefficient; the
multiple correlation coefficient is^O.87 close enough to 1.0
for our purposes. Finally in Table

5.2 the errors on the diffe

rent coefficients are very reasonable.
As a matter of principle the "mathematical" result could
improve for instance by allowing a larger number of coefficents,
which would require a larger number of data points. Alternative;
ly we could "eliminate" so.me "bad point" giving a value of
TCDD drastically different from the nearby values and reflecting an anomalous large fluctuation.
In this paper

however by all means we do want to give an

unbiased interpolated description without any arbitrary elimi.
nation of any value.
Therefore we claim that the result presented is the best
possible in the given circumstances.

�29.

COEFF
MO

1
2
3
4
5
6
7
8
9
10

11

12
13
14
15
16
17
18
19
20
21
22
23
24
25
26
27
28
29
30

SUM OF SQUARES
OF RESIDUALS

REDUCTION OF
OF SQUARES

0.3536308594E+04
0.2996910889E+04
0.24290?5947E+04
0.2265266357E+04
0.2099861084E+04
0.1831718872E+04
0.1688964111E+04
0.1568103638E+04
0.1356953613E+04
0.1051628662E+04
0.9939321899E+03
0.9610200806E+03
0.8918918457E+03
0.8129942017E'+03
0.7688598633E+03
0.7501573486Ef03
0.7405953979E+03
0.7146628418E+03
0.6897740479E+03
0.6724725342E+03
0.6638720093E+03
0.6075493774E+03
0.5990665894E+03
0.5884318848E+03
0.5616769409E+03
0.5530006714E+03
0.5437915039E+03
0.5315605469E+03
0.5212128906E+03
0.5128872681E4-03

0,3754131775E'f03
0.5393977661E+03
0.5678148804F+03
0.1638295898E+03
0.1654051971E+03
0.2681422729E+03
0.1427547302E+03
0.1208605042E+03
0.2111499786E+03
0.3053250122E+03
0.5769648743E+02
0.3291210556E+02
0.6912826538E+02
0.7889766693E-K-2
0.4413433838E+02
0.1870249748E+02
0.95A1931610E+01
0»2593254089E+02
0.2488878632E+02
0.1730154228E+02
0.8600533485E+01
0.5632264328F. + 02
0.8482768059E+01
0.1063469791E+02
0.2675496292E+02
0«8674253319E+01
0.920918J786E+01
0»1223097420E+02
0.1034767246E+02
0.8325633049E+01

MULTIPLE CORRELATION COEFFICIENT

Tab. 5.1:

Results of the function weight
W(r)=[S(r)32(l+T(r))
2
2
R - r
S(r) =
2
2
R + r

0.868885E+00

�COEFFICIENTS

VALUE

VARIANCE

0
1
2
3

0.2611816406E+01
0.7591783404E+00
-0.2681191862E+00
•0.8827306628E+00
-0.4400894046E-01
0.5425338745E+00
0.6950988173E+00
0.6278941631E+00
0.5745822191E+00
0.2406100035E+00
0.1857A45333E+00
-0.3786304593E+00
0.3746468425E+00
0.2251543403E+00
0.6250208616E+00
0.392A346600E+00
0.2824673951E+00
0.4311328530E+00
0.6149656773E+00
0.6629428864E+00
-0.4905254394E-0"!
-0.5814285B74E+00
-0.6244755387E+00
-0.6606221199E-01
0.2131620049E+00
-0.3567886055E+00
-0.1992565244E+00
0.5482710898E-02
-0.2291990817E+00
0.1528140604E+00
-0.1678609997E+00

0.182943E + 00
0.140330E+00
0.100968E+00
0.479781E4-00
0.116808E+00
0.242769E+00
0.129216E+00
0.132157E+00
0.974676E-01
0.13815lEfOO
0.5A6410E-01
0.667838E-01
0.998844E-01
0.917134E-01
0.762477E-01
0.259199E+00
0.149761E+00
0.224754E+00
0,199875EtOO
0.532743E-01
0.121924E+00
0.993173F.-01
0.462425E-01
0.700691E-01
0.7A5648E-01
0.877238E-01
0.753213E-01
0.666651E-01
0.782392E-01
0.760031E-01

4
5
6
7
8
9
10
11
12
13
14
15
16
17
18
19
20
21
22
23
24
25
26
27
28
29
30

Tab. 5 - 2 :

POWERS OF VARIABLES
IN M O N O M I A L

0 0

Results of the function weight W(r)=[s(r)J

()
2
4
1
3
3
1
5
3
5
0
2
5
7
7
1
0
1
2
A
3
1
0
4
7
7
8
8
7
8

1
0
2
1
0
1
5
2
5
3
5
6
4
5
6
0
2
2
2
0
3
6
8
5
2
3
4
5
7
6

(l+T(r)) ; S(r)= R -r
—
2 2
R +r

CM

O

�31

5.3 Graphycal Results of the approximation.
Having obtained the analytical form

of the function

D(x,y) completing (5.2.2) with all the terms indicated in
Table 5.2 (that is having obtained the mathematical descri^
ption of the TCDD distribution on the ground),we can graphy^
cally visualize the result so as to give a direct check of
the overall properties of the distribution function and of
the approximation procedure adopted. (The graphycal visua- .
lization could also suggest general comments on the topogra.
phycal distribution in comparison with the equal density line
description given in ref.8).
To solve the graphycal problem,we have used the program
SURFAC *•

. It is a multipurpose program which produces a

prospectic view of a function given in cartesian coordinates.
The resulting figure draws the intersections of the sur
face with parallel planes orthogonal to the axes. To obtain
the visualization of possible "hidden points"

of the surface

it is possible to rotate the entire figure by a variable angle (which can be properly

chosen) from -90° and *90°.

In fig.s 5.1, 5.2,5.3,5.4 the function D(x,y) given by
(5.2.2) is shown from different points of view under different
angles. The vertical axis (In TCDD concentration) is not relevant here and is reported only on fig. 5.1.
Let us comment on fig: 5.1 which shows the function rotated
by 30° clockwise

with respect to the North-South direction.

We can clearly notice that there are two pronounced peaks
in the vicinity of the ICMESA Factory; then the function decre
ases along the y axis maintaining

however large TCDD values

�32.

along the well defined band of maximum concentration mentioned in Sect. 4.4 and determined in ref. 8 .
Note that zone A is included in the rectangle (fig.5.1); the
contours of the function are not always slowly degrading but
show secondary maxima. This is due to the fact that the analy_
sis has been limited to zone A where the TCDD concentration is
maximal, but which does not cover all the

domain of the conta

minated region. Nonetheless, the secondary maxima are not very
relevant and coincide with those shown in ref.8 .
Fig. 5.3 seen from,an angle of 60° clockwise, shows the
surface from a direction almost perpendicular to the maximum
concentration line.
Fig. 5.4, seen from an angle of 60° counterclockwiset
shows the surface almost along the maximum concentration line
clearly showing the decrease of the TCDD concentration with the
distance from the ICMESA Factory.
It is important

to point out that the weak points of

the analysis is concentrated at the boundaries. There the
number of measured points _ls small.
It is however interesting to note that,in spite of this
the surface is satisfacorily

reproducing the known overall

characterics of the distribution (even if the knowledge is relatively scanty).
A quick subdivision of zone A into small rectangles

gives

the average TCDD concentrations reported in Table 5.3.
The graphycal description reproduces also quantitatively
the numerical description.
We can thus conclude that the empirical model proposed in this
paper

is adeguate to reproduce the reality with sufficient

accu

�33

racy and proves that the approach used may be interesting
for applications to similar problems.

5.4 Concluding remarks
The analysis performed in this paper is one of the possible investigations which can be performed in connection with
the ICMESA accident. Although with a much lower significance
one could extend the analysis to all the contaminated region
taking nontrivial risks, but providing a tentative complete
mathematical description of the phenomenon.
We certainly believe that the procedures used could be
applied to similar cases since, by using relatively simple
and handy mathematical formulae it is possible to build a
descriptive function over a given geographycal extension of
an area interested by a measured phenomenon, putting in evidence both the global and local characteristics of the measu
rement.
As of the value of the integral we prefer to be as cautious
as possible.
As explicitely stated in ref.8 and in ref.1 the multiplication factor between analyzed area and contaminated area is
c

R=3.04x10^ for zone A.
This imposes a priori an enormous incertainty on any poss_i
ble result. The numerical integration performed here is however
the best mathematical calculation which can be performed, given
the original measurements.

�F i g . _ 5 . 1 : Rotation ane;le + 30 C

�CO

Fig.5.1 : Rotation angle + 3O°
This grhafh id limited to A zone borders

�TCMMSA

I
*
VJI

Fig. 5.L&gt;: rotation angle 45'

�w
ICMESA

Fig.5.2: rotation
angle 45°
This grafh is limited to A zone borders

45'

�TCMESA

Fie.

5.3 :

rnhat-.i nn

�HA

-60

F i g . r &gt; . 4 ; rotation

angle -

�TCMESA

Q
•

*f

Fig. 5.4: rotation tingle - 60°
This gr-aph is limited

to A zone borders

�38.

TCDD= TCDD=
3.720

4. 104

ICMESA

TCDD= TCDD= TCDD= TCDD=
1.7H

5.081

2.102

0.312

TCDD= TCDD= TCDD= TCDD=
0.681

1.116

3.589

1.185

TCDD= TCDD= TCDD= TCDD=
2.502
3.811
1.702
2.911
TCDD= TCDD= TCDD= TCDD =
2.890
2.233
2.657
2.167
TCDD= TCDD= TCDD=
2.752
2.015
2.371
Table 5 - 3 : Average concentrations of the logarithm of TCDD

�. ,^:1
39.

6. ACKNOWLEDGEMENTS

We thank all the personnel of the Institute of Nuclear
Physics - University of Pavia - and of INFN - Sezione di
Pavia for their collaboration.
In particular Mr. F.Bossi and G.Fumagalli for the excel^
lent support in the use of the computers and of the program
libraries .
REFERENCES

1) G.Belli, S.Cerlesi, S.P.Ratti: "Valutazione della quanti_
ta di Diossina depositata al suolo entro la zona A"
IFNUP/RL

14/81

2) G.Belli, G.Bressi, S.Cerlesi, S.P.Ratti: "The chemical
accident at Seveso (Italy):statistical analysis in regions
of low contamination".

(CHEMOSPHERE 12, 517-521

1983);

3) R.Brun, M.Mansroul, H.Wind: "MUDIFI - Multi Dimensional
FIT Program".
CERN Report DATA Handling Division
4) K.S.Kunz: "Numerical Analysis"

McGraw-Hill, N.York (1957)

5) Ch.Jordan: "Calculus of Finite Differences"
Chelsea, N.York (1950)
6) Monografie di Matematica Applicata

CNR

G.Vitali, G.Sansone: "Moderna teoria delle funzioni di
variabile reale" Zanichelli
Parte II: "Sviluppi in serie di funzioni ortogonali"
Sansone

1946

7) a - D.Shepard: "Proc. XXIIIrd A.C.M. National Conf.
Las Vegas" (1968) p.517
b - S.A.Gustafson, K.O.Kortanek, J.R.Sweigart
J.Appl.Meteor. jL^, 1243 (1977)

�r

40.

c - W.R.Goodin, G.J.McRae, J.H.Seinfeld
J.Appl.Meteor. 1_8, 761 (1979)
d - H.R.Glahn
J.Appl.Meteor. 20, 88 (1980)
8) G.Belli, G.Bressi, E.Calligarich, S.Cerlesi, S.P.Ratti: in
"Chlorinated Dioxin &amp; related compounds: impact on environment" (Ed. O.Hutzinger et al.

Pergamon Press, Oxford,

N.York) 1982 p. 155
9) R.Brun, I.Ivanchenko, P.Palazzi: "Hbook User's Guide, version
3.0"

CERN Report DATA Handling Division

10) Harold V.McIntosh: "SURFAC"
11) S.Cerlesi: "10 luglio 1976: incidente ICMESA" (Thesis
Univ. of Pavia 1979) .
12) P.Sartori: "Analisi statistica della distribuzione di
diossina fuoriuscita dal reattore chimico dell'Icmesa"
(Thesis Univ. of Milano 1980 Unpublished).
13) G.Belli, G.Bressi, E.Calligarich, S.Cerlesi, S.P.Ratti:
in "Chlorinated Dioxins &amp; related compounds: impact on
environment" (Ed. O.Hutzinger et al. Pergamon Press,
Oxford, N.York) 1982 p. 137
14) E.Milani: "Distribuzione di diossina sul terreno inquinato attorno a Seveso" (Thesis Univ. of Pavia 1981 Unpublished) .

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                  <text>&lt;p style="margin-top: -1em; line-height: 1.2em;"&gt;The Alvin L. Young Collection on Agent Orange comprises 120 linear feet and spans the late 1800s to 2005; however, the bulk of the coverage is from the 1960s to the 1980s and there are many undated items. The collection was donated to Special Collections of the National Agricultural Library in 1985 by Dr. Alvin L. Young (1942- ). Dr. Young developed the collection as he conducted extensive research on the military defoliant Agent Orange. The collection is in good condition and includes letters, memoranda, books, reports, press releases, journal and newspaper clippings, field logs and notebooks, newsletters, maps, booklets and pamphlets, photographs, memorabilia, and audiotapes of an interview with Dr. Young.&lt;/p&gt;&#13;
&lt;p&gt;For more about this collection, &lt;a href="/exhibits/speccoll/exhibits/show/alvin-l--young-collection-on-a"&gt;view the Agent Orange Exhibit.&lt;/a&gt;&lt;/p&gt;</text>
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                  <text>&lt;p style="margin-top: -1em; line-height: 1.2em;"&gt;The Alvin L. Young Collection on Agent Orange comprises 120 linear feet and spans the late 1800s to 2005; however, the bulk of the coverage is from the 1960s to the 1980s and there are many undated items. The collection was donated to Special Collections of the National Agricultural Library in 1985 by Dr. Alvin L. Young (1942- ). Dr. Young developed the collection as he conducted extensive research on the military defoliant Agent Orange. The collection is in good condition and includes letters, memoranda, books, reports, press releases, journal and newspaper clippings, field logs and notebooks, newsletters, maps, booklets and pamphlets, photographs, memorabilia, and audiotapes of an interview with Dr. Young.&lt;/p&gt;&#13;
&lt;p&gt;For more about this collection, &lt;a href="/exhibits/speccoll/exhibits/show/alvin-l--young-collection-on-a"&gt;view the Agent Orange Exhibit.&lt;/a&gt;&lt;/p&gt;</text>
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