Estadística
Programación con Matlab
MÉTODOS DE COMPUTACIÓN ESTADÍSTICA
Chapter 1
Introduction to MATLAB
1.38. The classic quadratic formula says that the two roots of the quadratic equa-
tion
ax2 + bx + c = 0
are
x1; x2 = ¡b § pb2 ¡ 4ac
2a
Use this formula in Matlab to compute both roots for
a = 1; b = ¡100000000; c = 1
Compare your computed results with
roots([a b c])
What happens if you try to compute the roots by hand or with a hand
calculator?
You should ¯nd that the classic formula is good for computing one root, but
not the other. So use it to compute one root accurately and then use the fact
that
x1x2 = c
a
to compute the other.
X1=(-10^-8+sqrt(10^16-4))/2
X1 =
5.0000e+007
X2=(-10^-8-sqrt(10^16-4))/2
X2 =
-50000000
>> help roots
roots([1 10^8 1])
ans =
1.0e+008 *
-1.0000
-0.0000
Ejercicio sin número sobre error absoluto y error relativo:
Calcular el error absoluto y relativo producido al calcular n factorial con la formula de Stirling n=1,……..,17.
f=factorial(10)
f =
3628800
>> fs=sqrt(2*pi*10)*exp(-10)*(10^10)
fs =
3.598695618741036e+006
>> er=abs(f-fs)/f
er =
0.00829596044394
ea=abs(f-fs)
ea =
3.010438125896407e+004
f=factorial(20)
f =
2.432902008176640e+018
>> fs=sqrt(2*pi*20)*exp(-20)*(20^20)
fs =
2.422786846761134e+018
>> ea=abs(f-fs)
ea =
1.011516141550643e+016
>> er=abs(f-fs)/f
er =
0.00415765262288
Ejercicio sin numero:
% error relativo y absoluto
%en la formula de Stirling
%imprime una tabla mostrando
%el error producido por la
%aproximacion de Stirling
%para n!
close all;clc
disp('')
disp(' Aproximation absolute relative')
disp(' n n! Stirling error error')
disp('----------------------------------------------------------------------------------------------')
e=exp(1);
nfact=1;
for n=1:17
%f=factorial(n);
f=n*f;
fs=sqrt(2*pi*n)*((n/e)^n);
abserror=abs(f-fs);
relerror=abserror/f;
d=sprintf(' %2.0f %16.0f %18.2f %16.2f %5.2e',...
n,f,fs,abserror,relerror);
IMPORTANTE:%18.2 es 18 digitos con 2decimales,por lo tanto quedan 16enteros;la f sigifica el formato que le corresponda y la e significa en formato decimal;como d=sprintf(' %2.0f %16.0f %18.2f %16.2f %5.2e',...
n,f,fs,abserror,relerror) esta entre comillas eso significa que es un texto
disp(d)
end
Lo compruebo o ejecuto:
Aproximation absolute relative
n n! Stirling error error
----------------------------------------------------------------------------------------------
1 1 0.92 0.08 7.79e-002
2 2 1.92 0.08 4.05e-002
3 6 5.84 0.16 2.73e-002
4 24 23.51 0.49 2.06e-002
5 120 118.02 1.98 1.65e-002
6 720 710.08 9.92 1.38e-002
7 5040 4980.40 59.60 1.18e-002
8 40320 39902.40 417.60 1.04e-002
9 362880 359536.87 3343.13 9.21e-003
10 3628800 3598695.62 30104.38 8.30e-003
11 39916800 39615625.05 301174.95 7.55e-003
12 479001600 475687486.47 3314113.53 6.92e-003
13 6227020800 6187239475.19 39781324.81 6.39e-003
14 87178291200 86661001740.60 517289459.40 5.93e-003
15 1307674368000 1300430722199.46 7243645800.54 5.54e-003
16 20922789888000 20814114415223.09 108675472776.91 5.19e-003
17 355687428096000 353948328666099.44 1739099429900.56 4.89e003
>>
14-marzo-06
MATLAB respuestas a la pagina 49 de unidades didácticas 01_intro.pdf
%este programa calcula el
%seno de x usando el
%desarrollo en serie de taylor
%en torno al cero
%sin(x) = x - x^3/3! + x^5/5! - ...
%el criterio de parada del
%bucle "while" consiste en
%que el siguiente termino
%de la serie sea tan pequeño
%que no modifique el resultado
%obtenido hasta el momento
function s = powersin(x)
s = 0;
t = x,
n = 1;
while s + t ~= s;
s = s+t;
t = - x.^2/((n+1)*(n+2)).*t *para hallar ~ es: alt+126
n = n+2;
end
-
control+c desbloquea las operaciones
lo abrimos y lo usamos:
>> powersin(pi)
t =
3.1416
ans =
2.4791e-016
>> x = 11*(pi)/2;
>> e=abs(powersin(x)-1)
t =
17.2788
e =
2.0000
>> sin(11*pi/2)
ans =
-1
>> sin(21*pi/2)
ans =
1
>> e = abs(powersin(x)+1)
t =
17.2788
e =
2.1287e-010
*donde e es igual al erros, abs igual al valor absoluto.
>> x = 21*(pi)/2;
>> e = abs(powersin(x)+1)
t =
32.9867
e =
1.9999
>> e = abs(powersin(x)-1)
t =
32.9867
e =
1.3324e-004
>> x = 31*(pi)/2;
>> e = abs(powersin(x)-1)
t =
48.6947
e =
5.8230e+003
-
modificamos el programa inicial:
function [s,k] = powersin(x)
s = 0;
t = x,
n = 1;
k = 0;
while s + t ~= s;
k = k +1;
s = s+t;
t = - x.^2/((n+1)*(n+2)).*t;
n = n+2;
end
Operamos:
>> [s,k]= powersin(x)
t =
48.6947
s =
-5.8220e+003
k =
78
>> x = (pi)/2;
>> [s,k]= powersin(x)
t =
1.5708
s =
1.0000
k =
11
*cambiamos de nuevo el programa :
function [s,k,tmax] = powersin(x)
s = 0;
t = x,
n = 1;
k = 0;
tmax=x;
while s + t ~= s;
k = k +1;
s = s+t;
t = - x.^2/((n+1)*(n+2)).*t;
if t > tmax
tmax = t;
end
n = n+2;
end
operamos:
>> x = (pi)/2;
>> [s,k,tmax]= powersin(x)
t =
1.5708
s =
1.0000
k =
11
tmax =
1.5708
>>
>> x = 11*(pi)/2;
>> [s,k,tmax]= powersin(x)
t =
17.2788
s =
-1.0000
k =
37
tmax =
3.0665e+006
Modificando de nuevo:
function [s,k,tmax,t] = powersin(x)
s = 0;
t = x,
n = 1;
k = 0;
tmax=x;
while s + t ~= s;
k = k +1;
s = s+t;
t = - x.^2/((n+1)*(n+2)).*t;
if t > tmax
tmax = t;
end
n = n+2;
end
Operamos
>> [s,k,tmax,t]= powersin(x)
t =
17.2788
s =
-1.0000
k =
37
tmax =
3.0665e+006
t =
-2.6232e-017
>>
28-marzo-06
Tenemos el programa lutx:
function [L,U,p] = lutx(A)
%LUTX Triangular factorization, textbook version
% [L,U,p] = lutx(A) produces a unit lower triangular matrix L,
% an upper triangular matrix U, and a permutation vector p,
% so that L*U = A(p,:)
[n,n] = size(A);
p = (1:n)';
for k = 1:n-1
% Find index of largest element below diagonal in k-th column
[r,m] = max(abs(A(k:n,k)));
m = m+k-1;
% Skip elimination if column is zero
if (A(m,k) ~= 0)
% Swap pivot row
if (m ~= k)
A([k m],:) = A([m k],:);
p([k m]) = p([m k]);
end
% Compute multipliers
i = k+1:n;
A(i,k) = A(i,k)/A(k,k);
% Update the remainder of the matrix
j = k+1:n;
A(i,j) = A(i,j) - A(i,k)*A(k,j);
end
end
y aplicamos en matlab:
>>A= [0 1;1 0]
A =
0 1
1 0
>> [L,U,p]= lutx(A)
Y:
function [L,U,p,sig] = lutx(A)
%LUTX Triangular factorization, textbook version
% [L,U,p] = lutx(A) produces a unit lower triangular matrix L,
% an upper triangular matrix U, and a permutation vector p,
% so that L*U = A(p,:)
[n,n] = size(A);
p = (1:n)';
sig=1;
for k = 1:n-1
% Find index of largest element below diagonal in k-th column
[r,m] = max(abs(A(k:n,k)));
m = m+k-1;
% Skip elimination if column is zero
if (A(m,k) ~= 0)
% Swap pivot row
if (m ~= k)
A([k m],:) = A([m k],:);
p([k m]) = p([m k]);
sig = -1*sig;
end
% Compute multipliers
i = k+1:n;
A(i,k) = A(i,k)/A(k,k);
% Update the remainder of the matrix
j = k+1:n;
A(i,j) = A(i,j) - A(i,k)*A(k,j);
end
end
% Separate result
L = tril(A,-1) + eye(n,n);
U = triu(A);
Aplicamos::
>> A
A =
0 1
1 0
>> [L,U,p] = lutx(A)
L =
1 0
0 1
U =
1 0
0 1
p =
2
1
>> [L,U,p,sig] = lusigno(A)
> [L,U,p,sig] = lusigno(A)
L =
1 0
0 1
U =
1 0
0 1
p =
2
1
sig =
-1
>> A = [1 2 3;2 1 4;-1 2 1]
A =
1 2 3
2 1 4
-1 2 1
>> [L,U,p,sig] = lusigno(A)
L =
1.0000 0 0
-0.5000 1.0000 0
0.5000 0.6000 1.0000
U =
2.0000 1.0000 4.0000
0 2.5000 3.0000
0 0 -0.8000
p =
2
3
1
sig =
1
>>
Programa:
%Ejercicio 2.7 del libro Moler
%este programa calcula el determinante
%de la matriz A utilizando la factorización
%LU como de A ,PA=LU
%det(A) = +- U(1,1)*U(2,2)*...*U(n,n)
%donde U(i,i) son los elementos de la diagonal
%de la matriz U, y el signo +- es
%+ si el numero de intercambios de filas
%que hemos realizado es par y menos en caso
%contrario. El signo se almacena en la
%variable sig
function d = mideterminante(A)
[L,U,p,sig] = lusigno(A)
Aplico:
>> A
A =
1 2 3
2 1 4
-1 2 1
>> A = [0 1;1 0]
A =
0 1
1 0
>> diag(A)
ans =
0
0
>> X
>> X=diag(A)
X =
0
0
>> B=diag(X)
B =
0 0
0 0
>> X= 1:5
X =
1 2 3 4 5
B =
1 0 0 0 0
0 2 0 0 0
0 0 3 0 0
0 0 0 4 0
0 0 0 0 5
>> mideterminante(A)
ans =
-1
> B=eye(50)
B =
Columns 1 through 12
1 0 0 0 0 0 0 0 0 0 0 0
0 1 0 0 0 0 0 0 0 0 0 0
0 0 1 0 0 0 0 0 0 0 0 0
0 0 0 1 0 0 0 0 0 0 0 0
0 0 0 0 1 0 0 0 0 0 0 0
0 0 0 0 0 1 0 0 0 0 0 0
0 0 0 0 0 0 1 0 0 0 0 0
0 0 0 0 0 0 0 1 0 0 0 0
0 0 0 0 0 0 0 0 1 0 0 0
0 0 0 0 0 0 0 0 0 1 0 0
0 0 0 0 0 0 0 0 0 0 1 0
0 0 0 0 0 0 0 0 0 0 0 1
0 0 0 0 0 0 0 0 0 0 0 0
0 0 0 0 0 0 0 0 0 0 0 0
0 0 0 0 0 0 0 0 0 0 0 0
0 0 0 0 0 0 0 0 0 0 0 0
0 0 0 0 0 0 0 0 0 0 0 0
0 0 0 0 0 0 0 0 0 0 0 0
0 0 0 0 0 0 0 0 0 0 0 0
0 0 0 0 0 0 0 0 0 0 0 0
0 0 0 0 0 0 0 0 0 0 0 0
0 0 0 0 0 0 0 0 0 0 0 0
0 0 0 0 0 0 0 0 0 0 0 0
0 0 0 0 0 0 0 0 0 0 0 0
0 0 0 0 0 0 0 0 0 0 0 0
0 0 0 0 0 0 0 0 0 0 0 0
0 0 0 0 0 0 0 0 0 0 0 0
0 0 0 0 0 0 0 0 0 0 0 0
0 0 0 0 0 0 0 0 0 0 0 0
0 0 0 0 0 0 0 0 0 0 0 0
0 0 0 0 0 0 0 0 0 0 0 0
0 0 0 0 0 0 0 0 0 0 0 0
0 0 0 0 0 0 0 0 0 0 0 0
0 0 0 0 0 0 0 0 0 0 0 0
0 0 0 0 0 0 0 0 0 0 0 0
0 0 0 0 0 0 0 0 0 0 0 0
0 0 0 0 0 0 0 0 0 0 0 0
0 0 0 0 0 0 0 0 0 0 0 0
0 0 0 0 0 0 0 0 0 0 0 0
0 0 0 0 0 0 0 0 0 0 0 0
0 0 0 0 0 0 0 0 0 0 0 0
0 0 0 0 0 0 0 0 0 0 0 0
0 0 0 0 0 0 0 0 0 0 0 0
0 0 0 0 0 0 0 0 0 0 0 0
0 0 0 0 0 0 0 0 0 0 0 0
0 0 0 0 0 0 0 0 0 0 0 0
0 0 0 0 0 0 0 0 0 0 0 0
0 0 0 0 0 0 0 0 0 0 0 0
0 0 0 0 0 0 0 0 0 0 0 0
0 0 0 0 0 0 0 0 0 0 0 0
Columns 13 through 24
0 0 0 0 0 0 0 0 0 0 0 0
0 0 0 0 0 0 0 0 0 0 0 0
0 0 0 0 0 0 0 0 0 0 0 0
0 0 0 0 0 0 0 0 0 0 0 0
0 0 0 0 0 0 0 0 0 0 0 0
0 0 0 0 0 0 0 0 0 0 0 0
0 0 0 0 0 0 0 0 0 0 0 0
0 0 0 0 0 0 0 0 0 0 0 0
0 0 0 0 0 0 0 0 0 0 0 0
0 0 0 0 0 0 0 0 0 0 0 0
0 0 0 0 0 0 0 0 0 0 0 0
0 0 0 0 0 0 0 0 0 0 0 0
1 0 0 0 0 0 0 0 0 0 0 0
0 1 0 0 0 0 0 0 0 0 0 0
0 0 1 0 0 0 0 0 0 0 0 0
0 0 0 1 0 0 0 0 0 0 0 0
0 0 0 0 1 0 0 0 0 0 0 0
0 0 0 0 0 1 0 0 0 0 0 0
0 0 0 0 0 0 1 0 0 0 0 0
0 0 0 0 0 0 0 1 0 0 0 0
0 0 0 0 0 0 0 0 1 0 0 0
0 0 0 0 0 0 0 0 0 1 0 0
0 0 0 0 0 0 0 0 0 0 1 0
0 0 0 0 0 0 0 0 0 0 0 1
0 0 0 0 0 0 0 0 0 0 0 0
0 0 0 0 0 0 0 0 0 0 0 0
0 0 0 0 0 0 0 0 0 0 0 0
0 0 0 0 0 0 0 0 0 0 0 0
0 0 0 0 0 0 0 0 0 0 0 0
0 0 0 0 0 0 0 0 0 0 0 0
0 0 0 0 0 0 0 0 0 0 0 0
0 0 0 0 0 0 0 0 0 0 0 0
0 0 0 0 0 0 0 0 0 0 0 0
0 0 0 0 0 0 0 0 0 0 0 0
0 0 0 0 0 0 0 0 0 0 0 0
0 0 0 0 0 0 0 0 0 0 0 0
0 0 0 0 0 0 0 0 0 0 0 0
0 0 0 0 0 0 0 0 0 0 0 0
0 0 0 0 0 0 0 0 0 0 0 0
0 0 0 0 0 0 0 0 0 0 0 0
0 0 0 0 0 0 0 0 0 0 0 0
0 0 0 0 0 0 0 0 0 0 0 0
0 0 0 0 0 0 0 0 0 0 0 0
0 0 0 0 0 0 0 0 0 0 0 0
0 0 0 0 0 0 0 0 0 0 0 0
0 0 0 0 0 0 0 0 0 0 0 0
0 0 0 0 0 0 0 0 0 0 0 0
0 0 0 0 0 0 0 0 0 0 0 0
0 0 0 0 0 0 0 0 0 0 0 0
0 0 0 0 0 0 0 0 0 0 0 0
Columns 25 through 36
0 0 0 0 0 0 0 0 0 0 0 0
0 0 0 0 0 0 0 0 0 0 0 0
0 0 0 0 0 0 0 0 0 0 0 0
0 0 0 0 0 0 0 0 0 0 0 0
0 0 0 0 0 0 0 0 0 0 0 0
0 0 0 0 0 0 0 0 0 0 0 0
0 0 0 0 0 0 0 0 0 0 0 0
0 0 0 0 0 0 0 0 0 0 0 0
0 0 0 0 0 0 0 0 0 0 0 0
0 0 0 0 0 0 0 0 0 0 0 0
0 0 0 0 0 0 0 0 0 0 0 0
0 0 0 0 0 0 0 0 0 0 0 0
0 0 0 0 0 0 0 0 0 0 0 0
0 0 0 0 0 0 0 0 0 0 0 0
0 0 0 0 0 0 0 0 0 0 0 0
0 0 0 0 0 0 0 0 0 0 0 0
0 0 0 0 0 0 0 0 0 0 0 0
0 0 0 0 0 0 0 0 0 0 0 0
0 0 0 0 0 0 0 0 0 0 0 0
0 0 0 0 0 0 0 0 0 0 0 0
0 0 0 0 0 0 0 0 0 0 0 0
0 0 0 0 0 0 0 0 0 0 0 0
0 0 0 0 0 0 0 0 0 0 0 0
0 0 0 0 0 0 0 0 0 0 0 0
1 0 0 0 0 0 0 0 0 0 0 0
0 1 0 0 0 0 0 0 0 0 0 0
0 0 1 0 0 0 0 0 0 0 0 0
0 0 0 1 0 0 0 0 0 0 0 0
0 0 0 0 1 0 0 0 0 0 0 0
0 0 0 0 0 1 0 0 0 0 0 0
0 0 0 0 0 0 1 0 0 0 0 0
0 0 0 0 0 0 0 1 0 0 0 0
0 0 0 0 0 0 0 0 1 0 0 0
0 0 0 0 0 0 0 0 0 1 0 0
0 0 0 0 0 0 0 0 0 0 1 0
0 0 0 0 0 0 0 0 0 0 0 1
0 0 0 0 0 0 0 0 0 0 0 0
0 0 0 0 0 0 0 0 0 0 0 0
0 0 0 0 0 0 0 0 0 0 0 0
0 0 0 0 0 0 0 0 0 0 0 0
0 0 0 0 0 0 0 0 0 0 0 0
0 0 0 0 0 0 0 0 0 0 0 0
0 0 0 0 0 0 0 0 0 0 0 0
0 0 0 0 0 0 0 0 0 0 0 0
0 0 0 0 0 0 0 0 0 0 0 0
0 0 0 0 0 0 0 0 0 0 0 0
0 0 0 0 0 0 0 0 0 0 0 0
0 0 0 0 0 0 0 0 0 0 0 0
0 0 0 0 0 0 0 0 0 0 0 0
0 0 0 0 0 0 0 0 0 0 0 0
Columns 37 through 48
0 0 0 0 0 0 0 0 0 0 0 0
0 0 0 0 0 0 0 0 0 0 0 0
0 0 0 0 0 0 0 0 0 0 0 0
0 0 0 0 0 0 0 0 0 0 0 0
0 0 0 0 0 0 0 0 0 0 0 0
0 0 0 0 0 0 0 0 0 0 0 0
0 0 0 0 0 0 0 0 0 0 0 0
0 0 0 0 0 0 0 0 0 0 0 0
0 0 0 0 0 0 0 0 0 0 0 0
0 0 0 0 0 0 0 0 0 0 0 0
0 0 0 0 0 0 0 0 0 0 0 0
0 0 0 0 0 0 0 0 0 0 0 0
0 0 0 0 0 0 0 0 0 0 0 0
0 0 0 0 0 0 0 0 0 0 0 0
0 0 0 0 0 0 0 0 0 0 0 0
0 0 0 0 0 0 0 0 0 0 0 0
0 0 0 0 0 0 0 0 0 0 0 0
0 0 0 0 0 0 0 0 0 0 0 0
0 0 0 0 0 0 0 0 0 0 0 0
0 0 0 0 0 0 0 0 0 0 0 0
0 0 0 0 0 0 0 0 0 0 0 0
0 0 0 0 0 0 0 0 0 0 0 0
0 0 0 0 0 0 0 0 0 0 0 0
0 0 0 0 0 0 0 0 0 0 0 0
0 0 0 0 0 0 0 0 0 0 0 0
0 0 0 0 0 0 0 0 0 0 0 0
0 0 0 0 0 0 0 0 0 0 0 0
0 0 0 0 0 0 0 0 0 0 0 0
0 0 0 0 0 0 0 0 0 0 0 0
0 0 0 0 0 0 0 0 0 0 0 0
0 0 0 0 0 0 0 0 0 0 0 0
0 0 0 0 0 0 0 0 0 0 0 0
0 0 0 0 0 0 0 0 0 0 0 0
0 0 0 0 0 0 0 0 0 0 0 0
0 0 0 0 0 0 0 0 0 0 0 0
0 0 0 0 0 0 0 0 0 0 0 0
1 0 0 0 0 0 0 0 0 0 0 0
0 1 0 0 0 0 0 0 0 0 0 0
0 0 1 0 0 0 0 0 0 0 0 0
0 0 0 1 0 0 0 0 0 0 0 0
0 0 0 0 1 0 0 0 0 0 0 0
0 0 0 0 0 1 0 0 0 0 0 0
0 0 0 0 0 0 1 0 0 0 0 0
0 0 0 0 0 0 0 1 0 0 0 0
0 0 0 0 0 0 0 0 1 0 0 0
0 0 0 0 0 0 0 0 0 1 0 0
0 0 0 0 0 0 0 0 0 0 1 0
0 0 0 0 0 0 0 0 0 0 0 1
0 0 0 0 0 0 0 0 0 0 0 0
0 0 0 0 0 0 0 0 0 0 0 0
Columns 49 through 50
0 0
0 0
0 0
0 0
0 0
0 0
0 0
0 0
0 0
0 0
0 0
0 0
0 0
0 0
0 0
0 0
0 0
0 0
0 0
0 0
0 0
0 0
0 0
0 0
0 0
0 0
0 0
0 0
0 0
0 0
0 0
0 0
0 0
0 0
0 0
0 0
0 0
0 0
0 0
0 0
0 0
0 0
0 0
0 0
0 0
0 0
0 0
0 0
1 0
0 1
Pasamos al ejemplo 2.11 del libro de moler capitulo 002 pagina 37.
2.7 lutx, bslashtx, lugui
We have three functions implementing the algorithms discussed in this chapter.
The ¯rst function, lutx, is a readable version of the built-in Matlab function lu.
There is one outer for loop on k that counts the elimination steps. The inner loops
on i and j are implemented with vector and matrix operations, so that the overall
function is reasonably e±cient.
function [L,U,p] = lutx(A)
%LU Triangular factorization
% [L,U,p] = lutx(A) produces a unit lower triangular
% matrix L, an upper triangular matrix U, and a
% permutation vector p, so that L*U = A(p,:).
[n,n] = size(A);
p = (1:n)'
for k = 1:n-1
% Find largest element below diagonal in k-th column
[r,m] = max(abs(A(k:n,k)));
m = m+k-1;
% Skip elimination if column is zero
if (A(m,k) ~= 0)
% Swap pivot row
if (m ~= k)
A([k m],:) = A([m k],:);
p([k m]) = p([m k]);
end
% Compute multipliers
i = k+1:n;
A(i,k) = A(i,k)/A(k,k);
% Update the remainder of the matrix
j = k+1:n;
A(i,j) = A(i,j) - A(i,k)*A(k,j);
end
end
% Separate result
L = tril(A,-1) + eye(n,n);
U = triu(A);
Y la versión simplificada de este operador la llama: Bslashtx(A,b) [backslash]:
function x = bslashtx(A,b)
% BSLASHTX Solve linear system (backslash)
% x = bslashtx(A,b) solves A*x = b
[n,n] = size(A);
if isequal(triu(A,1),zeros(n,n))
% Lower triangular
x = forward(A,b);
return
elseif isequal(tril(A,-1),zeros(n,n))
% Upper triangular
x = backsubs(A,b);
return
elseif isequal(A,A')
[R,fail] = chol(A);
if ~fail
% Positive definite
y = forward(R',b);
x = backsubs(R,y);
return
end
end
Realizamos otro programa para la inversa (ejercicio 2.11 de moler)
%Ejercicio 2.11 del libro de Moler
%este programa nos permite calcular
%la matriz inversa de una matriz
%usando la factorización LU y
%las versiones sencillas de los
%programas LU y \ que nos ofrece
%el libro de Moler
function X = miinversa(A)
[n,n] = size (A);
E = eye(n);
for i=1:n
%x(:,i)=bslashtx(A,E(:,i));
X(:,i)= A\E(:,i);
end
aplicamos en matlab:
A =
0 1
1 0
>> miinversa(A)
ans =
0 1
1 0
>> B=rand(50);
>> X=miinversa(B);
>> norm(B*X - eye(50))
ans =
2.3934e-014
>> X2=inv(B);
>>
>> norm(B*X2 - eye(50))
ans =
1.2760e-013
>> cond(B)
ans =
517.6219
4-abril-06
CAPITULO 3 PDF
A =
1 1 1
1 2 4
1 3 9
>> B= [2;1;3]
B =
2
1
3
>> P = A\B
P =
6.0000
-5.5000
1.5000
>> X= [1;2;3]
X =
1
2
3
>> Y = [2; 1; 3]
Y =
2
1
3
>>plot(X,Y,'r*')
Y obtenemos un gráfico:
>> plot(X,Y,'r*',u,v)
u=0:0.01:4;
>> v= 6 -5.5*u+315*u.^2;
(es el polinomio obtenido antes evaluado en los puntos dados)
>> plot(X,Y,'r*',u,v)
Y obtenemos:
*Tenemos los siguientes programas:
function v = polyinterp(x,y,u)
%POLYINTERP Polynomial interpolation.
% v = POLYINTERP(x,y,u) computes v(j) = P(u(j)) where P is the
% polynomial of degree d = length(x)-1 with P(x(i)) = y(i).
% Use Lagrangian representation.
% Evaluate at all elements of u simultaneously.
n = length(x);
v = zeros(size(u));
for k = 1:n
w = ones(size(u));
for j = [1:k-1 k+1:n]
w = (u-x(j))./(x(k)-x(j)).*w;
end
v = v + w*y(k);
end
número de puntos
Y:
function v = piecelin(x,y,u)
%PIECELIN Piecewise linear interpolation.
% v = piecelin(x,y,u) finds the piecewise linear L(x)
% with L(x(j)) = y(j) and returns v(k) = L(u(k)).
% First divided difference
delta = diff(y)./diff(x);
% Find subinterval indices k so that x(k) <= u < x(k+1)
n = length(x);
k = ones(size(u));
for j = 2:n-1
k(x(j) <= u) = j;
end
% Evaluate interpolant
s = u - x(k);
v = y(k) + s.*delta(k);
>> X= 0:10
X =
0 1 2 3 4 5 6 7 8 9 10
>> Y=rand(1,11);
>> u= -0.1:0.01:10.1;
>> Y = 10*Y;
>> v= polyinterp(X,Y,u);
>> plot(X,Y,'r*',u,v)
Y obtenemos:
>> x=[1 4 5 4 -1 2 0]
x =
1 4 5 4 -1 2 0
>> diff(x)
ans =
3 1 -1 -5 3 -2
>>
>> x
x =
0 1 2 3 4 5 6 7 8
>> y = 10*rand(1,9);
>> y
y =
Columns 1 through 7
4.3866 4.9831 2.1396 6.4349 3.2004 9.6010 7.2663
Columns 8 through 9
4.1195 7.4457
>> u = -1:0.01:9;
>> v = piecelin(x,y,u);
>> plot(x,y,'r*',u,v)
06/04/06
Del capitulo 3pdf la segunda parte.
-
Este es un buen método (el pichip) para interpolar, pero los hay mejores(el splines)
*Los ptos di son “knots”
K=1 d0+4d1+d3 = 31+3 2 eliminada
K=2 d1+4d2+d4=3 2+3 3
K=3 d2+4d3+d5=3 3+3 4
K=4 d1+4d4+d6=3 4+3 5
K=5 d4+4d5+ d7=3 5+3 6 eliminada
.-Si esto no funciona usamos spline, de la cual una versión simplificada es la splinetx.m , que es:
function v = splinetx(x,y,u)
%SPLINETX Textbook spline function.
% v = splinetx(x,y,u) finds the piecewise cubic interpolatory
% spline S(x), with S(x(j)) = y(j), and returns v(k) = S(u(k)).
%
% See SPLINE, PCHIPTX.
% First derivatives
h = diff(x);
delta = diff(y)./h;
d = splineslopes(h,delta);
% Piecewise polynomial coefficients
n = length(x);
c = (3*delta - 2*d(1:n-1) - d(2:n))./h;
b = (d(1:n-1) - 2*delta + d(2:n))./h.^2;
% Find subinterval indices k so that x(k) <= u < x(k+1)
k = ones(size(u));
for j = 2:n-1
k(x(j) <= u) = j;
end
% Evaluate spline
s = u - x(k);
v = y(k) + s.*(d(k) + s.*(c(k) + s.*b(k)));
Ensaya las primeras derivadas
* Implementa alguno de los métodos para hallar las di. (not-a kan ; loked)
De momento esto lo olvidamos
P(x) = s, es el output.
*para ordenar los puntos de manera creciente, en matlab usamos el comando “sort”.
Por ejemplo si tenemos un vector X usamos un comando Y=sort(x), nos aparece un vector ordenado de menor a mayor.
miramos del capitulo 3:
Donde gráficamente reconocemos si una función es o no derivable por las propiedades estudiadas en cálculo.
Seguimos usando el programa splinetx.m y aplicamos en matlab.
*el punto antes de una operación significa, componente a componente.
También usamos el programa splineslopes:
function d = splineslopes(h,delta)
% SPLINESLOPES Slopes for cubic spline interpolation.
% splineslopes(h,delta) computes d(k) = S'(x(k)).
% Uses not-a-knot end conditions.
% Diagonals of tridiagonal system
n = length(h)+1;
a = zeros(size(h)); b = a; c = a; r = a;
a(1:n-2) = h(2:n-1);
a(n-1) = h(n-2)+h(n-1);
b(1) = h(2);
b(2:n-1) = 2*(h(2:n-1)+h(1:n-2));
b(n) = h(n-2);
c(1) = h(1)+h(2);
c(2:n-1) = h(1:n-2);
% Right-hand side
r(1) = ((h(1)+2*c(1))*h(2)*delta(1)+h(1)^2*delta(2))/c(1);
r(2:n-1) = 3*(h(2:n-1).*delta(1:n-2)+h(1:n-2).*delta(2:n-1));
r(n) = (h(n-1)^2*delta(n-2)+(2*a(n-1)+h(n-1))*h(n-2)*delta(n-1))/a(n-1);
% Solve tridiagonal linear system
d = tridisolve(a,b,c,r);
Usa una matriz tri-diagonal (con tres diagonales) y se soluciona gracias a tridisolve
Tridiagonal:
Trisolve(a,b,c,r)
Ax = r
x = A \ r
las condiciones descritas en nuestro ejemplo “not-a-knot”
Para la primera ecuación: h2d1+h2+a1d2 = … = (hn-1+hn-2)dn-1+hn-2*dn= …
Del capitulo 3 del libro de Mooler, página 22 :
3.11. Modify splinetx and pchiptx so that, if called with two output arguments,
they produce both the value of the interpolant and its ¯rst derivative. That
is,
[v,vprime] = pchiptx(x,y,u)
and
[v,vprime] = splinetx(x,y,u)
compute P(u) and P0(u).
[v,v1,v2,v3] = splintex4(x,y,n)
Creamos un nuevo programa a partir del splintex:
%Este programa resuelve el problema 3.11
% del libro de mooler(modificado)
function [v,v1,v2,v3] = splinetx3(x,y,u)
%SPLINETX Textbook spline function.
% v = splinetx(x,y,u) finds the piecewise cubic interpolatory
% spline S(x), with S(x(j)) = y(j), and returns v(k) = S(u(k)).
% and the first, second and third derivatives
%v1 , v2, v3.
% See SPLINE, PCHIPTX.
% First derivatives
h = diff(x);
delta = diff(y)./h;
d = splineslopes(h,delta);
% Piecewise polynomial coefficients
n = length(x);
c = (3*delta - 2*d(1:n-1) - d(2:n))./h;
b = (d(1:n-1) - 2*delta + d(2:n))./h.^2;
% Find subinterval indices k so that x(k) <= u < x(k+1)
k = ones(size(u));
for j = 2:n-1
k(x(j) <= u) = j;
end
% Evaluate spline and its three first derivatives.
s = u - x(k);
v = y(k) + s.*(d(k) + s.*(c(k) + s.*b(k)));
v1= d(k) +s.*(2*c(k)) + 3*s.*(b(k));
v2= 2+c(k)+6*s.*b(k);
v3= 6*b(k);
%-----------------------------------------------------------------------
En command window:
>> x = [1 1.5 3 4.5 7 8.1 9.2 10]
x =
Columns 1 through 7
1.0000 1.5000 3.0000 4.5000 7.0000 8.1000 9.2000
Column 8
10.0000
>> y = [2 -3 4 6 2.3 4 -1 3 6 8]
y =
Columns 1 through 7
2.0000 -3.0000 4.0000 6.0000 2.3000 4.0000 -1.0000
Columns 8 through 10
3.0000 6.0000 8.0000
>> format short
>> x
x =
Columns 1 through 7
1.0000 1.5000 3.0000 4.5000 7.0000 8.1000 9.2000
Column 8
10.0000
>> u = 0.5:0.01:10.5;
>> [v,v1,v2,v3]=splinetx3(x,y,u)
>> [v,v1,v2,v3]=splinetx3(x,y,u);
>> plot(x,y,'r*',u,v2,'g',u,v3,'c')
>> plot(x,y,'r*',u,v,'r*',u,v1,'b',u,v2,'g',u,v3,'c')
Teniamos que tener el programa triidsolve:
function x = tridisolve(a,b,c,d)
% TRIDISOLVE Solve tridiagonal system of equations.
% x = TRIDISOLVE(a,b,c,d) solves the system of linear equations
% b(1)*x(1) + c(1)*x(2) = d(1),
% a(j-1)*x(j-1) + b(j)*x(j) + c(j)*x(j+1) = d(j), j = 2:n-1,
% a(n-1)*x(n-1) + b(n)*x(n) = d(n).
%
% The algorithm does not use pivoting, so the results might
% be inaccurate if abs(b) is much smaller than abs(a)+abs(c).
% More robust, but slower, alternatives with pivoting are:
% x = T\d where T = diag(a,-1) + diag(b,0) + diag(c,1)
% x = S\d where S = spdiags([[a; 0] b [0; c]],[-1 0 1],n,n)
x = d;
n = length(x);
for j = 1:n-1
mu = a(j)/b(j);
b(j+1) = b(j+1) - mu*c(j);
x(j+1) = x(j+1) - mu*x(j);
end
x(n) = x(n)/b(n);
for j = n-1:-1:1
x(j) = (x(j)-c(j)*x(j+1))/b(j);
end
cambiamos le valor de y:
>> y = [0 2 4 -1 -3 0 4 8 9 9];
>> u=0.9:0.01:10.1;
>> [v,v1,v2,v3] = splinetx3(x,y,u);
>> plot(x,y,'r*',u,v,'r*',u,v1,'b',u,v2,'g',u,v3,'c')
Mirar problem3.11
Mirar problem 3.9
18-ABRIL-06
<<Chapter 4>>
Teorema de los ceros de Bolzano.
*en matlab el poner ó es lo mismo que poner =.
En los apuntes:
Given a,b,f(a),f(b),e
while |b-a|>e|b|
x=a+b/2
if f(x) = 0 then
end
if f(x)f(a)<0 then
b=x
else
a=x
end
end
Hacemos un programa para hala ceros con el método de la bisección:
%este programa calcula los ceros
%de una función f(x) por el
%método de la bisección
%Inputs a,b,e
%a,b extremos del intervalo
%e error relativo admisible
% la función f(x) se escribe
%en un fichero auxiliar de nombre
%fun.m
function c = bisec(a,b,e)
fa = feval(`fun',a);
fb = feval(`fun',b);
while abs(b-a) > e*abs(b)
c = (a+b)/2;
fc = feval(`fun',c);
if fc == 0
break
end
if fc*fa < 0
b = c;
else
a = c;
end
end
y otro programa:
% este fichero sirve para almacenar la función
%f(x)
function y = fun(x)
y = sin(x.^2)-x.^3;
En matlab:
>> c = feval('fun',0)
c =
0
>> feval('fun',3)
ans =
-26.5879
>>>> sin(3^2)-3^3
ans =
-26.5879
>>>> feval('fun',8)
ans =
-511.0800
>> feval('fun',0.1)
ans =
0.0090
>> feval('fun',0)
ans =
0
>> c= bisec(0.1,3,10^-6)
c =
0.8960
>> format long
>> c= bisec(0.1,3,10^-6)
c =
0.89599368572235
Modificamos el primer programa:
%este programa calcula los ceros
%de una función f(x) por el
%método de la bisección
%Inputs a,b,e
%a,b extremos del intervalo
%e error relativo admisible
% la función f(x) se escribe
%en un fichero auxiliar de nombre
%fun.m
function [c,k] = bisec(a,b,e)
k=0;
fa = feval('fun',a);
fb = feval('fun',b);
while abs(b-a) > e*abs(b)
k = k+1;
c = (a+b)/2;
fc = feval('fun',c);
if fc == 0
break
end
if fc*fa < 0
b = c;
else
a = c;
end
end
modificamos también el segundo:
% este fichero sirve para almacenar la función
%f(x)
function y = fun(x)
y = x.^3 - 2.000001*x.^2+1.000002*x - 0.000001;
>> feval('fun',-10)
ans =
-1.210000121000000e+003
>> feval('fun',10)
ans =
8.099999190000000e+002
>> c = bisec(-10,10,10^-6)
c =
1.000000224848918e-006
>> u = -2:0.01:2;
>> v = feval('fun',u);
>> plot(u,v)
>> z= 0*u;
>> plot(u,v,u,z,'k')
>> c = bisec(-1,0.5,10^-12)
c =
1.000000000000350e-006
>> c = bisec(-1,0.5,10^-13)
c =
9.999999999999430e-007
>> c = bisec(-1,0.5,10^-14)
c =
9.999999999999989e-007
>> c = bisec(-1,0.5,10^-15)
c =
9.999999999999995e-007
>> c = bisec(-1,0.5,10^-16)
c =
1.000000000000000e-006
>> u = 0.5:0.001:1.5;
>> z= 0*u;
>> v = feval('fun',u);
>> plot(u,v,u,z,'k')
>>
>> feval('fun',1)
ans =
-8.226659269441623e-017
>>
Otro método es: EL MÉTODO DE NEWTON
Creamos el programa newton:
%Este programa obtiene los
%ceros de la función f(x)
% por el método de Newton
%Inputs: x0 (punto de partida),e (error relativo)
%Necesitamos dos ficheros auxiliares:
% - fun.m (donde guardamos la función f(x))
% - derfun.m (donde almacenamos la derivada
%f'(x) de la función f(x))
function [c,k] = newton(a,e)
k=0;
b=a;
fa=feval('fun',a);
dfa=feval('derfun',a);
c=a-fa/dfa;
while abs(c-b) > e*abs(b)
a=c;
b=a;
k = k+1;
fa = feval ('fun',a);
dfa=feval('derfun',a);
c= a-fa/dfa;
end
creamos el programa derfun:
%este fichero contiene la derivada de la función
%f(x) que esta guardada en el fichero fun.m
function dy = derfun(x)
%la otra función que usabamos era: dy = 2*cos (x.^2).*x-3*x.^2;
dy = 3*x^2-2*2.000001*x+1.000002;
20-abril-06
+página 10 del capítulo 5
Fix point method
(puntos fijos)
El algoritmo de punto fijo dice:
Dados x y e mientras que |g(x) -x | > |x|:
Given x
While |g(x) -x | > |x|
X g(x)
End
***** Creamos un programa llamado fijo.m: *******
%este programa calcula los puntos
%fijos de la función g(x)
% g(x*) = x*
% la función g(x) esta almacenada en el fichero fun.m
%inputs: dato inicio x0, error relativo (epsilon)
% outputs: punto fijo x*, numero de iteraciones k
function [x,k] = fijo(x0,e)
k = 0;
x= x0;
gx = feval('fun',x);
% en feval('fun',x); evalua g(x)
while abs( gx - x) > e*abs(x)
x = gx;
gx=feval('fun',x);
k = k+1;
end
y el programa:
function y = fun(x)
y = cos(x);
y ejecuto en matlab:
>> [x,k]=fijo (0,10^-6)
x =
0.7391
k =
35
Y con el programa derfun Nuevo:
%este fichero contiene la derivada de la función
%f(x) que esta guardada en el fichero fun.m
function dy = derfun(x)
%la otra función que usabamos era: dy = 2*cos (x.^2).*x-3*x.^2;
%dy = 3*x^2-2*2.000001*x+1.000002;
dy = -sin(x)-1;
en matlab:
>> [x,k] = newton(0.1,10^-6)
x =
0.7391
k =
4
26-abril-06
+apuntes libro moler pagina zero página 20 en adelante
Con los programas:
derfun:
function dy = dfun(x)
% y = cos(x);
dy = 3*x^2-2 -5;
y:
fun:
function y = fun(x)
%y = cos(x)-x;
y = x.^3-2.*x-5;
En matlab:
>> u = 0:0.01:3;
>> v = fun(u);
>> z=0*u;
>> plot(u,v,u,z,'k');
>>
>> [c,k] = bisec(0,3,eps)
c =
2.0946
k =
53
>> [c,k] = newton(0,eps)
c =
2.0946
k =
19
>>
Donde bisec:
%Este programa calcula los ceros de una funcion f(x)
%por el metodo de la biseccion
%e error relativo admisible
%la funcion f(x) se escribe en un fichero auxiliar
%con el nombre fun.m
function [x,p] = bisec(a,b,e)
fa = feval('fun',a); %feval evalua la funcion en el punto dado
fb = feval('fun',b);
p = 0;
while abs(b-a) > e*abs(b)
p = p+1;
x = (a+b)/2;
fx = feval('fun',x);
if fx == 0
break
end
if fx*fa < 0
b = x;
else a = x;
end
end
Donde newton:
%Este programa obtiene los ceros de la funcion f(x)
%por el metodo de Newton
%x0 = punto de partida, e = error relativo
%necesitamos dos ficheros auxiliares
%fun.m(donde guardamos la funcion f(x)
%derfun.m(donde almacenamos la derivada
%f'(x) de la funcion f(x)
function [c,k] = newton(x,e)
k = 0;
b = x;
fx = feval('fun',x);
dfx = feval('derfun',x);
c = x - fx/dfx;
while abs(c-b) > e*abs(b);
x = c;
b = x;
k = k+1;
fx = feval('fun',x);
dfx = feval('derfun',x);
c = x-fx/dfx;
end
la nueva function derfun:
function dy = derfun(x)
% y = cos(x);
dy = 1./(1+x.^2);
>> [c,k] = newton(0,eps)
c =
1.7321
k =
6
>>
Ahora la funcion fun:
function y = fun(x)
y = sign(x-2).*sqrt(abs(x-2));
>> v = fun(u);
>> u = 0:0.01:4;
>> v = fun(u);
>> z=0*u;
>> plot(u,v,u,z,'k');
Ahora derfun:
function dy = derfun(x)
% y = cos(x);
%dy = 1./(1+x.^2);
dy = 1./(2*sqrt(abs(x-2)));
>> [c,k] = bisec(0,4,eps)
c =
2
k =
1
>>
>> v = fun(u);
>> u = 0:0.01:4;
>> v = fun(u);
>> z=0*u;
>> plot(u,v,u,z,'k');
>> [c,k] = bisec(0,4,eps)
c =
2
k =
1
[c,k] = newton (0,eps)
>> u = -20:0.01:20;
>> v = besselj(0,u);
>> z=0*u;
>> plot(u,v,u,z,'k');
Warning: Imaginary parts of complex X and/or Y arguments ignored.
>>
>> u = 0:0.01:20;
>> v = besselj(0,u);
>> z=0*u;
>> plot(u,v,u,z,'k');
>> u = 0:0.01:40;
>> v = besselj(0,u);
>> z=0*u;
>> plot(u,v,u,z,'k');
>> u = -69:0.01:69;
>> v = besselj(0,u);
>> z=0*u;
>> plot(u,v,u,z,'k');
Cambio fun:
function y = fun(x)
%y = cos(x)-x;
%y = x.^3-2.*x-5;
%y = atan(x)-pi/3;
%y = sign(x-2).*sqrt(abs(x-2));
y = besselj(0,x);
y creo el problema 4 el programa:
% este pequeño programa (script)
%resuelve el problema 4.10
% del libro de mooler, buscamos
%los 10 primeros ceros de la función
% de Bessel de primera especie
%de orden 0, J_0(x),
%Para ello usamos el metodo de la bisección
%aplicado a los intervalos [1,4],
% [4,7],...,[29,32]
%Los intervalos los hemos obtenido
%por inspección representando graficamente
%la función.
x = [1 4 7 10 13 17 20 24 27 29 32];
c = zeros(10,1);
for n = 1:10
c(n) = bisec(x(n),x(n+1),eps)
end
*que no lleva function porque no tiene inputs
>> problem4_10
c =
2.4048
0
0
0
0
0
0
0
0
0
c =
2.4048
5.5201
0
0
0
0
0
0
0
0
c =
2.4048
5.5201
8.6537
0
0
0
0
0
0
0
c =
2.4048
5.5201
8.6537
11.7915
0
0
0
0
0
0
c =
2.4048
5.5201
8.6537
11.7915
14.9309
0
0
0
0
0
c =
2.4048
5.5201
8.6537
11.7915
14.9309
18.0711
0
0
0
0
c =
2.4048
5.5201
8.6537
11.7915
14.9309
18.0711
21.2116
0
0
0
c =
2.4048
5.5201
8.6537
11.7915
14.9309
18.0711
21.2116
24.3525
0
0
c =
2.4048
5.5201
8.6537
11.7915
14.9309
18.0711
21.2116
24.3525
27.4935
0
c =
2.4048
5.5201
8.6537
11.7915
14.9309
18.0711
21.2116
24.3525
27.4935
30.6346
>> besselj(0,c(1))
ans =
0
>>
09/05/06
Capitulo 5 Last squares (minimos cuadrados)
Recordamos:
Reales(n) Complejos(n)
( , ) < , >
Linealidad:
< x, y+z > = <x,y> + <x,z>
<x,By> = B <x,y>
<x,x> mayor o igual que cero, <x,y> + <x,z>
<x,y> = 1/ <x,y>
(x,y) = xT * y ; <x,y> = media(xT) * y
[ e1,e2,…,en] ortonormal
<ei,ej> = dij = 1 si i = j; 0 si i distinto de j
En matlab:
>> Y = [-1,3,0];
>> X=[1,2,3];
>> X*Y'
ans =
5
>> X=[i,-1,0]
X =
0 + 1.0000i -1.0000
X =
0 + 1.0000i -1.0000 0
>> Y = [-2; sqrt(2) + i; 1]
Y =
-2.0000
1.4142 + 1.0000i
1.0000
y =
-2.0000
1.4142 + 1.0000i
1.0000
>> Y'*Y
ans =
8
>> X= [i;-1;0]
X =
0 + 1.0000i
-1.0000
0
>> X'*X
ans =
2
>> X'*Y
ans =
-1.4142 + 1.0000i
>> norm(X)
ans =
1.4142 (es raís de2)
>> norm(Y)
ans =
(es raíz de8)
*tenemos un vector fila: (v1,….,vn) no ortonormal
aplicamos Grand Smith (q1,…,qn) ortonormal
<qi,qj> = dij
Peo no nos sirve Grand Smith, asi que usamos otros métodos. En matlab tenemos la factorización de QR.
Es decir: tenemos = |v1|, … |vn| qr Q 0 |q1|,…|qn|
En matlab:
>> A= rand(4)
A =
0.9501 0.8913 0.8214 0.9218
0.2311 0.7621 0.4447 0.7382
0.6068 0.4565 0.6154 0.1763
0.4860 0.0185 0.7919 0.4057
>> rank(A)
ans =
4
>>> v1 = A(:,1)
v1 =
0.9501
0.2311
0.6068
0.4860
>> v2 = A(:,2)
v2 =
0.8913
0.7621
0.4565
0.0185
>> v3 = A(:,3)
v3 =
0.8214
0.4447
0.6154
0.7919
>> v4 = A(:,4)
v4 =
0.9218
0.7382
0.1763
0.4057
>> v2'*v3
ans =
1.3666
>> v1'*v4
ans =
1.3506
>> [Q,R]= qr(A)
Q =
-0.7606 -0.1354 0.4523 0.4457
-0.1850 -0.8151 -0.5489 -0.0062
-0.4858 0.0754 0.0617 -0.8686
-0.3890 0.5582 -0.7002 0.2163
R =
-1.2492 -1.0478 -1.3141 -1.0811
0 -0.6971 0.0148 -0.4867
0 0 -0.3892 -0.2615
0 0 0 0.3409
q3 =
0.4523
-0.5489
0.0617
-0.7002
>> q4=Q(:,4)
q4 =
0.4457
-0.0062
-0.8686
0.2163
>> q1 =
-0.7606
-0.1850
-0.4858
-0.3890
>> q2=Q(:,2)
q2 =
-0.1354
-0.8151
0.0754
0.5582
>> q2'*q3
ans =
5.5511e-017
>> q1'*q4
ans =
1.3878e-017
>> q1'*q1
ans =
1.0000
>> q4'*q4
ans =
1.0000
*perpendicular X e Y : X_|_ Y
En los apuntes:
Classical Gram-Schmidt algorithm:
for j = 1:n
vj = aj
for k = 1:j-1
rjk = aj*qk
vj= vj - rjk qk
end
rjj = ||vj||
qj = vj/rjj
end
Exercise: Study the numerical stability of the
classical GS algorithm.
Exercise: Modify the classical GS algorithm
to correct its numerical unstability.
Gram-Schmidt
orthogonallization method:
Initial basis B = {ai }
ui ð
vi
ri
, ri
2
= vi ,vi
vi ð ai ð ai ,uk uk
kð1
ið1
ð
Classical Gram-Schmidt algorithm:
for j = 1:n
vj = aj
for k = 1:j-1
rjk = aj*qk
vj= vj - rjk qk
end
rjj = ||vj||
qj = vj/rjj
end
Exercise: Study the numerical stability of the
classical GS algorithm.
Exercise: Modify the classical GS algorithm
to correct its numerical unstability.
QR factorization:
A = QR
Q = [u1 u2 … un] orthogonal matrix
R = [Rij] upper triangular matrix
Tengo los siguientes programas:
Demo_ortog:
% This script explores the lost of orthogonality
% due to the intrinsic numerical unstability
% of the classical and
% modified Gram-Schmidt algorithms.
clc
disp(' Losing orthogonality on Gram-Schmidt algorithms ')
disp(' delta Error on QR Error on CGS Error on MGS ')
disp('------------------------------------------------------------------------')
for delta = logspace(-4,-16,7)
A = [1+delta 2;1 2];
[Q1,R1]= qr(A);
[Q2,R2]= cgs(A);
[Q3,R3]= mgs(A);
error1 = norm(Q1'*Q1 - eye(2));
error2 = norm(Q2'*Q2 - eye(2));
error3 = norm(Q3'*Q3 - eye(2));
disp(sprintf(' %5.0e %20.15f %20.15f %20.15f ', delta,error1,error2,error3))
end
cgs:
% Gram-Schmidt orthogonalization (unstable)
function [Q,R] = cgs(A)
n = length(A);
% starting variables
R = zeros(n,n);
Q = zeros(n,n);
V = zeros(n,n);
% Normalizing the first column vector A
R(1,1)=norm(A(:,1));
Q(:,1)= A(:,1)/R(1,1);
% Classical Gram-Schmidt
for j = 2:n
V(:,j) = A(:,j);
for i = 1:j-1
R(i,j) = Q(:,i)'*A(:,j);
V(:,j)= V(:,j)-R(i,j)*Q(:,i);
end
R(j,j)=norm(V(:,j));
Q(:,j)=V(:,j)/R(j,j);
end
Q;
R;
Mgs:
% Modified Gram-Schmidt algorithm (stable)
function [Q,R] = mgs(A)
[m,n] = size(A);
% Initializating variables
R = zeros(m,n);
S = zeros(m,m);
Q = zeros(m,m);
V = [A floor(10*rand(m,m-n))];
for i = 1:n
R(i,i)=norm(V(:,i));
Q(:,i)=V(:,i)/R(i,i);
for j = i+1:n
R(i,j) = Q(:,i)'*V(:,j);
V(:,j)= V(:,j)-R(i,j)*Q(:,i);
end
end
for i = n+1:m
S(i,i)=norm(V(:,i));
Q(:,i)=V(:,i)/S(i,i);
for j = i+1:n
S(i,j) = Q(:,i)'*V(:,j);
V(:,j)= V(:,j)-S(i,j)*Q(:,i);
end
end
Q;
R;
En matlab:
Demo_ortog
Losing orthogonality on Gram-Schmidt algorithms
delta Error on QR Error on CGS Error on MGS
------------------------------------------------------------------------
1e-004 0.000000000000000 0.000000000002109 0.000000000002109
1e-006 0.000000000000001 0.000000000399139 0.000000000399139
1e-008 0.000000000000000 0.000000028306691 0.000000028306691
1e-010 0.000000000000000 0.000003330622496 0.000003330622496
1e-012 0.000000000000000 0.000444049689291 0.000444049689291
1e-014 0.000000000000000 0.032949132854297 0.032949132854297
1e-016 0.000000000000000 1.000000000000000 1.000000000000000
>> A= [1 + 10^-14 2;1 2]
A =
1.0000 2.0000
1.0000 2.0000
>> format long
>> A= [1 + 10^-14 2;1 2]
A =
1.00000000000001 2.00000000000000
1.00000000000000 2.00000000000000
>> [Q,R] = cgs(A)
Q =
0.70710678118655 -0.68342428808113
0.70710678118654 0.73002139863212
R =
1.41421356237310 2.82842712474619
0 0.00000000000001
>> q1=Q(:,1)
q1 =
0.70710678118655
0.70710678118654
>> q2=Q(:,2)
q2 =
-0.68342428808113
0.73002139863212
>> q1'*q1
ans =
1.00000000000000
>> q2'*q2
ans =
1.00000000000000
>> q1'*q2
ans =
0.03294913285430
>> plot(q1(1),q1(2),'r*',q2(1),q2(2),'b*')
>> plot(q1(1),q1(2),'r*',q2(1),q2(2),'b*',0,0,'k*')
*nota : hemos añadido un punto en el (0,0)
Con el programa demo_cgs_mgs.m:
% Numerical comparison:
% Classical Gram-Schmidt and
% modified Gram-Schmidt
% First we generate a random matrix A
% with eigenvalues spaced by a factor 2
% between 2^-1 and 2^-80
[U,X]= qr(randn(80));
S = diag(2.^(-1:-1:-80));
A = U*S*U';
E = eig(A);
% We use now classical Gram-Schmid cgs(A)
% and modified Gram-Schmidt mgs(A) to compute Q and R
[Q1,R1]=cgs(A);
[Q2,R2]=mgs(A);
% We represent the diagonal R elements
% in logarithmic scale for both matrices R1 and R2.
x = 1:80;
y1 = log2(diag(R1));
y2 = log2(diag(R2));
y6 = log2(-sort(-abs(E)));
y3 = -23*ones(1,80);
y4 = -55*ones(1,80);
y5 = -x;
plot(x,y1,'bo',x,y2,'rx',x,y6,'g*',x,y3,':',x,y4,':',x,y5,'-');
xlabel('R(i,i) elements in logarithmic scale');
en matlab:
>> demo_cgs_mgs
>> 2^-55
ans =
2.775557561562891e-017
11-05-06
AX = B
A = Q * R = triángular superior
Q columnas (ó filas) son una base ortonormal, se llama ortogonal.
Q' * Q = Q * Q' = I
Q' Q RX = Q' B ; como Q' Q = I RX = Q' B
5. Singular value decomposition
(Página 7 del capitulo 5)
A = Q R = U S V'
Donde S es diagonal, y U y V' ortgonales
|s1 0 |
S = | s2 |
| 0 s3 |
Real Ortgonal
Compleja Unitaria
Ambas tmatrices tienen las columnas en bases ortonormales.
En marlab sería: >> [u,s,v] = svd(A) s1>>s2>>…>>sn
Hacemos en matlab:
>> help svd
SVD Singular value decomposition.
[U,S,V] = SVD(X) produces a diagonal matrix S, of the same
dimension as X and with nonnegative diagonal elements in
decreasing order, and unitary matrices U and V so that
X = U*S*V'.
S = SVD(X) returns a vector containing the singular values.
[U,S,V] = SVD(X,0) produces the "economy size"
decomposition. If X is m-by-n with m > n, then only the
first n columns of U are computed and S is n-by-n.
For m <= n, SVD(X,0) is equivalent to SVD(X).
[U,S,V] = SVD(X,'econ') also produces the "economy size"
decomposition. If X is m-by-n with m >= n, then it is
equivalent to SVD(X,0). For m < n, only the first m columns
of V are computed and S is m-by-m.
See also svds, gsvd.
Overloaded functions or methods (ones with the same name in other directories)
help sym/svd.m
Reference page in Help browser doc svd
>> A = rand(3)
A =
0.9501 0.4860 0.4565
0.2311 0.8913 0.0185
0.6068 0.7621 0.8214
>> [u,s,v]= svd(A)
u =
-0.6068 0.4443 -0.6591
-0.4007 -0.8871 -0.2290
-0.6865 0.1251 0.7163
s =
1.8109 0 0
0 0.6319 0
0 0 0.3748
v =
-0.5995 0.4637 -0.6523
-0.6489 -0.7587 0.0572
-0.4684 0.4576 0.7558
>> >> u*u'
ans =
1.0000 0 -0.0000
0 1.0000 0.0000
-0.0000 0.0000 1.0000
>> A - u*s*v'
ans =
1.0e-015 *
0.1110 -0.3886 0.1110
-0.3608 0 -0.3192
-0.3331 -0.6661 -0.1110
>> norm(A - u*s*v')
ans =
8.2930e-016
>> A = [1 0 0; 0 0 1; 1 1 1]
A =
1 0 0
0 0 1
1 1 1
>> spy(A)
>> A = [1 1 1 1; 1 1 1 1; 1 1 0 0; 1 1 1 1;1 1 0 0;1 1 1 1 ;1 1 1 1]
A =
1 1 1 1
1 1 1 1
1 1 0 0
1 1 1 1
1 1 0 0
1 1 1 1
1 1 1 1
>> spy(A)
En editor:
function L = letterL
L = [1 1 0 0 0 0;
1 1 0 0 0 0;
1 1 0 0 0 0;
1 1 0 0 0 0;
1 1 0 0 0 0;
1 1 0 0 0 0;
1 1 1 1 1 1;
1 1 1 1 1 1];
function O = letterO
O = [1 1 1 1 1 1;
1 1 1 1 1 1;
1 1 0 0 1 1;
1 1 0 0 1 1;
1 1 0 0 1 1;
1 1 0 0 1 1;
1 1 1 1 1 1;
1 1 1 1 1 1];
function E = letterE
E = [1 1 1 1 1 1;
1 1 1 1 1 1;
1 1 1 0 0 0;
1 1 1 1 1 1;
1 1 1 1 1 1;
1 1 1 0 0 0;
1 1 1 1 1 1 ;
1 1 1 1 1 1];
function H = letterH
H = [1 1 0 0 1 1;
1 1 0 0 1 1;
1 1 0 0 1 1;
1 1 1 1 1 1;
1 1 1 1 1 1;
1 1 0 0 1 1;
1 1 0 0 1 1;
1 1 0 0 1 1];
Hacemos el programa:
%este script nos escribe la palabra "HELLO"
% por una matriz formada con 1 y 0
function h = hello
h = zeros(12,42);
h(3:10,3:8)= h(3:10,3:8) + letterH;
h(3:10,11:16)= h(3:10,11:16) + letterE;
h(3:10,19:24)= h(3:10,19:24) + letterL;
h(3:10,27:32)= h(3:10,27:32) + letterL;
h(3:10,35:40)= h(3:10,35:40) + letterO;
>> spy(hello)
>> [U,S,V]= svd(hello);
>> diag(S)
ans =
12.0087
3.7201
2.1501
1.8247
0.0000
0.0000
0.0000
0.0000
0
0
0
0
>> pcolor(hello)
U1 =
0 0 0 0
0 0 0 0
-0.3598 -0.0869 0.1134 0.5917
-0.3598 -0.0869 0.1134 0.5917
-0.2923 -0.2906 -0.5635 -0.1124
-0.3483 -0.3132 0.4093 -0.3362
-0.3483 -0.3132 0.4093 -0.3362
-0.2923 -0.2906 -0.5635 -0.1124
-0.4047 0.5567 -0.0461 -0.1555
-0.4047 0.5567 -0.0461 -0.1555
0 0 0 0
0 0 0 0
>> V1 =V(:,1:4);
>> S1= S(1:4,1:4);
>> S1
S1 =
12.0087 0 0 0
0 3.7201 0 0
0 0 2.1501 0
0 0 0 1.8247
>> hello = U1*S1*V1';
>> pcolor(hello)
>> U2 = U(:,1:2);
>> V2 =V(:,1:2);
>> S2= S(1:2,1:2);
>> hello3 = U2*S2*V2'
16/05/06
(Tema 6)
CHAPTER 6. Quadratures
Tenemos el programa PesosNC:
% Este fichero almacena los
% pesos de las reglas de
% cuadratura de Newton-Cotes
% con m puntos
%
% m es un entero que satisface 2 <= m <= 11
%
% p es un vector columna que contiene
% los pesos para la regla de cuadratura
% de Newton-Cotes con m puntos.
%
function p = pesosNC(m);
if m==2
p=[1 1]'/2;
elseif m==3
p=[1 4 1]'/6;
elseif m==4
p=[1 3 3 1]'/8;
elseif m==5
p=[7 32 12 32 7]'/90;
elseif m==6
p=[19 75 50 50 75 19]'/288;
elseif m==7
p=[41 216 27 272 27 216 41]'/840;
elseif m==8
p=[751 3577 1323 2989 2989 1323 3577 751]'/17280;
elseif m==9
p=[989 5888 -928 10496 -4540 10496 -928 5888 989]'/28350;
elseif m==10
p=[2857 15741 1080 19344 5778 5778 19344 1080 15741 2857]'/89600;
else
p=[16067 106300 -48525 272400 -260550 427368 -260550 272400 -48525 106300 16067]'/598752;
end;
regla se simpson
en matlab:
>> pesosnc(3)
ans =
0.1667
0.6667
0.1667
>> pesosnc(5)
ans =
0.0778
0.3556
0.1333
0.3556
0.0778
Con el programa simpson:
% This function computes the
% Simpson quadrature rule for
% computing the integral of f(x) on
% the interval [a,b]
function I = simpson(fname,a,b)
fa = feval(fname,a);
fm = feval(fname, (a+b)/2);
fb = feval(fname, b);
I = ( fa + 4*fm + fb)*(b-a)/6;
Y el programa fname:
%
function y = fname(x)
y = 2 - 3*x + 4*x.^2;
En matlab:
>> I = simpson('fname',1,4)
I =
67.5000
Cambiamos el programa:
%
function y = fname(x)
%y = 2 - 3*x + 4*x.^2;
y = 1 - x.^4;
>> I = simpson('fname',0,2)
I =
-4.6667
>> 22/5
ans =
4.4000
Otro programa: simpsoncom:
% This function computes
% the Simpson composite quadrature rule
% with n subintervals
function I = simpsoncom(fname,a,b,n);
h = (b-a)/n;
x = [a:h:b];
f = feval(fname, x);
I = 0;
for k = 1:n
I = I + simpson('fname',x(k),x(k+1));
End
Y cuadraturaNC:
% Este fichero calcula la cuadratura
% de Newton-Cotes de la funcion fname
% con m puntos y extremos del intervalo a y b.
% a,b numeros reales
% m entero entre 2 <= m <=11
% El computo devuelve el numero I
%
function I = cuadraturaNC(fname,a,b,m)
p = pesosNC(m);
%x = linspace(a,b,m)';
h = (b-a)/(m-1);
x = (a:h:b)';
f = feval(fname,x);
I = (b-a)*(p'*f);
>> I = cuadraturaNC('fname',0,2,3)
Warning: Function call pesosNC invokes inexact match E:\computacion estadistica\16-05-06\pesosnc.m.
> In cuadraturaNC at 9
I =
-4.6667
>> I = cuadraturaNC('fname',0,2,4)
I =
-4.5185
>> I = cuadraturaNC('fname',0,2,5)
I =
-4.40000000000000
>> 22/5
ans =
4.40000000000000
Cambiamos fname:
%
function y = fname(x)
%y = 2 - 3*x + 4*x.^2;
%y = 1 - x.^4;
y = sin(x);
>> I = cuadraturaNC('fname',0,pi,3)
I =
2.09439510239320
>> I = cuadraturaNC('fname',0,pi,5)
I =
1.99857073182384
>> I = cuadraturaNC('fname',0,pi,11)
I =
2.00000000114677
>> I = simpsoncom('fname',0,pi,2)
I =
2.00455975498442
>> I = simpsoncom('fname',0,pi,10)
I =
2.00000678444180
>> I = simpsoncom('fname',0,pi,100)
I =
2.00000000067647
>> I = simpsoncom('fname',0,pi,1000)
I =
2.00000000000007
>> I = simpsoncom('fname',0,pi,10000)
I =
2
*nota, para borrar la pantalla: clear clc
Tenemos cuadraturacom;
% Este fichero calculo la cuadratura
% de Newton-Cotes compuesta con m nodos
% y n subintervalos
% a,b numeros reales, a < b
% m numero de puntos, 2 <= m <=11
% n numero de subintervalos
%
% El programa calcula
% I La aproximacion de Newton-Cotes compuesta
% de la integral de f(x) entre a y b.
% La regla es aplicada a cada uno de los
% n subintervalos iguales de [a,b].
%
function I = cuadcompNC(fname,a,b,m,n)
Delta = (b-a)/n;
h = Delta/(m-1);
x = a+h*(0:(n*(m-1)))';
p = pesosNC(m);
%x = linspace(a,b,n*(m-1)+1)';
f = feval(fname,x);
I = 0;
first = 1;
last = m;
for i=1:n
%A-adimos al producto interno el valor en
% el subintervalo i-esimo.
I = I + p'*f(first: last);
first = last;
last = last+m-1;
end
I = Delta*I;
Cambio fname:
%
function y = fname(x)
%y = 2 - 3*x + 4*x.^2;
%y = 1 - x.^4;
%y = sin(x);
y = sin(x)./x;
con el programa cuadraturacomNC:
% Este fichero calcula la cuadratura
% de Newton-Cotes de la funcion fname
% con m puntos y extremos del intervalo a y b.
% a,b numeros reales
% m entero entre 2 <= m <=11
% El computo devuelve el numero I
%
function I = cuadraturaNC(fname,a,b,m)
p = pesosNC(m);
%x = linspace(a,b,m)';
h = (b-a)/(m-1);
x = (a:h:b)';
f = feval(fname,x);
I = (b-a)*(p'*f);
18/05/06
Tema 6 del book moler
Ejercicio 5.9
5.9. Statistical Reference Datasets. NIST, the National Institute of Standards and
Technology, is the branch of the U.S. Department of Commerce responsible
for setting national and international standards. NIST maintains Statistical
Reference Datasets, StRD, for use in testing and certifying statistical soft-
ware. The home page on the Web is [3]. Data sets for linear least squares are
under \Linear Regression." This exercise involves two of the NIST reference
data sets.
² Norris. Linear polynomial for calibration of ozone monitors.
² Pontius. Quadratic polynomial for calibration of load cells.
For each of these data sets, follow the Web links labeled
² Data ¯le (ASCII Format)
² Certi¯ed Values
² Graphics
Download each ASCII ¯le. Extract the observations. Compute the polyno-
mial coe±cients. Compare the coe±cients with the certi¯ed values. Make
plots similar to the NIST plots of both the ¯t and the residuals.
Copiamos de: http://www.itl.nist.gov/div898/strd/lls/data/LINKS/DATA/Norris.dat
NIST/ITL StRD
Dataset Name: Norris (Norris.dat)
File Format: ASCII
Certified Values (lines 31 to 46)
Data (lines 61 to 96)
Procedure: Linear Least Squares Regression
Reference: Norris, J., NIST.
Calibration of Ozone Monitors.
Data: 1 Response Variable (y)
1 Predictor Variable (x)
36 Observations
Lower Level of Difficulty
Observed Data
Model: Linear Class
2 Parameters (B0,B1)
y = B0 + B1*x + e
Certified Regression Statistics
Standard Deviation
Parameter Estimate of Estimate
B0 -0.262323073774029 0.232818234301152
B1 1.00211681802045 0.429796848199937E-03
Residual
Standard Deviation 0.884796396144373
R-Squared 0.999993745883712
Certified Analysis of Variance Table
Source of Degrees of Sums of Mean
Variation Freedom Squares Squares F Statistic
Regression 1 4255954.13232369 4255954.13232369 5436385.54079785
Residual 34 26.6173985294224 0.782864662630069
Data: y x
0.1 0.2
338.8 337.4
118.1 118.2
888.0 884.6
9.2 10.1
228.1 226.5
668.5 666.3
998.5 996.3
449.1 448.6
778.9 777.0
559.2 558.2
0.3 0.4
0.1 0.6
778.1 775.5
668.8 666.9
339.3 338.0
448.9 447.5
10.8 11.6
557.7 556.0
228.3 228.1
998.0 995.8
888.8 887.6
119.6 120.2
0.3 0.3
0.6 0.3
557.6 556.8
339.3 339.1
888.0 887.2
998.5 999.0
778.9 779.0
10.2 11.1
117.6 118.3
228.9 229.2
668.4 669.1
449.2 448.9
0.2 0.5
*Para importer datos: File Import Data seleccionas los datos que quieres importar
aceptas a todo y finalizas luego en matlab pones el nombre del archivo y se abre en el programa.
En matlab:
>> y = norris2(:,1)
y =
0.1000
338.8000
118.1000
888.0000
9.2000
228.1000
668.5000
998.5000
449.1000
778.9000
559.2000
0.3000
0.1000
778.1000
668.8000
339.3000
448.9000
10.8000
557.7000
228.3000
998.0000
888.8000
119.6000
0.3000
0.6000
557.6000
339.3000
888.0000
998.5000
778.9000
10.2000
117.6000
228.9000
668.4000
449.2000
0.2000
>> x = norris2(:,2)
x =
0.2000
337.4000
118.2000
884.6000
10.1000
226.5000
666.3000
996.3000
448.6000
777.0000
558.2000
0.4000
0.6000
775.5000
666.9000
338.0000
447.5000
11.6000
556.0000
228.1000
995.8000
887.6000
120.2000
0.3000
0.3000
556.8000
339.1000
887.2000
999.0000
779.0000
11.1000
118.3000
229.2000
669.1000
448.9000
0.5000
>> n = length(x)
n =
36
>> A = ones(36,2);
>> A(:,2) = x;
>> A
A =
1.0000 0.2000
1.0000 337.4000
1.0000 118.2000
1.0000 884.6000
1.0000 10.1000
1.0000 226.5000
1.0000 666.3000
1.0000 996.3000
1.0000 448.6000
1.0000 777.0000
1.0000 558.2000
1.0000 0.4000
1.0000 0.6000
1.0000 775.5000
1.0000 666.9000
1.0000 338.0000
1.0000 447.5000
1.0000 11.6000
1.0000 556.0000
1.0000 228.1000
1.0000 995.8000
1.0000 887.6000
1.0000 120.2000
1.0000 0.3000
1.0000 0.3000
1.0000 556.8000
1.0000 339.1000
1.0000 887.2000
1.0000 999.0000
1.0000 779.0000
1.0000 11.1000
1.0000 118.3000
1.0000 229.2000
1.0000 669.1000
1.0000 448.9000
1.0000 0.5000
>> rank(A)
ans =
2
>> rank([A y])
ans =
3
>> beta = A\y
beta =
-0.2623
1.0021
>> format long
>> beta = A\y
beta =
-0.26232307377407
1.00211681802045
Ahora pegamos de la misma página :
Pointius:
NIST/ITL StRD
Dataset Name: Pontius
File Format: ASCII
Certified Values (lines 31 to 47)
Data (lines 61 to 100)
Procedure: Linear Least Squares Regression
Reference: Pontius, P., NIST.
Load Cell Calibration.
Data: 1 Response Variable (y)
1 Predictor Variable (x)
40 Observations
Lower Level of Difficulty
Observed Data
Model: Quadratic Class
3 Parameters (B0,B1,B2)
y = B0 + B1*x + B2*(x**2)
Certified Regression Statistics
Standard Deviation
Parameter Estimate of Estimate
B0 0.673565789473684E-03 0.107938612033077E-03
B1 0.732059160401003E-06 0.157817399981659E-09
B2 -0.316081871345029E-14 0.486652849992036E-16
Residual
Standard Deviation 0.205177424076185E-03
R-Squared 0.999999900178537
Certified Analysis of Variance Table
Source of Degrees of Sums of Mean
Variation Freedom Squares Squares F Statistic
Regression 2 15.6040343244198 7.80201716220991 185330865.995752
Residual 37 0.155761768796992E-05 0.420977753505385E-07
Data: y x
.11019 150000
.21956 300000
.32949 450000
.43899 600000
.54803 750000
.65694 900000
.76562 1050000
.87487 1200000
.98292 1350000
1.09146 1500000
1.20001 1650000
1.30822 1800000
1.41599 1950000
1.52399 2100000
1.63194 2250000
1.73947 2400000
1.84646 2550000
1.95392 2700000
2.06128 2850000
2.16844 3000000
.11052 150000
.22018 300000
.32939 450000
.43886 600000
.54798 750000
.65739 900000
.76596 1050000
.87474 1200000
.98300 1350000
1.09150 1500000
1.20004 1650000
1.30818 1800000
1.41613 1950000
1.52408 2100000
1.63159 2250000
1.73965 2400000
1.84696 2550000
1.95445 2700000
2.06177 2850000
2.16829 3000000
Y en matlab se importan igual los datos y (solo los numeros le llamo pointius2):
pointius2 =
1.0e+006 *
0.00000011019000 0.15000000000000
0.00000021956000 0.30000000000000
0.00000032949000 0.45000000000000
0.00000043899000 0.60000000000000
0.00000054803000 0.75000000000000
0.00000065694000 0.90000000000000
0.00000076562000 1.05000000000000
0.00000087487000 1.20000000000000
0.00000098292000 1.35000000000000
0.00000109146000 1.50000000000000
0.00000120001000 1.65000000000000
0.00000130822000 1.80000000000000
0.00000141599000 1.95000000000000
0.00000152399000 2.10000000000000
0.00000163194000 2.25000000000000
0.00000173947000 2.40000000000000
0.00000184646000 2.55000000000000
0.00000195392000 2.70000000000000
0.00000206128000 2.85000000000000
0.00000216844000 3.00000000000000
0.00000011052000 0.15000000000000
0.00000022018000 0.30000000000000
0.00000032939000 0.45000000000000
0.00000043886000 0.60000000000000
0.00000054798000 0.75000000000000
0.00000065739000 0.90000000000000
0.00000076596000 1.05000000000000
0.00000087474000 1.20000000000000
0.00000098300000 1.35000000000000
0.00000109150000 1.50000000000000
0.00000120004000 1.65000000000000
0.00000130818000 1.80000000000000
0.00000141613000 1.95000000000000
0.00000152408000 2.10000000000000
0.00000163159000 2.25000000000000
0.00000173965000 2.40000000000000
0.00000184696000 2.55000000000000
0.00000195445000 2.70000000000000
0.00000206177000 2.85000000000000
0.00000216829000 3.00000000000000
-
Nota : si en el programa no tenemos la opción de “import data” , importaríamkos los datos de la siguiente manera: Pointius = load(`pointius.txt');
>> y = pointius2(:,1);
>> x = pointius2(:,2);
>> n = lenght(x)
>> n = length(x)
n =
40
>> A = ones(40,3);
>> A(:,2) = x;
>> A(:,3) = x.^2;
A =
1.0e+012 *
0.00000000000100 0.00000015000000 0.02250000000000
0.00000000000100 0.00000030000000 0.09000000000000
0.00000000000100 0.00000045000000 0.20250000000000
0.00000000000100 0.00000060000000 0.36000000000000
0.00000000000100 0.00000075000000 0.56250000000000
0.00000000000100 0.00000090000000 0.81000000000000
0.00000000000100 0.00000105000000 1.10250000000000
0.00000000000100 0.00000120000000 1.44000000000000
0.00000000000100 0.00000135000000 1.82250000000000
0.00000000000100 0.00000150000000 2.25000000000000
0.00000000000100 0.00000165000000 2.72250000000000
0.00000000000100 0.00000180000000 3.24000000000000
0.00000000000100 0.00000195000000 3.80250000000000
0.00000000000100 0.00000210000000 4.41000000000000
0.00000000000100 0.00000225000000 5.06250000000000
0.00000000000100 0.00000240000000 5.76000000000000
0.00000000000100 0.00000255000000 6.50250000000000
0.00000000000100 0.00000270000000 7.29000000000000
0.00000000000100 0.00000285000000 8.12250000000000
0.00000000000100 0.00000300000000 9.00000000000000
0.00000000000100 0.00000015000000 0.02250000000000
0.00000000000100 0.00000030000000 0.09000000000000
0.00000000000100 0.00000045000000 0.20250000000000
0.00000000000100 0.00000060000000 0.36000000000000
0.00000000000100 0.00000075000000 0.56250000000000
0.00000000000100 0.00000090000000 0.81000000000000
0.00000000000100 0.00000105000000 1.10250000000000
0.00000000000100 0.00000120000000 1.44000000000000
0.00000000000100 0.00000135000000 1.82250000000000
0.00000000000100 0.00000150000000 2.25000000000000
0.00000000000100 0.00000165000000 2.72250000000000
0.00000000000100 0.00000180000000 3.24000000000000
0.00000000000100 0.00000195000000 3.80250000000000
0.00000000000100 0.00000210000000 4.41000000000000
0.00000000000100 0.00000225000000 5.06250000000000
0.00000000000100 0.00000240000000 5.76000000000000
0.00000000000100 0.00000255000000 6.50250000000000
0.00000000000100 0.00000270000000 7.29000000000000
0.00000000000100 0.00000285000000 8.12250000000000
0.00000000000100 0.00000300000000 9.00000000000000
>> rank(A)
ans =
3
>> rank([A y])
ans =
3
>> beta = A\y
beta =
1.0e-003 *
0.67356578947336
0.00073205916040
-0.00000000000316
1) Ecuaciones normales AX = B ; A' A X = A' B
A' A X = M; MX = C
2) A = Q R
RX = Q' R X = R(Q*__); donde (Q*___) = D
3) A = U S V'
X = VS + U' B
>> M = A'*A
M =
1.0e+026 *
0.00000000000000 0.00000000000000 0.00000000000129
0.00000000000000 0.00000000000129 0.00000297675000
0.00000000000129 0.00000297675000 7.31699325000000
>> C = A' * y
C =
1.0e+014 *
0.00000000000046
0.00000093646979
2.15689932675000
>> beta1= M\C
Warning: Matrix is close to singular or badly scaled.
Results may be inaccurate. RCOND = 4.938239e-027.
beta1 =
1.0e-003 *
0.67356578947410
0.00073205916040
-0.00000000000316
>> [Q,R]=qr(A);
>> D = Q'*y;
>> beta2= R\D;
>> beta2
beta2 =
1.0e-003 *
0.67356578947465
0.00073205916040
-0.00000000000316
>> [U,S,V]= svd(A);
>> V
V =
0.00000000000018 0.00000129952456 0.99999999999916
0.00000040682694 0.99999999999907 -0.00000129952456
0.99999999999992 -0.00000040682694 0.00000000000035
>> S1 = pinv(S);
>> S1(1,2)
ans =
0
>> diag(S1)
ans =
0.00000000000004
0.00000035250209
0.52607450611596
>> beta3 = V*S1*U'*y;
>> beta3
beta3 =
1.0e-003 *
0.67356576935354
0.00073205916049
-0.00000000000316
>> norm(A*(beta2 - beta3))
ans =
2.128137835323598e-009
>> norm(A'*A*(beta2 - beta3))
ans =
5.735906807875822e+004
Cogemos el ejercicio 5.10 del moler ( y es el que entregamos de práctica)
5.10. Filip data set. One of the Statistical Reference Datasets from the NIST is the
\Filip" dataset. The data consists of several dozen observations of a variable
y at di®erent values of x. The task is to model y by a polynomial of degree
10 in x.
This dataset is controversial. A search of the Web for \¯lip strd" will ¯nd
several dozen postings, including the original page at NIST [3]. Some math-
ematical and statistical packages are able to reproduce the polynomial coef-
¯cients that NIST has decreed to be the \certi¯ed values." Other packages
give warning or error messages that the problem is too badly conditioned to
solve. A few packages give di®erent coe±cients without warning. The Web
o®ers several opinions about whether or not this is a reasonable problem.
Let's see what MATLAB does with it.
The data set is available from the NIST Web site. There is one line for
each data point. The data is given with the ¯rst number on the line a value
of y, and the second number the corresponding x. The x-values are not
monotonically ordered, but it is not necessary to sort them. Let n be the
number of data points and p = 11 the number of polynomial coe±cients.
(a) As your ¯rst experiment, load the data into MATLAB, plot it with '.'
as the line type, and then invoke the Basic Fitting tool available under the
Tools menu on the ¯gure window. Select the 10th degree polynomial ¯t. You
will be warned that the polynomial is badly conditioned, but ignore that for
now. How do the computed coe±cients compare with the certi¯ed values on
the NIST Web page? How does the plotted ¯t compare with the graphic on
the NIST Web page? The basic ¯tting tool also displays the norm of the
residuals, krk. Compare this with the NIST quantity \Residual Standard
Deviation," which is
krk pn ¡ p
(b) Examine this data set more carefully by using six di®erent methods to
compute the polynomial ¯t. Explain all the warning messages you receive
during these computations.
² Poly¯t: Use polyfit(x,y,10)
² Backslash: Use Xny where X is the n-by-p truncated Vandermonde ma-
trix with elements
Xi;j = xp¡j
i ; i = 1; : : : ; n; j = 1; : : : ; p
² Pseudoinverse: Use pinv(X)*y
² Normal equations: Use inv(X'*X)*X'*y.
² Centering: Let ¹ = mean(x); ¾ = std(x); t = (x ¡ ¹)=¾.
Use polyfit(t,y,10).
² Certi¯ed coe±cients: Obtain the coe±cients from the NIST Web page.
(c) What are the norms of the residuals for the ¯ts computed by the six
di®erent methods?
24 Chapter 5. Least Squares
(d) Which one of the six methods gives a very poor ¯t? (Perhaps the packages
that are criticized on theWeb for reporting bad results are using this method.)
(e) Plot the ¯ve good ¯ts. Use dots, '.', at the data values and curves
obtained by evaluating the polynomials at a few hundred points over the
range of the x's. The plot should look like ¯gure 5.5. There are ¯ve di®erent
plots, but only two visually distinct ones. Which methods produce which
plots?
(f) Why do poly¯t and backslash give di®erent results?
"9 "8 "7 "6 "5 "4 "3
0.76
0.78
0.8
0.82
0.84
0.86
0.88
0.9
0.92
0.94
NIST Filip data set
Data
Rank 11
Rank 10
Figure 5.5. NIST Filip standard reference data set
TEMA 6 del mooler:
Ejercicio 6.4:
6.4. Use quadtx with various tolerances to compute pi by approximating
pi = integral desde -1 a 1 de : 2/(1+x^2) dx
solución : 2*arcotg entre -1 y 1 = 2 [ pi/4 - (-pi/4)] = pi
How do the accuracy and the function evaluation count vary with tolerance?
Una manera de calcular pi es por cuadraturas, pero no es muy eficiente.
F(x) = 2/(1+x^2)
Fname.m
Inline
En matlab:
>> F = inline('2./(1+x^2)')
F =
Inline function:
F(x) = 2./(1+x^2)
>> G = inline('x.^y','x','y')
G =
Inline function:
G(x,y) = x.^y
Con el programa quadtx:
function [Q,fcount] = quadtx(F,a,b,tol,varargin)
%QUADTX Evaluate definite integral numerically.
% Q = QUADTX(F,A,B) approximates the integral of F(x) from A to B
% to within a tolerance of 1.e-6. F is a string defining a function
% of a single variable, an inline function, a function handle, or a
% symbolic expression involving a single variable.
%
% Q = QUADTX(F,A,B,tol) uses the given tolerance instead of 1.e-6.
%
% Arguments beyond the first four, Q = QUADTX(F,a,b,tol,p1,p2,...),
% are passed on to the integrand, F(x,p1,p2,..).
%
% [Q,fcount] = QUADTX(F,...) also counts the number of evaluations
% of F(x).
%
% See also QUAD, QUADL, DBLQUAD, QUADGUI.
% Make F callable by feval.
if ischar(F) & exist(F)~=2
F = inline(F);
elseif isa(F,'sym')
F = inline(char(F));
end
% Default tolerance
if nargin < 4 | isempty(tol)
tol = 1.e-6;
end
% Initialization
c = (a + b)/2;
fa = feval(F,a,varargin{:});
fc = feval(F,c,varargin{:});
fb = feval(F,b,varargin{:});
% Recursive call
[Q,k] = quadtxstep(F, a, b, tol, fa, fc, fb, varargin{:});
fcount = k + 3;
% ---------------------------------------------------------
function [Q,fcount] = quadtxstep(F,a,b,tol,fa,fc,fb,varargin)
% Recursive subfunction used by quadtx.
h = b - a;
c = (a + b)/2;
fd = feval(F,(a+c)/2,varargin{:});
fe = feval(F,(c+b)/2,varargin{:});
Q1 = h/6 * (fa + 4*fc + fb);
Q2 = h/12 * (fa + 4*fd + 2*fc + 4*fe + fb);
if abs(Q2 - Q1) <= tol
Q = Q2 + (Q2 - Q1)/15;
fcount = 2;
else
[Qa,ka] = quadtxstep(F, a, c, tol, fa, fd, fc, varargin{:});
[Qb,kb] = quadtxstep(F, c, b, tol, fc, fe, fb, varargin{:});
Q = Qa + Qb;
fcount = ka + kb + 2;
end
>> I = quadtx(F,-1,1,10^-6)
I =
3.14159265370804
I2 = cuadcompNC(F,-1,1,3,10)
I2=
3.14159261393922
I2= cuadcmpNC(F,-1,1,8,10)
I2 =
3.14159265358986
I2= cuadcompNC(F,-1,1,8,100)
I2 =
3.14159265358979
Otro ejercicio es el 6.6 (página14 del capitulo 6 del mooler)
6.6. The error function, erf(x), is de¯ned by an integral,
erf(x) = 2/raiz(pi) * integral de 0 a x de “e” elevado a “-x^2”
Use quadtx to tabulate erf(x) for x = 0:1; 0:2; : : : ; 1:0: Compare the results
with the built-in Matlab function erf(x).
*Nota para el 6.8 . Tenemos una gamma(n+1) = n!
30-05-06
Capitulo 8 (chapter 7)
*Metodo de Picard
Tenemos el archivo:
Harmonic:
function ydot = harmonic(t,y)
ydot = [y(2); -y(1)];
en matlab:
>> [t,y] = ode23('harmonic',[0 5],[3;0]);
>> [t,y] = ode23('harmonic',[0 5],[3;0])
t =
0
0.0000
0.0002
0.0008
0.0042
0.0208
0.1008
0.2361
0.4164
0.6367
0.8973
1.1880
1.4396
1.5862
1.7328
1.8913
2.0918
2.3317
2.6147
2.8857
3.0680
3.2062
3.3445
3.5157
3.7276
3.9793
4.2768
4.5361
4.6975
4.8589
5.0000
y =
3.0000 0
3.0000 -0.0001
3.0000 -0.0005
3.0000 -0.0025
3.0000 -0.0125
2.9993 -0.0625
2.9848 -0.3019
2.9167 -0.7019
2.7435 -1.2134
2.4118 -1.7834
1.8704 -2.3443
1.1194 -2.7813
0.3917 -2.9719
-0.0467 -2.9972
-0.4841 -2.9581
-0.9448 -2.8446
-1.4923 -2.5993
-2.0671 -2.1698
-2.5902 -1.5058
-2.8981 -0.7573
-2.9872 -0.2194
-2.9889 0.1945
-2.9335 0.6046
-2.7875 1.0955
-2.4945 1.6571
-2.0029 2.2258
-1.2619 2.7144
-0.5234 2.9467
-0.0431 2.9924
0.4383 2.9604
0.8503 2.8692
>> plot(t,y(:,1))
> [t,y] = ode23('harmonic',[0 50],[3;0]);
>> plot(t,y(:,1))
Tenemos el programa :
Harmonic_damped al que llamamos por comodidad : harmonicd :
function ydot = harmonic_damped(t,y)
alpha = .5;
ydot = [y(2); -y(1) - alpha *y(2)];
en matlab:
>> [t,y] = ode23('harmonicd',[0 50],[3;0]);
>> plot(t,y(:,1))
Cambiamos el alfa del programa:
function ydot = harmonic_damped(t,y)
alpha = .1;
ydot = [y(2); -y(1) - alpha *y(2)];
>> [t,y] = ode23('harmonicd',[0 50],[3;0]);
>> plot(t,y(:,1))
Cambiamos el programa:
function ydot = harmonic_damped(t,y)
alpha = .1; beta = 1.2;
ydot = [y(2); -y(1) - alpha *(y(2).^beta)];
en matlab:
>> [t,y] = ode23('harmonicd',[0 50],[3;0]);
>> plot(t,y(:,1))
Warning: Imaginary parts of complex X and/or Y arguments ignored.
>> plot(y(:,1),y(:,2))
Warning: Imaginary parts of complex X and/or Y arguments ignored.
>> [t,y] = ode23('harmonicd',[0 50],[7;2]);
>> [t,y] = ode23('harmonicd',[0 100],[7;2]);
>> plot(y(:,1),y(:,2))
Warning: Imaginary parts of complex X and/or Y arguments ignored.
Tenemos el programa:
Twobody:
function ydot = twobody(t,y)
r = sqrt(y(1)^2 + y(2)^2);
ydot = [y(3); y(4); -y(1)/r^3 ; -y(2)/r^3];
>> [t,y] = ode23('twobody',[0 3],[5;0;0;0.1]);
>> plot(y(:,1),y(:,2))
>> [t,y] = ode23('twobody',[0 10],[10;0;0;0.1]);
>> plot(y(:,1),y(:,2))
>> [t,y] = ode23('twobody',[0 10],[3;0;0;0.1]);
>> plot(y(:,1),y(:,2))
>>
>> [t,y] = ode23('twobody',[0 20],[3;0;0;0.1]);
>> plot(y(:,1),y(:,2))
>> [t,y] = ode45('twobody',[0 20],[3;0;0;0.1]);
>> plot(y(:,1),y(:,2))
>> [t,y] = ode45('twobody',[0 200],[3;0;0;0.1]);
>> plot(y(:,1),y(:,2))
1-junio-06
Ejercicio del libro moler (26 Chapter 5. Least Squares):
5.12. Planetary orbit [2]. The expression z = ax2+bxy+cy2+dx+ey+f is known
as a quadratic form. The set of points (x; y) where z = 0 is a conic section.
It can be an ellipse, a parabola, or a hyperbola, depending on the sign of
the discriminant b2 ¡ 4ac. Circles and lines are special cases. The equation
z = 0 can be normalized by dividing the quadratic form by any nonzero
coe±cient. For example, if f 6= 0, we can divide all the other coe±cients by
f and obtain a quadratic form with the constant term equal to one. You can
use the Matlab meshgrid and contour functions to plot conic sections. Use
meshgrid to create arrays X and Y. Evaluate the quadratic form to produce
Z. Then use contour to plot the set of points where Z is zero.
[X,Y] = meshgrid(xmin:deltax:xmax,ymin:deltay:ymax);
Z = a*X.^2 + b*X.*Y + c*Y.^2 + d*X + e*Y + f;
contour(X,Y,Z,[0 0])
A planet follows an elliptical orbit. Here are ten observations of its position
in the (x; y) plane:
x = [1.02 .95 .87 .77 .67 .56 .44 .30 .16 .01]';
y = [0.39 .32 .27 .22 .18 .15 .13 .12 .13 .15]';
(a) Determine the coe±cients in the quadratic form that ¯ts this data in
the least squares sense by setting one of the coe±cients equal to one and
solving a 10-by-5 overdetermined system of linear equations for the other
¯ve coe±cients. Plot the orbit with x on the x-axis and y on the y-axis.
Superimpose the ten data points on the plot.
(b) This least squares problem is nearly rank de¯cient. To see what e®ect this
has on the solution, perturb the data slightly by adding to each coordinate
of each data point a random number uniformly distributed in the interval
[-.005,.005]. Compute the new coe±cients resulting from the perturbed data.
Plot the new orbit on the same plot with the old orbit. Comment on your
comparison of the sets of coe±cients and the orbits.
En matlab:
Practica3
[x,y]=meshgrid(-2:0.01:2,-2:0.01:2);
a=1;b=1;c=1;e=1;f=-1;
>> z = a*x.^2+b*x.*y+c*y.^2+b*x+e*y+f;
>> contour(x,y,z,[0 0])
>> contour(x,y,z,5)
>> contour(x,y,z,10)
Para cada punto de x e y tenemos una ecuación diferente de:
= ax^2 + bxy +cy^2+dx+ey
C= (a b c d e)' ; A*C = (1 …. 1)' = r
X`2= (x1^2 …. X10^2)'
A=[X`2 XY Y^2 X Y]
C = A/r
En matlab:
>> x = [1.02 .95 .87 .77 .67 .56 .44 .30 .16 .01]';
>> y = [0.39 .32 .27 .22 .18 .15 .13 .12 .13 .15]';
>> x
x =
1.0200
0.9500
0.8700
0.7700
0.6700
0.5600
0.4400
0.3000
0.1600
0.0100
>> y
y =
0.3900
0.3200
0.2700
0.2200
0.1800
0.1500
0.1300
0.1200
0.1300
0.1500
>> A = [x.^2 x.*y y.^2 x y];
>> size(A)
ans =
10 5
>> r= ones(10,1)
r =
1
1
1
1
1
1
1
1
1
1
>> [X,Y]= meshgrid(-2:0.01:2,-2:0.01:2);
>> z = a*X.^2+b*X.*Y+c*Y.^2+b*X+e*Y+f;
>> A = [x.^2 x.*y y.^2 x y];
>> C=A\r;
>> a = C(1);b=C(2);c= C(3);d=C(4);e=C(5);
>> Z = a*X.^2+b*X.*Y+c*Y.^2+b*X+e*Y+f;
>> [X,Y]= meshgrid(-2:0.01:2,-2:0.01:2);
>> x = [1.02 .95 .87 .77 .67 .56 .44 .30 .16 .01]';
>> y = [0.39 .32 .27 .22 .18 .15 .13 .12 .13 .15]';
>> Z = a*X.^2+b*X.*Y+c*Y.^2+b*X+e*Y+f;
>> C=A\r;
>> a = C(1);b=C(2);c= C(3);d=C(4);e=C(5);
>> contour(X,Y,Z,[0 0])
>> plot(x,y,'r*')
>> x = x + 0.005*(rand(10,1)-0.5);
>> y = y + 0.005*(rand(10,1)-0.5);
>> A = [x.^2 x.*y y.^2 x y];
>> C = A\r;
>> Z = a*X.^2+b*X.*Y+c*Y.^2+b*X+e*Y+f;
>> a = C(1); b = C(2); c = C(3); d = C(4); e = C(5);
>> Z = a*X.^2+b*X.*Y+c*Y.^2+b*X+e*Y+f;
>> contour(X,Y,Z,[0 0])
>> hold on
PROGRAMAS USADOS:
BSLASHTX
function x = bslashtx(A,b)
% BSLASHTX Solve linear system (backslash)
% x = bslashtx(A,b) solves A*x = b
[n,n] = size(A);
if isequal(triu(A,1),zeros(n,n))
% Lower triangular
x = forward(A,b);
return
elseif isequal(tril(A,-1),zeros(n,n))
% Upper triangular
x = backsubs(A,b);
return
elseif isequal(A,A')
[R,fail] = chol(A);
if ~fail
% Positive definite
y = forward(R',b);
x = backsubs(R,y);
return
end
end
% Triangular factorization
[L,U,p] = lutx(A);
% Permutation and forward elimination
y = forward(L,b(p));
% Back substitution
x = backsubs(U,y);
% ------------------------------
function x = forward(L,x)
% FORWARD. Forward elimination.
% For lower triangular L, x = forward(L,b) solves L*x = b.
[n,n] = size(L);
x(1) = x(1)/L(1,1);
for k = 2:n
j = 1:k-1;
x(k) = (x(k) - L(k,j)*x(j))/L(k,k);
end
% ------------------------------
function x = backsubs(U,x)
% BACKSUBS. Back substitution.
% For upper triangular U, x = backsubs(U,b) solves U*x = b.
[n,n] = size(U);
x(n) = x(n)/U(n,n);
for k = n-1:-1:1
j = k+1:n;
x(k) = (x(k) - U(k,j)*x(j))/U(k,k);
end
CGS
% Gram-Schmidt orthogonalization (unstable)
function [Q,R] = cgs(A)
n = length(A);
% starting variables
R = zeros(n,n);
Q = zeros(n,n);
V = zeros(n,n);
% Normalizing the first column vector A
R(1,1)=norm(A(:,1));
Q(:,1)= A(:,1)/R(1,1);
% Classical Gram-Schmidt
for j = 2:n
V(:,j) = A(:,j);
for i = 1:j-1
R(i,j) = Q(:,i)'*A(:,j);
V(:,j)= V(:,j)-R(i,j)*Q(:,i);
end
R(j,j)=norm(V(:,j));
Q(:,j)=V(:,j)/R(j,j);
end
Q;
R;
CUADCOMNC
% Este fichero calcula la cuadratura
% de Newton-Cotes de la funcion fname
% con m puntos y extremos del intervalo a y b.
% a,b numeros reales
% m entero entre 2 <= m <=11
% El computo devuelve el numero I
%
function I = cuadraturaNC(fname,a,b,m)
p = pesosNC(m);
%x = linspace(a,b,m)';
h = (b-a)/(m-1);
x = (a:h:b)';
f = feval(fname,x);
I = (b-a)*(p'*f);
CUADRATURA
% Este fichero calcula la cuadratura
% de Newton-Cotes de la funcion fname
% con m puntos y extremos del intervalo a y b.
% a,b numeros reales
% m entero entre 2 <= m <=11
% El computo devuelve el numero I
%
function I = cuadraturaNC(fname,a,b,m)
p = pesosNC(m);
%x = linspace(a,b,m)';
h = (b-a)/(m-1);
x = (a:h:b)';
f = feval(fname,x);
I = (b-a)*(p'*f);
CUADRATURANC
% Este fichero calculo la cuadratura
% de Newton-Cotes compuesta con m nodos
% y n subintervalos
% a,b numeros reales, a < b
% m numero de puntos, 2 <= m <=11
% n numero de subintervalos
%
% El programa calcula
% I La aproximacion de Newton-Cotes compuesta
% de la integral de f(x) entre a y b.
% La regla es aplicada a cada uno de los
% n subintervalos iguales de [a,b].
%
function I = cuadcompNC(fname,a,b,m,n)
Delta = (b-a)/n;
h = Delta/(m-1);
x = a+h*(0:(n*(m-1)))';
p = pesosNC(m);
%x = linspace(a,b,n*(m-1)+1)';
f = feval(fname,x);
I = 0;
first = 1;
last = m;
for i=1:n
%A-adimos al producto interno el valor en
% el subintervalo i-esimo.
I = I + p'*f(first: last);
first = last;
last = last+m-1;
end
I = Delta*I;
DEMO_CGS_MGS
% Numerical comparison:
% Classical Gram-Schmidt and
% modified Gram-Schmidt
% First we generate a random matrix A
% with eigenvalues spaced by a factor 2
% between 2^-1 and 2^-80
[U,X]= qr(randn(80));
S = diag(2.^(-1:-1:-80));
A = U*S*U';
E = eig(A);
% We use now classical Gram-Schmid cgs(A)
% and modified Gram-Schmidt mgs(A) to compute Q and R
[Q1,R1]=cgs(A);
[Q2,R2]=mgs(A);
% We represent the diagonal R elements
% in logarithmic scale for both matrices R1 and R2.
x = 1:80;
y1 = log2(diag(R1));
y2 = log2(diag(R2));
y6 = log2(-sort(-abs(E)));
y3 = -23*ones(1,80);
y4 = -55*ones(1,80);
y5 = -x;
plot(x,y1,'bo',x,y2,'rx',x,y6,'g*',x,y3,':',x,y4,':',x,y5,'-');
xlabel('R(i,i) elements in logarithmic scale');
DEMO_INTER
%
% This script shows the graphic of cos(4x)
% by interpolating with a polynomial of degree
% 12 found by least squares.
close all
t = (linspace(0,5,50))';
A = vander(t);
A = A(:,38:50);
b = (cos(4*t));
u = 0:0.01:5;
v = cos(4*u);
p = A\b;
pvals = horner(p,t);
plot(t,b,'or',t,pvals,'b',u,v,'g')
DEMO_ORTOG
% This script explores the lost of orthogonality
% due to the intrinsic numerical unstability
% of the classical and
% modified Gram-Schmidt algorithms.
clc
disp(' Losing orthogonality on Gram-Schmidt algorithms ')
disp(' delta Error on QR Error on CGS Error on MGS ')
disp('------------------------------------------------------------------------')
for delta = logspace(-4,-16,7)
A = [1+delta 2;1 2];
[Q1,R1]= qr(A);
[Q2,R2]= cgs(A);
[Q3,R3]= mgs(A);
error1 = norm(Q1'*Q1 - eye(2));
error2 = norm(Q2'*Q2 - eye(2));
error3 = norm(Q3'*Q3 - eye(2));
disp(sprintf(' %5.0e %20.15f %20.15f %20.15f ', delta,error1,error2,error3))
end
EULER
function y = euler(f,t0,y0,h,tf)
t = t0;
y = y0;
while t <= tf
y = y + h*feval(f,t,y);
t = t + h;
end
FZEROTX
function b = fzerotx(F,ab,varargin)
%FZEROTX Textbook version of FZERO.
% x = fzerotx(F,[a,b]) tries to find a zero of F(x) between a and b.
% F(a) and F(b) must have opposite signs. fzerotx returns one
% end point of a small subinterval of [a,b] where F changes sign.
% Arguments beyond the first two, fzerotx(F,[a,b],p1,p2,...),
% are passed on, F(x,p1,p2,..).
%
% Example:
% fzerotx('sin(x)',[1,4])
% Make F callable by feval.
if ischar(F) & exist(F)~=2
F = inline(F);
elseif isa(F,'sym')
F = inline(char(F));
end
% Initialize.
a = ab(1);
b = ab(2);
fa = feval(F,a,varargin{:});
fb = feval(F,b,varargin{:});
if sign(fa) == sign(fb)
error('Function must change sign on the interval')
end
c = a;
fc = fa;
d = b - c;
e = d;
% Main loop, exit from middle of the loop
while fb ~= 0
% The three current points, a, b, and c, satisfy:
% f(x) changes sign between a and b.
% abs(f(b)) <= abs(f(a)).
% c = previous b, so c might = a.
% The next point is chosen from
% Bisection point, (a+b)/2.
% Secant point determined by b and c.
% Inverse quadratic interpolation point determined
% by a, b, and c if they are distinct.
if sign(fa) == sign(fb)
a = c; fa = fc;
d = b - c; e = d;
end
if abs(fa) < abs(fb)
c = b; b = a; a = c;
fc = fb; fb = fa; fa = fc;
end
% Convergence test and possible exit
m = 0.5*(a - b);
tol = 2.0*eps*max(abs(b),1.0);
if (abs(m) <= tol) | (fb == 0.0)
break
end
% Choose bisection or interpolation
if (abs(e) < tol) | (abs(fc) <= abs(fb))
% Bisection
d = m;
e = m;
else
% Interpolation
s = fb/fc;
if (a == c)
% Linear interpolation (secant)
p = 2.0*m*s;
q = 1.0 - s;
else
% Inverse quadratic interpolation
q = fc/fa;
r = fb/fa;
p = s*(2.0*m*q*(q - r) - (b - c)*(r - 1.0));
q = (q - 1.0)*(r - 1.0)*(s - 1.0);
end;
if p > 0, q = -q; else p = -p; end;
% Is interpolated point acceptable
if (2.0*p < 3.0*m*q - abs(tol*q)) & (p < abs(0.5*e*q))
e = d;
d = p/q;
else
d = m;
e = m;
end;
end
% Next point
c = b;
fc = fb;
if abs(d) > tol
b = b + d;
else
b = b - sign(b-a)*tol;
end
fb = feval(F,b,varargin{:});
end
HARMONIC
function ydot = harmonic(t,y)
ydot = [y(2); -y(1)];
HARMONIC DAM PED
function ydot = harmonic_damped(t,y)
alpha = .5;
ydot = [y(2); -y(1) - alpha *y(2)];
HORNER
% This function evaluates
% the polynomial of degree n-1 with coefficients a1,...,an
% at the point z by using Horner's algorithm
function p = horner(a,z)
n = length(a);
m = length(z);
p = a(1)*ones(m,1);
for k = 2:n
p = z.*p + a(k);
end
LUTX
function [L,U,p] = lutx(A)
%LUTX Triangular factorization, textbook version
% [L,U,p] = lutx(A) produces a unit lower triangular matrix L,
% an upper triangular matrix U, and a permutation vector p,
% so that L*U = A(p,:)
[n,n] = size(A);
p = (1:n)';
for k = 1:n-1
% Find index of largest element below diagonal in k-th column
[r,m] = max(abs(A(k:n,k)));
m = m+k-1;
% Skip elimination if column is zero
if (A(m,k) ~= 0)
% Swap pivot row
if (m ~= k)
A([k m],:) = A([m k],:);
p([k m]) = p([m k]);
end
% Compute multipliers
i = k+1:n;
A(i,k) = A(i,k)/A(k,k);
% Update the remainder of the matrix
j = k+1:n;
A(i,j) = A(i,j) - A(i,k)*A(k,j);
end
end
% Separate result
L = tril(A,-1) + eye(n,n);
U = triu(A);
MGS
% Modified Gram-Schmidt algorithm (stable)
function [Q,R] = mgs(A)
[m,n] = size(A);
% Initializating variables
R = zeros(m,n);
S = zeros(m,m);
Q = zeros(m,m);
V = [A floor(10*rand(m,m-n))];
for i = 1:n
R(i,i)=norm(V(:,i));
Q(:,i)=V(:,i)/R(i,i);
for j = i+1:n
R(i,j) = Q(:,i)'*V(:,j);
V(:,j)= V(:,j)-R(i,j)*Q(:,i);
end
end
for i = n+1:m
S(i,i)=norm(V(:,i));
Q(:,i)=V(:,i)/S(i,i);
for j = i+1:n
S(i,j) = Q(:,i)'*V(:,j);
V(:,j)= V(:,j)-S(i,j)*Q(:,i);
end
end
Q;
R;
ODE23TX
function [tout,yout] = ode23tx(F,tspan,y0,arg4,varargin)
%ODE23TX Solve non-stiff differential equations. Textbook version of ODE23.
%
% ODE23TX(F,TSPAN,Y0) with TSPAN = [T0 TFINAL] integrates the system
% of differential equations y' = f(t,y) from t = T0 to t = TFINAL. The
% initial condition is y(T0) = Y0. The input argument F is the
% name of an M-file, or an inline function, or simply a character string,
% defining f(t,y). This function must have two input arguments, t and y,
% and must return a column vector of the derivatives, y'.
%
% With two output arguments, [T,Y] = ODE23TX(...) returns a column
% vector T and an array Y where Y(:,k) is the solution at T(k).
%
% With no output arguments, ODE23TX plots the emerging solution.
%
% ODE23TX(F,TSPAN,Y0,RTOL) uses the relative error tolerance RTOL
% instead of the default 1.e-3.
%
% ODE23TX(F,TSPAN,Y0,OPTS) where OPTS = ODESET('reltol',RTOL, ...
% 'abstol',ATOL,'outputfcn',@PLOTFUN) uses relative error RTOL instead
% of 1.e-3, absolute error ATOL instead of 1.e-6, and calls PLOTFUN
% instead of ODEPLOT after each successful step.
%
% More than four input arguments, ODE23TX(F,TSPAN,Y0,RTOL,P1,P2,...),
% are passed on to F, F(T,Y,P1,P2,...).
%
% ODE23TX uses the Runge-Kutta (2,3) method of Bogacki and Shampine (BS23).
%
% Example
% tspan = [0 2*pi];
% y0 = [1 0]';
% F = '[0 1; -1 0]*y';
% ode23tx(F,tspan,y0);
%
% See also ODE23.
% Initialize variables.
rtol = 1.e-3;
atol = 1.e-6;
plotfun = @odeplot;
if nargin >= 4 & isnumeric(arg4)
rtol = arg4;
elseif nargin >= 4 & isstruct(arg4)
if ~isempty(arg4.RelTol), rtol = arg4.RelTol; end
if ~isempty(arg4.AbsTol), atol = arg4.AbsTol; end
if ~isempty(arg4.OutputFcn), plotfun = arg4.OutputFcn; end
end
t0 = tspan(1);
tfinal = tspan(2);
tdir = sign(tfinal - t0);
plotit = (nargout == 0);
threshold = atol / rtol;
hmax = abs(0.1*(tfinal-t0));
t = t0;
y = y0(:);
% Make F callable by feval.
if ischar(F) & exist(F)~=2
F = inline(F,'t','y');
elseif isa(F,'sym')
F = inline(char(F),'t','y');
end
% Initialize output.
if plotit
feval(plotfun,tspan,y,'init');
else
tout = t;
yout = y.';
end
% Compute initial step size.
s1 = feval(F, t, y, varargin{:});
r = norm(s1./max(abs(y),threshold),inf) + realmin;
h = tdir*0.8*rtol^(1/3)/r;
% The main loop.
while t ~= tfinal
hmin = 16*eps*abs(t);
if abs(h) > hmax, h = tdir*hmax; end
if abs(h) < hmin, h = tdir*hmin; end
% Stretch the step if t is close to tfinal.
if 1.1*abs(h) >= abs(tfinal - t)
h = tfinal - t;
end
% Attempt a step.
s2 = feval(F, t+h/2, y+h/2*s1, varargin{:});
s3 = feval(F, t+3*h/4, y+3*h/4*s2, varargin{:});
tnew = t + h;
ynew = y + h*(2*s1 + 3*s2 + 4*s3)/9;
s4 = feval(F, tnew, ynew, varargin{:});
% Estimate the error.
e = h*(-5*s1 + 6*s2 + 8*s3 - 9*s4)/72;
err = norm(e./max(max(abs(y),abs(ynew)),threshold),inf) + realmin;
% Accept the solution if the estimated error is less than the tolerance.
if err <= rtol
t = tnew;
y = ynew;
if plotit
if feval(plotfun,t,y,'');
break
end
else
tout(end+1,1) = t;
yout(end+1,:) = y.';
end
s1 = s4; % Reuse final function value to start new step.
end
% Compute a new step size.
h = h*min(5,0.8*(rtol/err)^(1/3));
% Exit early if step size is too small.
if abs(h) <= hmin
warning('Step size %e too small at t = %e.\n',h,t);
t = tfinal;
end
end
if plotit
feval(plotfun,[],[],'done');
end
ORBIT EULER
function orbit_euler(F,tspan,h,y0)
clc
%t0 = 0;
%h = 0.001;
%y0 = [1;0];
t0 = tspan(1);
tf = tspan(2);
t1 = t0 + h;
u = t0:h:tf;
v = u;
k = 1;
hs = h/10;
while t1 <= tf
y = euler(F,t0,y0,hs,t1);
u(k) = y(1);
v(k) = y(2);
plot(u(k),v(k),'b')
hold on
t0 = t1;
t1 = t0 + h;
y0 = y;
k = k+1;
end
PCHIPSLOPES
function d = pchipslopes(h,delta)
% PCHIPSLOPES Slopes for shape-preserving Hermite cubic
% interpolation. pchipslopes(h,delta) computes d(k) = P'(x(k)).
% Slopes at interior points
% delta = diff(y)./diff(x).
% d(k) = 0 if delta(k-1) and delta(k) have opposites signs
% or either is zero.
% d(k) = weighted harmonic mean of delta(k-1) and delta(k)
% if they have the same sign.
n = length(h)+1;
d = zeros(size(h));
k = find(sign(delta(1:n-2)).*sign(delta(2:n-1)) > 0) + 1;
w1 = 2*h(k)+h(k-1);
w2 = h(k)+2*h(k-1);
d(k) = (w1+w2)./(w1./delta(k-1) + w2./delta(k));
% Slopes at endpoints
d(1) = pchipendpoint(h(1),h(2),delta(1),delta(2));
d(n) = pchipendpoint(h(n-1),h(n-2),delta(n-1),delta(n-2));
% -------------------------------------------------------
PCHIPTX
function v = pchiptx(x,y,u)
%PCHIPTX Textbook piecewise cubic Hermite interpolation.
% v = pchiptx(x,y,u) finds the shape-preserving piecewise cubic
% interpolant P(x), with P(x(j)) = y(j), and returns v(k) = P(u(k)).
%
% See PCHIP, SPLINETX.
% First derivatives
h = diff(x);
delta = diff(y)./h;
d = pchipslopes(h,delta);
% Piecewise polynomial coefficients
n = length(x);
c = (3*delta - 2*d(1:n-1) - d(2:n))./h;
b = (d(1:n-1) - 2*delta + d(2:n))./h.^2;
% Find subinterval indices k so that x(k) <= u < x(k+1)
k = ones(size(u));
for j = 2:n-1
k(x(j) <= u) = j;
end
% Evaluate interpolant
s = u - x(k);
v = y(k) + s.*(d(k) + s.*(c(k) + s.*b(k)));
% -------------------------------------------------------
function d = pchipslopes(h,delta)
% PCHIPSLOPES Slopes for shape-preserving Hermite cubic
% interpolation. pchipslopes(h,delta) computes d(k) = P'(x(k)).
% Slopes at interior points
% delta = diff(y)./diff(x).
% d(k) = 0 if delta(k-1) and delta(k) have opposites signs
% or either is zero.
% d(k) = weighted harmonic mean of delta(k-1) and delta(k)
% if they have the same sign.
n = length(h)+1;
d = zeros(size(h));
k = find(sign(delta(1:n-2)).*sign(delta(2:n-1)) > 0) + 1;
w1 = 2*h(k)+h(k-1);
w2 = h(k)+2*h(k-1);
d(k) = (w1+w2)./(w1./delta(k-1) + w2./delta(k));
% Slopes at endpoints
d(1) = pchipendpoint(h(1),h(2),delta(1),delta(2));
d(n) = pchipendpoint(h(n-1),h(n-2),delta(n-1),delta(n-2));
% -------------------------------------------------------
function d = pchipendpoint(h1,h2,del1,del2)
% Noncentered, shape-preserving, three-point formula.
d = ((2*h1+h2)*del1 - h1*del2)/(h1+h2);
if sign(d) ~= sign(del1)
d = 0;
elseif (sign(del1) ~= sign(del2)) & (abs(d) > abs(3*del1))
d = 3*del1;
end
PESOSNC
% Este fichero almacena los
% pesos de las reglas de
% cuadratura de Newton-Cotes
% con m puntos
%
% m es un entero que satisface 2 <= m <= 11
%
% p es un vector columna que contiene
% los pesos para la regla de cuadratura
% de Newton-Cotes con m puntos.
%
function p = pesosNC(m);
if m==2
p=[1 1]'/2;
elseif m==3
p=[1 4 1]'/6;
elseif m==4
p=[1 3 3 1]'/8;
elseif m==5
p=[7 32 12 32 7]'/90;
elseif m==6
p=[19 75 50 50 75 19]'/288;
elseif m==7
p=[41 216 27 272 27 216 41]'/840;
elseif m==8
p=[751 3577 1323 2989 2989 1323 3577 751]'/17280;
elseif m==9
p=[989 5888 -928 10496 -4540 10496 -928 5888 989]'/28350;
elseif m==10
p=[2857 15741 1080 19344 5778 5778 19344 1080 15741 2857]'/89600;
else
p=[16067 106300 -48525 272400 -260550 427368 -260550 272400 -48525 106300 16067]'/598752;
end;
PIECELIN
function v = piecelin(x,y,u)
%PIECELIN Piecewise linear interpolation.
% v = piecelin(x,y,u) finds the piecewise linear L(x)
% with L(x(j)) = y(j) and returns v(k) = L(u(k)).
% First divided difference
delta = diff(y)./diff(x);
% Find subinterval indices k so that x(k) <= u < x(k+1)
n = length(x);
k = ones(size(u));
for j = 2:n-1
k(x(j) <= u) = j;
end
% Evaluate interpolant
s = u - x(k);
v = y(k) + s.*delta(k);
POLYINTERP
function v = polyinterp(x,y,u)
%POLYINTERP Polynomial interpolation.
% v = POLYINTERP(x,y,u) computes v(j) = P(u(j)) where P is the
% polynomial of degree d = length(x)-1 with P(x(i)) = y(i).
% Use Lagrangian representation.
% Evaluate at all elements of u simultaneously.
n = length(x);
v = zeros(size(u));
for k = 1:n
w = ones(size(u));
for j = [1:k-1 k+1:n]
w = (u-x(j))./(x(k)-x(j)).*w;
end
v = v + w*y(k);
end
QRSTEPS
function [A,b] = qrsteps(A,b)
%QRSTEPS Orthogonal-triangular decomposition.
% Demonstrates M-file version of built-in QR function.
% R = QRSTEPS(A) is the upper trapezoidal matrix R that
% results from the orthogonal transformation, R = Q'*A.
% With no output argument, QRSTEPS(A) shows the steps in
% the computation of R. Press <enter> key after each step.
% [R,bout] = QRSTEPS(A,b) also applies the transformation to b.
[m,n] = size(A);
if nargin < 2, b = zeros(m,0); end
% Householder reduction to triangular form.
if nargout == 0
clc
A
if ~isempty(b), b, end
pause
end
for k = 1:min(m-1,n)
% Introduce zeros below the diagonal in the k-th column.
% Use Householder transformation, I - rho*u*u'.
i = k:m;
u = A(i,k);
sigma = norm(u);
% Skip transformation if column is already zero.
if sigma ~= 0
if u(1) ~= 0, sigma = sign(u(1))*sigma; end
u(1) = u(1) + sigma;
rho = 1/(conj(sigma)*u(1));
% Update the k-th column.
A(i,k) = 0;
A(k,k) = -sigma;
% Apply the transformation to remaining columns of A.
j = k+1:n;
v = rho*(u'*A(i,j));
A(i,j) = A(i,j) - u*v;
% Apply the transformation to b.
if ~isempty(b)
tau = rho*(u'*b(i));
b(i) = b(i) - tau*u;
end
end
if nargout == 0
clc
A
if ~isempty(b), b, end
pause
end
end
QUADTX
function [Q,fcount] = quadtx(F,a,b,tol,varargin)
%QUADTX Evaluate definite integral numerically.
% Q = QUADTX(F,A,B) approximates the integral of F(x) from A to B
% to within a tolerance of 1.e-6. F is a string defining a function
% of a single variable, an inline function, a function handle, or a
% symbolic expression involving a single variable.
%
% Q = QUADTX(F,A,B,tol) uses the given tolerance instead of 1.e-6.
%
% Arguments beyond the first four, Q = QUADTX(F,a,b,tol,p1,p2,...),
% are passed on to the integrand, F(x,p1,p2,..).
%
% [Q,fcount] = QUADTX(F,...) also counts the number of evaluations
% of F(x).
%
% See also QUAD, QUADL, DBLQUAD, QUADGUI.
% Make F callable by feval.
if ischar(F) & exist(F)~=2
F = inline(F);
elseif isa(F,'sym')
F = inline(char(F));
end
% Default tolerance
if nargin < 4 | isempty(tol)
tol = 1.e-6;
end
% Initialization
c = (a + b)/2;
fa = feval(F,a,varargin{:});
fc = feval(F,c,varargin{:});
fb = feval(F,b,varargin{:});
% Recursive call
[Q,k] = quadtxstep(F, a, b, tol, fa, fc, fb, varargin{:});
fcount = k + 3;
% ---------------------------------------------------------
function [Q,fcount] = quadtxstep(F,a,b,tol,fa,fc,fb,varargin)
% Recursive subfunction used by quadtx.
h = b - a;
c = (a + b)/2;
fd = feval(F,(a+c)/2,varargin{:});
fe = feval(F,(c+b)/2,varargin{:});
Q1 = h/6 * (fa + 4*fc + fb);
Q2 = h/12 * (fa + 4*fd + 2*fc + 4*fe + fb);
if abs(Q2 - Q1) <= tol
Q = Q2 + (Q2 - Q1)/15;
fcount = 2;
else
[Qa,ka] = quadtxstep(F, a, c, tol, fa, fd, fc, varargin{:});
[Qb,kb] = quadtxstep(F, c, b, tol, fc, fe, fb, varargin{:});
Q = Qa + Qb;
fcount = ka + kb + 2;
end
RESTRICTED
function dydt = restricted(t,y)
mu = 1 / 82.45;
mustar = 1 - mu;
r13 = ((y(1) + mu)^2 + y(2)^2) ^ 1.5;
r23 = ((y(1) - mustar)^2 + y(2)^2) ^ 1.5;
dydt = [ y(3)
y(4)
(2*y(4) + y(1) - mustar*((y(1)+mu)/r13) - mu*((y(1)-mustar)/r23))
(-2*y(3) + y(2) - mustar*(y(2)/r13) - mu*(y(2)/r23)) ];
SIMPSON
% This function computes the
% Simpson quadrature rule for
% computing the integral of f(x) on
% the interval [a,b]
function I = simpson(fname,a,b)
fa = feval(fname,a);
fm = feval(fname, (a+b)/2);
fb = feval(fname, b);
I = ( fa + 4*fm + fb)*(b-a)/6;
SIMPSONCOM
% This function computes
% the Simpson composite quadrature rule
% with n subintervals
function I = simpsoncom(fname,a,b,n);
h = (b-a)/n;
x = [a:h:b];
f = feval(fname, x);
I = 0;
for k = 1:n
I = I + simpson('fname',x(k),x(k+1));
end
SPLINESLOPES
function d = splineslopes(h,delta)
% SPLINESLOPES Slopes for cubic spline interpolation.
% splineslopes(h,delta) computes d(k) = S'(x(k)).
% Uses not-a-knot end conditions.
% Diagonals of tridiagonal system
n = length(h)+1;
a = zeros(size(h)); b = a; c = a; r = a;
a(1:n-2) = h(2:n-1);
a(n-1) = h(n-2)+h(n-1);
b(1) = h(2);
b(2:n-1) = 2*(h(2:n-1)+h(1:n-2));
b(n) = h(n-2);
c(1) = h(1)+h(2);
c(2:n-1) = h(1:n-2);
% Right-hand side
r(1) = ((h(1)+2*c(1))*h(2)*delta(1)+h(1)^2*delta(2))/c(1);
r(2:n-1) = 3*(h(2:n-1).*delta(1:n-2)+h(1:n-2).*delta(2:n-1));
r(n) = (h(n-1)^2*delta(n-2)+(2*a(n-1)+h(n-1))*h(n-2)*delta(n-1))/a(n-1);
% Solve tridiagonal linear system
d = tridisolve(a,b,c,r);
SPLINTEX
function v = splinetx(x,y,u)
%SPLINETX Textbook spline function.
% v = splinetx(x,y,u) finds the piecewise cubic interpolatory
% spline S(x), with S(x(j)) = y(j), and returns v(k) = S(u(k)).
%
% See SPLINE, PCHIPTX.
% First derivatives
h = diff(x);
delta = diff(y)./h;
d = splineslopes(h,delta);
% Piecewise polynomial coefficients
n = length(x);
c = (3*delta - 2*d(1:n-1) - d(2:n))./h;
b = (d(1:n-1) - 2*delta + d(2:n))./h.^2;
% Find subinterval indices k so that x(k) <= u < x(k+1)
k = ones(size(u));
for j = 2:n-1
k(x(j) <= u) = j;
end
% Evaluate spline
s = u - x(k);
v = y(k) + s.*(d(k) + s.*(c(k) + s.*b(k)));
% -------------------------------------------------------
TRAPCOM
% This function computes
% the composite trapezoid quadrature rule with
% n subintervals
function I = trapezoid(fname,a,b,n);
h = (b-a)/n;
x = [a:h:b];
f = feval(fname, x);
I = h*(sum(f)-(f(1)+ f(length(f)))/2);
TWOBODY
function ydot = twobody(t,y)
r = sqrt(y(1)^2 + y(2)^2);
ydot = [y(3); y(4); -y(1)/r^3 ; -y(2)/r^3];
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Enviado por: | El remitente no desea revelar su nombre |
Idioma: | castellano |
País: | España |