%Feature extraction for files with 5000 points function [Fault,f,y]=calculo_m(Featurefile) %file could be bearing, gearmesh, imbalance, misalignment or resonance M=zeros(1000,5); for i=1:5 M(:,i)=Featurefile((1+1000*(i-1)):(i*1000),1); end %Normalised M, each column of N is xi N=zeros(1000,5); for j=1:5 N(:,j)=M(:,j)-mean(M(:,j)); end %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%% %Feature 1: the Root Mean Square(RMS) of the signal %PSD of each column of N y=zeros(129,5); f=zeros(129,5); for k=1:5 [y(:,k),f(:,k)]=pwelch(N(:,k),[],[],[],1000); end ONE=zeros(5,1); for i=1:5 ONE(i,1)=norm(y(:,i))/sqrt(1000); end %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%% %Feature 2: RMS of low frequencies 0-50 Hz %each column of N is filtered J=zeros(1000,5); [B,A]=butter(11,0.1); for j=1:5 J(:,j)=filter(B,A,N(:,j)); end %PSD of each column of J y2=zeros(129,5); f2=zeros(129,5); for k=1:5 [y2(:,k),f2(:,k)]=pwelch(J(:,k),[],[],[],1000); end TWO=zeros(5,1); for i=1:5 TWO(i,1)=norm(y2(:,i))/sqrt(1000); end %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%% %Feature 3: RMS of middle frequencies 50-200 Hz %each column of N is filtered J=zeros(1000,5); [B,A]=butter(13,[0.1 0.4]); for j=1:5 J(:,j)=filter(B,A,N(:,j)); end %PSD of each column of J y3=zeros(129,5); f3=zeros(129,5); for k=1:5 [y3(:,k),f3(:,k)]=pwelch(J(:,k),[],[],[],1000); end THREE=zeros(5,1); for i=1:5 THREE(i,1)=norm(y3(:,i))/sqrt(1000); end %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%% %Feature 4: RMS of high frequencies 200-500 Hz %each column of N is filtered J=zeros(1000,5); [B,A]=butter(18,0.4,'high'); for j=1:5 J(:,j)=filter(B,A,N(:,j)); end %PSD of each column of J y4=zeros(129,5); f4=zeros(129,5); for k=1:5 [y4(:,k),f4(:,k)]=pwelch(J(:,k),[],[],[],1000); end FOUR=zeros(5,1); for i=1:5 FOUR(i,1)=norm(y4(:,i))/sqrt(1000); end %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%% Fault=zeros(5,4); for m=1:5 Fault(m,1)=ONE(m,1); Fault(m,2)=TWO(m,1); Fault(m,3)=THREE(m,1); Fault(m,4)=FOUR(m,1); end e-REdING. Biblioteca de la Escuela Superior de Ingenieros de Sevilla.


SISTEMA DE MONITORIZACIÓN DE TURBINAS DE GAS AERONÁUTICAS

: Rodríguez Barquero, María
: Ingeniería Industrial
Contenido del proyecto: