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Fullload=75;Ia=4.55;Vl=2200;
Fulload=Fullload/100
Ih=Fullload*Ia
function[x,y]=polar2rect(r,theta)
x=r*cos(theta*%pi/180);
y=r*sin(theta*%pi/180);
endfunction
[x1,y1]=polar2rect(Vl,0)
[x2,y2]=polar2rect(35.46,-53.13)
[x3,y3]=polar2rect(106.73,36.87)
X1=x1+%i*y1
X2=x2+%i*y2
X3=x3+%i*y3
X=X1+X2+X3
function[r,theta]=rect2polar(x,y)
r=sqrt(x^2+y^2);
theta=atan(y/x)*180/%pi;
endfunction
[V,Angle]=rect2polar(2306.5,35.67)
VolReg=(V-Vl)/Vl*100
function[x,y]=polar2rect(r,theta)
x=r*cos(theta*%pi/180);
y=r*sin(theta*%pi/180);
endfunction
[x1,y1]=polar2rect(Vl,0)
[x2,y2]=polar2rect(35.46,53.13)
[x3,y3]=polar2rect(106.73,143.13)
X1=x1+%i*y1
X2=x2+%i*y2
X3=x3+%i*y3
X=X1+X2+X3
function[r,theta]=rect2polar(x,y)
r=sqrt(x^2+y^2);
theta=atan(y/x)*180/%pi;
endfunction
[V1,Angle1]=rect2polar(2135.89,92.4)
VolReg=(V1-Vl)/Vl*100
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