mn=input('Modül Giriniz:');
T=input('Teeth Numbers :');
at=input('Transverse pressure angle: ');
ad=input('Addendum Coef: ');
de=input('Deddendum Coef :');
Hobtip=input('Hob Tip Radius coef: ');
rg=mn*T/2;
rr=rg-(de*mn);
br=rg*cosd(at);
tr=rg+(ad*mn);
b=(tr-br)/180;
r=br;
a=1;
r2=num2cell(br:b:tr);
inva=tand(at)-(at*pi/180);
ctt1=pi*mn/2;
% Involute Curves
while r<=tr
r=r+b;
a=a+1;
end
for i=1:1:a
teta{i}=acosd(br/r2{i});
invteta{i}=tand(teta{i})-(teta{i}*pi/180);
ctt2{i}=2*r2{i}*((0.5*ctt1/rg)+inva-invteta{i});
B{i}=0.5*ctt2{i}/r2{i};
x{i}=r2{i}*sin( B{i});
y{i}=r2{i}*cos(B{i});
leftx{i}=-1*r2{i}*sin(B{i});
end
% Trochoid Curves
B_tr=(de*mn)-(Hobtip*mn);
L=(pi*mn/4.0)-(B_tr*tand(at))-(Hobtip*mn/(cosd(at)));
W=((((pi*mn)/2.0)-L)/rg);
E=0;
e=E;
Emax=50*pi/180;
tro=Emax/179;
o=1;
E2=num2cell(0:tro:Emax);
while (e<=Emax)
e=e+tro;
o=o+1;
end
for q=1:o
Yz{q}=((rg-B_tr)*cos(E2{q}))+((rg*E2{q}*sin(E2{q})));
Xz{q}=(rg*E2{q}*cos(E2{q}))-((rg-B_tr)*sin(E2{q}));
DXZ{q}=(-(rg*E2{q}).*sin(E2{q}))+((B_tr*cos(E2{q})));
DYZ{q}=(B_tr*sin(E2{q}))+((rg*E2{q})*cos(E2{q}));
if(E==0)
A{q}=90*pi/180.;
end
A{q}=atan(DXZ{q}./DYZ{q});
Xt{q}=Xz{q}+((Hobtip*mn).*cos(A{q}));
Yt{q}=Yz{q}-(Hobtip*mn.*sin(A{q}));
Xtr{q}=Yt{q}.*sin(W)-Xt{q}.*cos(W);
Ytr{q}=Yt{q}.*cos(W)+Xt{q}.*sin(W);
leftXtr{q}=-1.*(Yt{q}.*sin(W)-Xt{q}.*cos(W));
end
% Tooth Curves
% Involute ones
plot(cell2mat(x),cell2mat(y));
hold on
plot(cell2mat(leftx),cell2mat(y));
hold on
% Trochoid Ones
plot(cell2mat(Xtr),cell2mat(Ytr));
hold on
plot(cell2mat(leftXtr),cell2mat(Ytr));

4 Kommentare

index exceeds matrix dimensions "teta{i}=acosd(br/r2{i})
"yz{q}=((rg-b_tr)*cos(e2{q}))+((rg*e2{q}*sin(e2{q})))"
"xz{q}=(rg*e2{q}*cos(e2{q}))-((rg-b_tr)*sin(e2{q})) "
Rik
Rik am 30 Jan. 2019
Have a read here (or here for more general advice). It will greatly improve your chances of getting an answer.
What have you tried to solve this problem yourself? Have you checked the dimensions of the arrays you're indexing when the error occurs?
Could you please define your inputs? So we can run your code?
mn=input('Modül Giriniz:');
T=input('Teeth Numbers :');
at=input('Transverse pressure angle: ');
ad=input('Addendum Coef: ');
de=input('Deddendum Coef :');
Hobtip=input('Hob Tip Radius coef: ');
BAHADIR Karba
BAHADIR Karba am 30 Jan. 2019
Bearbeitet: BAHADIR Karba am 30 Jan. 2019
case 1 :
mn=3
T=20
at=20
ad=1.0
de=1.25
Hobtip=0.38
whenever i used any pertinent inputs programs give errors especially like that
indexing exceed,actually main problem due to double / cells
"teta{i}=acosd(br/r2{i})
"yz{q}=((rg-b_tr)*cos(e2{q}))+((rg*e2{q}*sin(e2{q})))"
"xz{q}=(rg*e2{q}*cos(e2{q}))-((rg-b_tr)*sin(e2{q})) "
Even i take an error like that sometimes,if ı rewrite plots on the command section can show plots correctly,But most of trying give errors and program stopped due to errors

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 Akzeptierte Antwort

Bob Thompson
Bob Thompson am 30 Jan. 2019

1 Stimme

Your first error occurs with teta{i} = acosd(br/r2{i}); because r2 has one less element than the max values of i. I would suggest initializing a as 0 instead of 1.
I did not encounter the other errors.

1 Kommentar

BAHADIR Karba
BAHADIR Karba am 30 Jan. 2019
Yes,I forgot this a and o values must be started from 0;and also solved.
Many thanks ,
Best regards

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