how to solve "Error using alpha. Too many output arguments."
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I am getting "Error using alpha. Too many output arguments." after alpha3. Can someone help me resolve this?
%
clear all
close all
% Given
a=3;
b=13;
c=0;
rPA=b/2;
rPB=c/2;
theta2=100; % degrees
theta4=90; % degrees
omega2=2000*2*pi/60; % rpm
alpha2=10; % rad/s^2
w2=1; %lb
w3=2; %lb
w4=4; %lb
g=32.2;
m2=w2/g;
m3=w3/g;
m4=w4/g;
I2=0.02; %lb.ft.s^2
I3=0.08; %lb.ft.s^2
F=[-1000-500]; %lb
% Open Circuit
theta32=asind((-a*sind(theta2)+c)/b)+180;
d2=a*cosd(theta2)-b*cosd(theta32);
% Crossed Circuit
theta31=asind((a*sind(theta2)-c)/b);
d1=(a*cosd(theta2))-(b*cosd(theta31));
% Find torqe T12, pin force F12, pin force F32, pin force F43
theta3=asind((-a*sind(theta2)+c)/b)+180;
omega3=a*omega2*cosd(theta2)/(b*cosd(theta3));
ddot=-a*omega2*sind(theta2)+b*omega3*sind(theta3);
alpha3=(a*alpha*cosd(theta2)-a*omega2^2*sind(theta2)+b*omega3^2*sind(theta3))/(b*cosd(theta3));
Dddot=-a*alpha2*sind(theta2)-a*omega2^2*cosd(theta2)+b*alpha3*sind(theta3)+b*omega3^2*cosd(theta3);
Aa=[-a*alpha2*sind(theta2)-a*omega2^2*cosd(theta2); a*alpha2*cosd(theta2)-a*omega2^2*sind(theta2)];
Ab=[Dddot;0];
R2=a*[cosd(theta2);sind(theta2)];
R12=-R2/2;
R32=R2/2;
R3=b*[cosd(theta3);sind(theta3)];
R23=R3/2;
R43=-R3/2;
rG2=a/2;
rG3=b/2;
A2=[-rG2*alpha2*sind(theta2)-rG2*omega2^2*cosd(theta2); ...
rG2*alpha2*cosd(theta2)-rG2*omega2^2*sind(theta2)];
Aa=[-a*alpha2*sind(theta2)-a*omega2^2*cosd(theta2); a*alpha2*cosd(theta2)-a*omega2^2*sind(theta2)];
Ag3a=[-rG3*alpha3*sind(theta3)-rG3*omega3^2*cosd(theta3);...
rG3*alpha3*cosd(theta3)-rG3*omega3^2*sind(theta3)];
A3=Aa-Ag3a;
A4=[Dddot;0];
A=[1 0 1 0 0 0 0 0
0 1 0 1 0 0 0 0
-R12(2) R12(1) -R32(2) R32(1) 0 0 0 1
0 0 -1 0 1 0 0 0
0 0 0 -1 0 1 0 0
0 0 R23(2) -R23(1) -R43(2) R43(1) 0 0
0 0 0 0 -1 0 mu 0
0 0 0 0 0 -1 1 0];
B=[m2*A2(1)
m2*A2(2)
I2*alpha2
m3*A3(1)
m3*A3(2)
I3*alpha3
m4*A4(1)-F(1)
-F(2)];
F=A\B
Antworten (1)
KALYAN ACHARJYA
am 29 Nov. 2019
Bearbeitet: KALYAN ACHARJYA
am 29 Nov. 2019
#Done with some minor changed, also mu to m2 (There is no mu variable)
% Given
a=3;
b=13;
c=0;
rPA=b/2;
rPB=c/2;
theta2=100; % degrees
theta4=90; % degrees
omega2=2000*2*pi/60; % rpm
alpha2=10; % rad/s^2
w2=1; %lb
w3=2; %lb
w4=4; %lb
g=32.2;
m2=w2/g;
m3=w3/g;
m4=w4/g;
I2=0.02; %lb.ft.s^2
I3=0.08; %lb.ft.s^2
F=[-1000 -500]; %lb
% Open Circuit
theta32=asind((-a*sind(theta2)+c)/b)+180;
d2=a*cosd(theta2)-b*cosd(theta32);
% Crossed Circuit
theta31=asind((a*sind(theta2)-c)/b);
d1=(a*cosd(theta2))-(b*cosd(theta31));
% Find torqe T12, pin force F12, pin force F32, pin force F43
theta3=asind((-a*sind(theta2)+c)/b)+180;
omega3=a*omega2*cosd(theta2)/(b*cosd(theta3));
ddot=-a*omega2*sind(theta2)+b*omega3*sind(theta3);
alpha3=(a*alpha2*cosd(theta2)-a*omega2^2*sind(theta2)+b*omega3^2*sind(theta3))/(b*cosd(theta3));
Dddot=-a*alpha2*sind(theta2)-a*omega2^2*cosd(theta2)+b*alpha3*sind(theta3)+b*omega3^2*cosd(theta3);
Aa=[-a*alpha2*sind(theta2)-a*omega2^2*cosd(theta2); a*alpha2*cosd(theta2)-a*omega2^2*sind(theta2)];
Ab=[Dddot;0];
R2=a*[cosd(theta2);sind(theta2)];
R12=-R2/2;
R32=R2/2;
R3=b*[cosd(theta3);sind(theta3)];
R23=R3/2;
R43=-R3/2;
rG2=a/2;
rG3=b/2;
A2=[-rG2*alpha2*sind(theta2)-rG2*omega2^2*cosd(theta2); ...
rG2*alpha2*cosd(theta2)-rG2*omega2^2*sind(theta2)];
Aa=[-a*alpha2*sind(theta2)-a*omega2^2*cosd(theta2); a*alpha2*cosd(theta2)-a*omega2^2*sind(theta2)];
Ag3a=[-rG3*alpha3*sind(theta3)-rG3*omega3^2*cosd(theta3);...
rG3*alpha3*cosd(theta3)-rG3*omega3^2*sind(theta3)];
A3=Aa-Ag3a;
A4=[Dddot;0];
A=[1 0 1 0 0 0 0 0
0 1 0 1 0 0 0 0
-R12(2) R12(1) -R32(2) R32(1) 0 0 0 1
0 0 -1 0 1 0 0 0
0 0 0 -1 0 1 0 0
0 0 R23(2) -R23(1) -R43(2) R43(1) 0 0
0 0 0 0 -1 0 m2 0
0 0 0 0 0 -1 1 0];
B=[m2*A2(1)
m2*A2(2)
I2*alpha2
m3*A3(1)
m3*A3(2)
I3*alpha3
m4*A4(1)-F(1)
-F(2)];
F=A\B

5 Kommentare
Sencer Comert
am 29 Nov. 2019
Bearbeitet: KALYAN ACHARJYA
am 29 Nov. 2019
KALYAN ACHARJYA
am 29 Nov. 2019
Bearbeitet: KALYAN ACHARJYA
am 29 Nov. 2019
%
a=3;
b=13;
c=0;
theta2=100; % degrees
theta4=90; % degrees
omega2=2000*2*pi/60; % rpm
alpha2=10; % rad/s^2
w2=1; %lb
w3=2; %lb
w4=4; %lb
g=32.2;
m2=w2/g;
m3=w3/g;
m4=w4/g;
I2=0.02; %lb.ft.s^2
I3=0.08; %lb.ft.s^2
F=[-1000 -500]; %lb
mu=0;
%Open Circuit
theta32=asind((-a*sind(theta2)+c)/b)+180;
d2=a*cosd(theta2)-b*cosd(theta32);
%Crossed Circuit
theta31=asind((a*sind(theta2)-c)/b);
d1=(a*cosd(theta2))-(b*cosd(theta31));
% Find torqe T12, pin force F12, pin force F32, pin force F43
theta3=asind((-a*sind(theta2)+c)/b)+180;
omega3=a*omega2*cosd(theta2)/(b*cosd(theta3));
ddot=-a*omega2*sind(theta2)+b*omega3*sind(theta3);
alpha3=(a*alpha2*cosd(theta2)-a*omega2^2*sind(theta2)+b*omega3^2*sind(theta3))/(b*cosd(theta3));
Dddot=-a*alpha2*sind(theta2)-a*omega2^2*cosd(theta2)+b*alpha3*sind(theta3)+b*omega3^2*cosd(theta3);
Aa=[-a*alpha2*sind(theta2)-a*omega2^2*cosd(theta2); a*alpha2*cosd(theta2)-a*omega2^2*sind(theta2)];
Ab=[Dddot;0];
R2=a*[cosd(theta2);sind(theta2)];
R12=-R2/2;
R32=R2/2;
R3=b*[cosd(theta3);sind(theta3)];
R23=R3/2;
R43=-R3/2;
rG2=a/2;
rG3=b/2;
A2=[-rG2*alpha2*sind(theta2)-rG2*omega2^2*cosd(theta2); ...
rG2*alpha2*cosd(theta2)-rG2*omega2^2*sind(theta2)];
Aa=[-a*alpha2*sind(theta2)-a*omega2^2*cosd(theta2); a*alpha2*cosd(theta2)-a*omega2^2*sind(theta2)];
Ag3a=[-rG3*alpha3*sind(theta3)-rG3*omega3^2*cosd(theta3);...
rG3*alpha3*cosd(theta3)-rG3*omega3^2*sind(theta3)];
A3=Aa-Ag3a;
A4=[Dddot;0];
A=[1 0 1 0 0 0 0 0
0 1 0 1 0 0 0 0
-R12(2) R12(1) -R32(2) R32(1) 0 0 0 1
0 0 -1 0 1 0 0 0
0 0 0 -1 0 1 0 0
0 0 R23(2) -R23(1) -R43(2) R43(1) 0 0
0 0 0 0 -1 0 mu 0
0 0 0 0 0 -1 1 0];
B=[m2*A2(1)
m2*A2(2)
I2*alpha2
m3*A3(1)
m3*A3(2)
I3*alpha3
m4*A4(1)-F(1)
-F(2)];
F=A\B
% For 2 rev, plot torqe T12, pin force F12, pin force F32, pin force F43 on same graph as function of theta2
THETA2=0:1:360;
for i=1:1:length(THETA2)
theta2=THETA2(i);
theta3=asind((-a*sind(theta2)+c)/b)+180;
omega3=a*omega2*cosd(theta2)/(b*cosd(theta3));
alpha3=(a*alpha2*cosd(theta2)-a*omega2^2*sind(theta2)+b*omega3^2*sind(theta3))/(b*cosd(theta3));
Dddot=-a*alpha2*sind(theta2)-a*omega2^2*cosd(theta2)+b*alpha3*sind(theta3)+b*omega3^2*cosd(theta3);
Aa=[-a*alpha2*sind(theta2)-a*omega2^2*cosd(theta2); a*alpha2*cosd(theta2)-a*omega2^2*sind(theta2)];
Ab=[Dddot;0];
g=32.2;
W2=1;
W3=2;
W4=4;
mu=0.4;
m2=W2/g;
m3=W3/g;
m4=W4/g;
I2=0.02;
I3=0.8;
F=[-1000;-500];
R2=a*[cosd(theta2);sind(theta2)];
R12=-R2/2;
R32=R2/2;
R3=b*[cosd(theta3);sind(theta3)];
R23=R3/2;
R43=-R3/2;
rG2=a/2;
rG3=b/2;
A2=[-rG2*alpha2*sind(theta2)-rG2*omega2^2*cosd(theta2); ...
rG2*alpha2*cosd(theta2)-rG2*omega2^2*sind(theta2)];
Aa=[-a*alpha2*sind(theta2)-a*omega2^2*cosd(theta2); a*alpha2*cosd(theta2)-a*omega2^2*sind(theta2)];
Ag3a=[-rG3*alpha3*sind(theta3)-rG3*omega3^2*cosd(theta3);...
rG3*alpha3*cosd(theta3)-rG3*omega3^2*sind(theta3)];
A3=Aa-Ag3a;
A4=[Dddot;0];
A=[1 0 1 0 0 0 0 0
0 1 0 1 0 0 0 0
-R12(2) R12(1) -R32(2) R32(1) 0 0 0 1
0 0 -1 0 1 0 0 0
0 0 0 -1 0 1 0 0
0 0 R23(2) -R23(1) -R43(2) R43(1) 0 0
0 0 0 0 -1 0 mu 0
0 0 0 0 0 -1 1 0];
B=[m2*A2(1)
m2*A2(2)
I2*alpha2
m3*A3(1)
m3*A3(2)
I3*alpha3
m4*A4(1)-F(1)
-F(2)];
F=A\B;
T21(i)=-F(8);
f12(i)=norm([F(1);F(2)]);
f32(i)=norm([F(3);F(4)]);
f43(i)=norm([F(5);F(6)]);
end
plot(THETA2,T21,THETA2,f12,THETA2,f32,THETA2,f43)
grid minor
legend('T21','F12','F32','F43')
legend('Location','north')
set(gcf,'Visible','on')
grid minor

Sencer Comert
am 29 Nov. 2019
KALYAN ACHARJYA
am 29 Nov. 2019
Please copy my answer (code) and execute it
Sencer Comert
am 29 Nov. 2019
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