Quasi newton method for NLP code problem
Show older comments
Hello, Can some one tell whats wrong with the following program ? I tried to change x and evaluate V but I got some difficulties to run. Is there any built in function to solve PRSopt_QN with quasi-newton ?
function V = PRSopt_QN(radius,alpha,beta)
L=1;
z=0.7071068;
ts=1/2;
t=0:ts:1;
for k=1:length(t)
xi_2=beta(k);
rp=radius(k);
for j=1:length(t)
xi_1=0;
xi_2=alpha(j);
xi_3=beta(j);
th(j)=-0.2*cos(2*pi*t(j));
psi(k)=0.2*sin(2*pi*t(k));
phi(j)=atan2(sin(psi(k))*sin(th(j)),(cos(psi(k))+cos(th(j))));
R=Rot('y',th(j))*Rot('x',psi(k))*Rot('z',phi(j));
x(k)=1/2*rp*(-cos(phi(j))*cos(psi(k))+cos(phi(j))*cos(th(j))+sin(phi(j))*sin(psi(k))*sin(th(j)));
y(k)=-rp*cos(psi(k))*sin(phi(j));
zc(k)=z;
delta(k)=sqrt(x(k)^2+y(k)^2)
p=[x(k);y(k);zc(k)];
a1(:,k)=R*[rp;0;0];
a2(:,k)=R*[rp*cos(xi_2);rp*sin(xi_2);0];
a3(:,k)=R*[rp*cos(xi_3);rp*sin(xi_3);0];
r1=p+R*[rp;0;0];
r2=p+R*[rp*cos(xi_2);rp*sin(xi_2);0];
r3=p+R*[rp*cos(xi_3);rp*sin(xi_3);0];
P=1/3*(r1+r2+r3);
g1=inv(Rot('z',0))*r1;
g2=inv(Rot('z',xi_2))*r2;
g3=inv(Rot('z',xi_3))*r3;
% leg length
b1(k)=g1(1)+sqrt(L^2-g1(3)^2);
b2(k)=g2(1)+sqrt(L^2-g2(3)^2);
b3(k)=g3(1)+sqrt(L^2-g3(3)^2);
% passive koint value
sin_th21=(g1(1)-b1(k))/L;
cos_th21=g1(3)/L;
th21(k)=atan2(sin_th21,cos_th21);
sin_th22=(g2(1)-b2(k))/L;
cos_th22=g2(3)/L;
th22(k)=atan2(sin_th22,cos_th22);
sin_th23=(g3(1)-b3(k))/L;
cos_th23=g3(3)/L;
th23(k)=atan2(sin_th23,cos_th23);
pr1(k)=norm(r1-p);
pr2(k)=norm(r3-p);
pr3(k)=norm(r3-p);
r12(k)=norm(r1-r2);
r23(k)=norm(r3-r2);
r31(k)=norm(r3-r1);
Link1(k)=norm(r1-[b1(k);0;0]);
Link2(k)=norm(r2-Rot('z',xi_2)*[b2(k);0;0]);
Link3(k)=norm(r3-Rot('z',xi_3)*[b3(k);0;0]);
s21=[0;1;0];
s22=[-sin(xi_2);cos(xi_2);0];
s23=[-sin(xi_3);cos(xi_3);0];
Constraint1(k)=(p+a1(:,k))'*s21;
Constraint2(k)=(p+a2(:,k))'*s22;
Constraint3(k)=(p+a3(:,k))'*s23;
Gc=[s21',cross(s21,a1(:,k))';s22',cross(s22,a2(:,k))';s23',cross(s23,a3(:,k))'];
M=[eye(6)-transpose(Gc)*pinv((transpose(Gc)))];
st(:,k)=[0.2*cos(2*pi*t(k))*0;0.2*sin(2*pi*t(k))*0;2*cos(2*pi*t(k))*0;2*cos(2*pi*t(k));2*sin(2*pi*t(k));-0.02*cos(2*pi*t(k))*0]; % Desired task velocity
stm(:,k)=M*st(:,k)
wx(k)=st(4,k);
wy(k)=st(5,k);
vz(k)=stm(3,k);
C1=[-sin(xi_1) cos(xi_1) -(a1(1)*cos(xi_1)+a1(2)*sin(xi_1)) ; -sin(xi_2) cos(xi_2) -(a2(1)*cos(xi_2)+a2(2)*sin(xi_2)) ; -sin( xi_3) cos( xi_3) -(a3(1)*cos( xi_3)+a3(2)*sin( xi_3)) ];
C2=[-a1(3)*cos(xi_1) -a1(3)*sin(xi_1) ;-a2(3)*cos(xi_2) -a2(3)*sin(xi_2);-a3(3)*cos( xi_3) -a3(3)*sin( xi_3)]
V(:,k)=(inv(C1)*C2)*[wx(k);wy(k)];
Stm(:,k)=M*[V(1,k);V(2,k);vz(k);wx(k);wy(k);V(3,k)]
constraint2(:,k)=Gc*Stm(:,k)
constraint1(:,k)=Gc*stm(:,k)
con1(k)=constraint1(1,k);
con2(k)=constraint1(2,k);
con3(k)=constraint1(3,k);
end
end
return;
end
%%
function Rotation = Rot(char,a)
c=cos(a); s=sin(a);
switch char
case 'x'
Rotation =[1, 0, 0;
0, c, -s;
0, s, c];
case 'y'
Rotation = [c, 0, s;
0, 1, 0;
-s, 0, c];
case 'z'
Rotation = [c, -s, 0;
s, c, 0;
0, 0, 1];
end
Accepted Answer
More Answers (0)
Categories
Find more on Solver Outputs and Iterative Display in Help Center and File Exchange
Community Treasure Hunt
Find the treasures in MATLAB Central and discover how the community can help you!
Start Hunting!