fn main() {
    // This code adapted from here: https://www.topopt.mek.dtu.dk/apps-and-software/a-99-line-topology-optimization-code-written-in-matlab
    let script = "
        function x = top(nelx,nely,volfrac,penal,rmin);
            % INITIALIZE
            x(1:nely,1:nelx) = volfrac;
            loop = 0;
            change = 1.;
            % START ITERATION
            while change > 0.01
              loop = loop + 1;
              xold = x;
            % FE-ANALYSIS
              [U]=FE(nelx,nely,x,penal);
            % OBJECTIVE FUNCTION AND SENSITIVITY ANALYSIS
              [KE] = lk;
              c = 0.;
              for ely = 1:nely
                for elx = 1:nelx
                  n1 = (nely+1)*(elx-1)+ely;
                  n2 = (nely+1)* elx   +ely;
                  Ue = U([2*n1-1;2*n1; 2*n2-1;2*n2; 2*n2+1;2*n2+2; 2*n1+1;2*n1+2],1);
                  c = c + x(ely,elx)^penal*Ue'*KE*Ue;
                  dc(ely,elx) = -penal*x(ely,elx)^(penal-1)*Ue'*KE*Ue;
                end
              end
            % FILTERING OF SENSITIVITIES
              [dc]   = check(nelx,nely,rmin,x,dc);
            % DESIGN UPDATE BY THE OPTIMALITY CRITERIA METHOD
              [x]    = OC(nelx,nely,x,volfrac,dc);
            % PRINT RESULTS
              change = max(max(abs(x-xold)));
              disp([' It.: ' sprintf('%4i',loop) ' Obj.: ' sprintf('%10.4f',c) ...
                   ' Vol.: ' sprintf('%6.3f',sum(sum(x))/(nelx*nely)) ...
                    ' ch.: ' sprintf('%6.3f',change )])
            % PLOT DENSITIES
              % colormap(gray); imagesc(-x); axis equal; axis tight; axis off;pause(1e-6);
            end
            %%%%%%%%%% OPTIMALITY CRITERIA UPDATE %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
            function [xnew]=OC(nelx,nely,x,volfrac,dc)
                l1 = 0; l2 = 100000; move = 0.2;
                while (l2-l1 > 1e-4)
                    lmid = 0.5*(l2+l1);
                    xnew = max(0.001,max(x-move,min(1.,min(x+move,x.*sqrt(-dc./lmid)))));
                    if sum(sum(xnew)) - volfrac*nelx*nely > 0;
                        l1 = lmid;
                    else
                        l2 = lmid;
                    end
                end
            end
            %%%%%%%%%% MESH-INDEPENDENCY FILTER %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
            function [dcn]=check(nelx,nely,rmin,x,dc)
                dcn=zeros(nely,nelx);
                for i = 1:nelx
                  for j = 1:nely
                    ssum=0.0;
                    for k = max(i-floor(rmin),1):min(i+floor(rmin),nelx)
                      for l = max(j-floor(rmin),1):min(j+floor(rmin),nely)
                        fac = rmin-sqrt((i-k)^2+(j-l)^2);
                        ssum = ssum+max(0,fac);
                        dcn(j,i) = dcn(j,i) + max(0,fac)*x(l,k)*dc(l,k);
                      end
                    end
                    dcn(j,i) = dcn(j,i)/(x(j,i)*ssum);
                  end
                end
            end
            %%%%%%%%%% FE-ANALYSIS %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
            function [U]=FE(nelx,nely,x,penal)
                [KE] = lk;
                K = sparse(2*(nelx+1)*(nely+1), 2*(nelx+1)*(nely+1));
                F = sparse(2*(nely+1)*(nelx+1),1); U = zeros(2*(nely+1)*(nelx+1),1);
                for elx = 1:nelx
                  for ely = 1:nely
                    n1 = (nely+1)*(elx-1)+ely;
                    n2 = (nely+1)* elx   +ely;
                    edof = [2*n1-1; 2*n1; 2*n2-1; 2*n2; 2*n2+1; 2*n2+2; 2*n1+1; 2*n1+2];
                    K(edof,edof) = K(edof,edof) + x(ely,elx)^penal*KE;
                  end
                end
                % DEFINE LOADS AND SUPPORTS (HALF MBB-BEAM)
                F(2,1) = -1;
                fixeddofs   = union([1:2:2*(nely+1)],[2*(nelx+1)*(nely+1)]);
                alldofs     = [1:2*(nely+1)*(nelx+1)];
                freedofs    = setdiff(alldofs,fixeddofs);
                % SOLVING
                U(freedofs,:) = K(freedofs,freedofs) \\ F(freedofs,:);
                U(fixeddofs,:)= 0;
            end
            %%%%%%%%%% ELEMENT STIFFNESS MATRIX %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
            function [KE]=lk()
                E = 1.;
                nu = 0.3;
                k=[ 1/2-nu/6   1/8+nu/8 -1/4-nu/12 -1/8+3*nu/8 ...
                   -1/4+nu/12 -1/8-nu/8  nu/6       1/8-3*nu/8];
                KE = E/(1-nu^2)*[ k(1) k(2) k(3) k(4) k(5) k(6) k(7) k(8)
                                  k(2) k(1) k(8) k(7) k(6) k(5) k(4) k(3)
                                  k(3) k(8) k(1) k(6) k(7) k(4) k(5) k(2)
                                  k(4) k(7) k(6) k(1) k(8) k(3) k(2) k(5)
                                  k(5) k(6) k(7) k(8) k(1) k(2) k(3) k(4)
                                  k(6) k(5) k(4) k(3) k(2) k(1) k(8) k(7)
                                  k(7) k(4) k(5) k(2) k(3) k(8) k(1) k(6)
                                  k(8) k(3) k(2) k(5) k(4) k(7) k(6) k(1)];
            end
        end


    z = top(10,10,0.5,3,3);
    
    ";

    let y = mocktave::eval(script);

    println!("{y:#?}");
}