function [k,m]=feframe2(el,xi,leng,area,rho,beta,ipt)

%--------------------------------------------------------------
%  Purpose:
%     Stiffness and mass matrices for the 2-d frame element
%     nodal dof {u_1 v_1 theta_1 u_2 v_2 theta_2}
%
%  Synopsis:
%     [k,m]=feframe2(el,xi,leng,area,rho,beta,ipt) 
%
%  Variable Description:
%     k - element stiffness matrix (size of 6x6)   
%     m - element mass matrix (size of 6x6)
%     el - elastic modulus 
%     xi - second moment of inertia of cross-section
%     leng - element length
%     area - area of beam cross-section
%     rho - mass density (mass per unit volume)
%     beta - angle between the local and global axes                                 ipt = 1: consistent mass matrix
%            is positive if the local axis is in the ccw direction from
%            the global axis
%     ipt = 1 - consistent mass matrix
%         = 2 - lumped mass matrix
%         = 3 - diagonal mass matrix
%--------------------------------------------------------------------------

% stiffness matrix at the local axis

 a=el*area/leng;
 c=el*xi/(leng^3);
 kl=[a   0           0            -a     0          0;...
     0   12*c        6*leng*c      0    -12* c      6*leng*c;...
     0   6*leng*c    4*leng^2*c    0    -6*leng*c   2*leng^2*c;...
    -a   0           0             a     0          0;...
     0  -12*c       -6*leng*c      0     12*c      -6*leng*c;...
     0   6*leng*c    2*leng^2*c    0    -6*leng*c   4*leng^2*c];
   
% rotation matrix

 r=[ cos(beta)  sin(beta)  0   0          0         0;...
    -sin(beta)  cos(beta)  0   0          0         0;...
     0          0          1   0          0         0;...
     0          0          0   cos(beta)  sin(beta) 0;...
     0          0          0  -sin(beta)  cos(beta) 0;...
     0          0          0   0          0         1];

% stiffness matrix at the global axis

 k=r'*kl*r;


% consistent mass matrix

 if ipt==1

    mm=rho*area*leng/420;
    ma=rho*area*leng/6;
    ml=[2*ma  0           0            ma    0            0;...
        0     156*mm      22*leng*mm   0     54*mm       -13*leng*mm;...
        0     22*leng*mm  4*leng^2*mm  0     13*leng*mm  -3*leng^2*mm;...
        ma    0           0            2*ma  0            0;...
        0     54*mm       13*leng*mm   0     156*mm      -22*leng*mm;...
        0    -13*leng*mm -3*leng^2*mm  0    -22*leng*mm   4*leng^2*mm];
  
% lumped mass matrix

 elseif ipt==2

    ml=zeros(6,6);
    mass=rho*area*leng;
    ml=mass*diag([0.5  0.5  0  0.5  0.5  0]);

% diagonal mass matrix

 else

    ml=zeros(6,6);
    mass=rho*area*leng;
    ml=mass*diag([0.5  0.5  leng^2/78  0.5  0.5  leng^2/78]);

end
 
% mass in the global system

    m=r'*ml*r;