% state calculations
% Gisle Otto Eikrem
% 12.05.04

weight = 2/3;

i = 12000;

% m_a = m(1,i); 
% m_gt = m(2,i);
% m_wt = m(3,i); 

x_1 = (1-weight)*m(1,i) + weight*m(1,i+1)
x_2 = (1-weight)*m(2,i) + weight*m(2,i+1)
x_3 = (1-weight)*m(3,i) + weight*m(3,i+1)

