Karthi Ramachandran

I wanted to develop Lyapunov(in planar case) /Halo orbits for restricted three body problem using matcont, which I have done using matlab already. where we take help of ODE events function and state transition matrix(STM) of the system to perform differential correction process to obtain the initial condition and then propagate to obtained the orbits and family. However , to obtain the same in Matcont (Note: the problem is point boundary valued) I am not able to figure out how to supply the final...