I have read that spacecraft use two mid-course corrections to approach the Lagrange point, then do a final orbital insertion maneuver to enter into a halo orbit.
Are there any specifics about this maneuver that can be explained to me considering I did not get through Classical Mechanics in my college days, many decades ago, so a highly technical answer will be way over my head.
I understand that halo orbits are constrained to one plane where lissajous orbits are not.
Is there a distinct difference between such a maneuver for a halo orbit compared to a lissajous orbit?