There are 2 circular orbits with different inclination and RAAN. I have to transfer from a specific point (true anomaly given) of one orbit to a given point of another in 1 month. The period of the orbits is 1 year.
Currently, I'm solving Lambert problem, using 2 maneuvers and it works. However, it may be more optimal to use up to 5 maneuvers. Thats's to say, changing the velocity in flight, not only in the beginning and at the end.
I would appreciate for explanation.