Hello everyone,
I'm currently planning a simple Earth-Earth-Venus mission in the Mission Architect for learning purposes and I'm having some issues in finding a solution with the optimizer. I think that the main problem are my constraints and my initial condition, so perhaps you guys could help me with those.
At the moment the mission architect looks like this:
My initial state is set to a SMA of 6574 and the rest of the parameters as zero. I have no idea to which value set the Epoch and I think that's what's causing the main issue. The bounds on the dV maneuvers are set to +/- 2km/s prograde, normal and +/- 50 m/s radial.
Thanks in advance!