Hello Emilio,
Thank you for your response and for what you guys are doing!
I have managed to run it without any further errors for a time now, but now it seems that is not converging in any of the mission segments. I am using a constant climb rate-constant speed segment to avoid throttle issues, but I still think that the problem lies somewhere in the prop-battery-motor area. Since I am using already real data, I would like to know more about the propeller inputs and mostly the "design" ones, because I probably feed the program with the wrong ones:
Specifically, design altitude, thrust, power, Cl, and RPM from the propeller, and the expected current from the motor.
I would like to know which design point do you specifically refer to! Should it be the max? Should it be for the cruise condition?
Also, would you recommend updating the package to the programmer version in order to follow the changes that you are constantly doing in the code?
Thanks a lot in advance!
Dimitris