Repository containing the files for the thesis : Optimization of an aircraft design problem for hybrid-electric configurations under manufacturing and certification constraints
Spent a great deal of time developing the Pipistrel as a reference aircraft for this code, and it's close enough to the results available online (a great deal of info on the electric power train inside the AFM of the SW128). Also includes:
It is now possible to directly connect a battery to a bus or sspc (not limited to dc/dc converter anymore)
It is now possible to recalibrate PMSM efficiency
Precondition current voltage and power of the battery is now available
Spent a great deal of time developing the Pipistrel as a reference aircraft for this code, and it's close enough to the results available online (a great deal of info on the electric power train inside the AFM of the SW128). Also includes: