Repository containing the files for the thesis : Optimization of an aircraft design problem for hybrid-electric configurations under manufacturing and certification constraints
This PR adds a way to compute the performance of an aircraft on an operational misssion. It reuses most of the component from the original mission excpet it uses a trick to rename all the variables so that they are defined somewhere else in the data structure. This theoretically mean we should be able to run both simultaneously. This also means the operational misssion has the same structure as the design one
This PR also adds a simplified models for the computation of environmental impact of the aircraft so that this score can appear as an optimization criteria
This PR adds a way to compute the performance of an aircraft on an operational misssion. It reuses most of the component from the original mission excpet it uses a trick to rename all the variables so that they are defined somewhere else in the data structure. This theoretically mean we should be able to run both simultaneously. This also means the operational misssion has the same structure as the design one
This PR also adds a simplified models for the computation of environmental impact of the aircraft so that this score can appear as an optimization criteria