A dynamic model of a Hybrid Electric Propulsive System for degradation assessment

Abstract The present study proposes a model for the simulation of steady-state and transient behaviors Hybrid Electric Propulsive System (HEPS), in presence several forms degrees performance degradation. power system, which is made turboshaft engine coupled with an electric source intended urban air mobility applications. proposed encompasses capability modeling battery aging effects, and, consequently, updating system life. Moreover, versatility makes it suitable analysis dynamic behavior example small perturbations around predefined operational settings or following known mission profile. In this investigation applied to test HEPS under different operating conditions degradation criteria, affecting both thermal drive levels severity. application allowed generation relevant information concerning propulsive state health will be processed employment machine learning algorithms accompanying paper.