Multi-Objective Optimization of Hybrid Energy System of Solar Rechargeable Aircraft

Abstract

This article aims on the development of structural models of structural elements of the UAVs that incorporates solar energy system with the usage of hybrid energy systems using the multi-objective optimization approach. Proposed models taking into account the parameters of the optimization procedure. Simulation environment is built to check the behavior of a given UAV structure obtained during multi-objective optimization stage for objectives validation. Results of the article are obtained by using the proposed UAV design procedure with a verification based on the Simulink environment.