33th Congress of the International Council of the Aeronautical Sciences

02 - Systems Engineering and Integration

HYBRID ELECTRIC PROPULSION SYSTEM OPTIMIZATION FOR A COMMUTER AIRCRAFT

P. Krus¹, I. Staack¹, A.A.M. Oliveira, Federal University of Santa Catharina, Brazil; ¹Linköping University, Sweden

In this paper it is shown how simulation based optimization can be used to investigate the impact of development of different technologies on the feasibility of electrical aircraft. This work investigates the design of an electric/hydrogen-powered commuter aircraft (certified according to CS/FAR 23). Based on a dynamic holistic cyber-physical system model with a 6DOF flight dynamics model for mission simulation


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