Summary
This article proposes a component‐sizing problem for a hybrid unmanned aircraft alongside a coordinated energy consumption and flight scheduling. The goal is to simultaneously minimize the fuel consumption, the gaseous emission, and the overall costs of components (capital and operating costs) including fuel cell, battery, electric motor, and thermal engines. To this end, a non‐linear programming is proposed, and by an efficient decomposition method, it is solved under GAMS. The numerical results are compared with some evolutionary algorithms and showed that the proposed optimization framework exerts influence on the overall costs, energy efficiency, and computation time.