Optimal energy management for hybrid electric aircraft
A convex formulation is proposed for optimal energy management in aircraft with hybrid propulsion systems consisting of gas turbine and electric motor components. By combining a point-mass aircraft dynamical model with models of electrical and mechanical powertrain losses, the fuel consumed over a p...
| المؤلفون الرئيسيون: | , , |
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| التنسيق: | Conference item |
| اللغة: | English |
| منشور في: |
Elsevier
2021
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