An aircraft hybrid electrical propulsion (HEP) propulsion and attitude control system includes a propulsion system, electrical system and HEP controller. The propulsion system includes at least one propulsor and at least one electric motor configured to drive the at least one propulsor to generate to generate one or both of thrust and lift. The electrical system delivers a first amount of power to the at least one electric motor and a second amount of power to a plurality of electrical loads. The HEP controller determines at least one attitude goal of the aircraft, and controls the electrical system to adjust at least one of the thrust or lift to achieve the at least one attitude goal.
AIRCRAFT HYBRID ELECTRIC PROPULSION AND ATTITUDE CONTROLLER
2024-12-26
Patent
Electronic Resource
English
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |
AIRCRAFT HYBRID ELECTRIC PROPULSION AND ATTITUDE CONTROLLER
European Patent Office | 2025
|Hybrid-Electric Propulsion for Aircraft
Online Contents | 2015
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