An aircraft hybrid electrical propulsion (HEP) propulsion and attitude control system (100) includes a propulsion system (104), electrical system and HEP controller (108). The propulsion system (104) includes at least one propulsor (122) and at least one electric motor (126) configured to drive the at least one propulsor (122) 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 (126) and a second amount of power to a plurality of electrical loads. The HEP controller (108) 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.


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    Title :

    AIRCRAFT HYBRID ELECTRIC PROPULSION AND ATTITUDE CONTROLLER


    Additional title:

    HYBRIDER ELEKTRISCHER FLUGZEUGANTRIEB UND LAGESTEUERUNG
    DISPOSITIF DE COMMANDE DE PROPULSION ÉLECTRIQUE HYBRIDE D'AÉRONEF ET D'ATTITUDE


    Contributors:
    JOSHI NINAD (author) / BAIG ZUBAIR A (author) / AMARI MARTIN (author)

    Publication date :

    2025-04-16


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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