An air vehicle and an air vehicle control system (100) include a computer-implemented controller. The controller is configured to control an air vehicle, where the air vehicle is logically divided into four sections of electrical and mechanical devices that are operatively connected to the controller via a control data bus and an actuation bus. The four sections include a forward sector (104), a left engine sector (108), a right engine sector (106), and an aft sector (105). The controller controls all four sections of electrical and mechanical devices of the air vehicle.
ELECTRIC VEHICLE MANAGEMENT ARCHITECTURE
ARCHITEKTUR FÜR DIE VERWALTUNG VON ELEKTROFAHRZEUGEN
ARCHITECTURE DE GESTION DE VÉHICULE ÉLECTRIQUE
2023-06-07
Patent
Electronic Resource
English
IPC: | H02J CIRCUIT ARRANGEMENTS OR SYSTEMS FOR SUPPLYING OR DISTRIBUTING ELECTRIC POWER , Schaltungsanordnungen oder Systeme für die Abgabe oder Verteilung elektrischer Leistung / B64C AEROPLANES , Flugzeuge / H04L TRANSMISSION OF DIGITAL INFORMATION, e.g. TELEGRAPHIC COMMUNICATION , Übertragung digitaler Information, z.B. Telegrafieverkehr |
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