Flugsteuergerät für ein Flugzeug sowie Flugzeug

Details

Veröffentlichungs-Nr.

EP3871984

Aktenzeichen

EP21153431

Anmeldetag

26. Januar 2021

Veröffentlichung

24. Juli 2024

Erteilung

24. Juli 2024

Rechtsraum

EP

IPC

B64D45/02

Abstract

An aircraft (1) includes a fuselage (10), a main wing (12), an electric field sensor (20), and a flight controller (26). The electric field sensor (20) is configured to detect surface electric field intensities at four or more of mutually different positions on the aircraft (1). The flight controller (26) includes a storage (50), a data extracting unit (52), an electric field intensity calculator (54), and an attitude control unit (60). The storage (50) holds an electric field distribution table. The data extracting unit (52) is configured to extract one of pieces of distribution data from the electric field distribution table. The electric field intensity calculator (54) is configured to calculate surface electric field intensities at respective positions on the basis of the extracted piece of the distribution data. The attitude control unit (60) is configured to perform prevention operation of the aircraft (1) on the basis of the calculated surface electric field intensities at the respective positions.

Anmelder

Firma

Subaru Corporation

Land

🇯🇵 Japan

Fachgebiete