Steuerung eines Flugzeugs zur Vermeidung von Geländehindernissen unter Verwendung von Modellen mit Geschlossenem Regelkreis von Reduzierter Ordnung

Details

Veröffentlichungs-Nr.

EP4242777

Aktenzeichen

EP23155060

Anmeldetag

6. Februar 2023

Veröffentlichung

25. Juni 2025

Erteilung

25. Juni 2025

Rechtsraum

EP

IPC

G08G5/21G08G5/53G08G5/74G08G5/80G05D105/22G01C21/20G05D1/622G05D109/20

Abstract

This disclosure relates to apparatuses, systems, and methods for controlling an aircraft. A computing system may identify a first command signal received via a flight control at a time point to control navigation of the aircraft through an environment. The computing system may attenuate the first command signal using a fade function over a time window relative to the time point to generate a second command signal. The computing system may input the second command signal to a model to generate predicted paths for the aircraft through the environment over the time window. The computing system may determine that at least one predicted path intersects with an obstacle in the environment during the time window. The computing system may generate a location to which to navigate the aircraft to avoid the obstacle. The computing system may perform an action to direct the aircraft to the location.

Anmelder

Firma

Lockheed Martin Corporation

Land

🇺🇸 USA

Fachgebiete