Flugzeugleit- Und/oder Navigationssystem unter Verwendung Künstlicher Magnetischer Felder

Details

Veröffentlichungs-Nr.

EP4807480

Anmeldetag

11. März 2025

Veröffentlichung

16. September 2026

Rechtsraum

EP

IPC

G05D1/20

Abstract

The present disclosure relates to a method M, in an aircraft guidance and/or navigation system S, to guide an aircraft AC towards or from a landing site LS using measurements, onboard the aircraft, of one or more unique artificial magnetic fields MF1, MF2, MFN assigned to a vicinity V of the landing site. The present disclosure also relates to a magnetic ground infrastructure MGI in the aircraft guidance and/or navigation system S, to guide the aircraft AC towards or from the landing site LS, the magnetic ground infrastructure comprising one or more emitters E1, E2, EN assigned to the vicinity V of the landing site, each emitter being adapted to generate a respective unique artificial magnetic field MF1, MF2, MFN. The present disclosure also relates to the aircraft AC in the aircraft guidance and/or navigation system S, to guide the aircraft towards or from the landing site LS, the aircraft comprising one or more magnetometers MM1, MM2, MMN adapted to detect the one or more unique artificial magnetic fields MF1, MF2, MFN assigned to the vicinity V of the landing site; and a navigation system NS adapted to calculate a relative or an absolute position of the aircraft in relation to the landing site, based on detection result of the one or more magnetometers.

Anmelder

Firma

Airbus Defence and Space GmbH

Land

🇩🇪 Deutschland

Fachgebiete