Flugzeugüberwachungs- und -Steuerungssystem und -Verfahren

Details

Veröffentlichungs-Nr.

EP4796439

Anmeldetag

26. Januar 2026

Veröffentlichung

26. August 2026

Rechtsraum

EP

IPC

B64C27/00, B06B1/16, B64D45/00

Abstract

An aircraft monitoring and control system includes a plurality of actuator controllers and a plurality of accelerometer. Each actuator controller is configured to receive actuator position control commands from at least one flight control computer and to supply accelerometer data it receives to the at least one flight control computer. Each actuator controller is further configured, in response to the actuator position control commands, to generate and supply actuator commands. Each accelerometer is associated with a different one of the actuator controllers. Each accelerometer is configured to sense vibrations and supply the accelerometer data, indicative of the sensed vibrations, to its associated actuator controller.

Anmelder

Firma

Honeywell International Inc.

Land

🇺🇸 USA

Fachgebiete