Systeme und Verfahren zur Gesteuerten Filtrierung einer Flugzeugsteuerungseingabe

Details

Veröffentlichungs-Nr.

EP3572900

Aktenzeichen

EP19174912

Anmeldetag

16. Mai 2019

Veröffentlichung

19. August 2020

Erteilung

19. August 2020

Rechtsraum

EP

IPC

G05D1/08

Abstract

In one embodiment, a method is performed by a control computer (380). The method includes receiving a time series of control inputs in relation to a control axis of an aircraft (100), where the control computer (380) causes actuation in response to each control input (302,304,306) in the time series as the control input (302,304,306) is received. The method also includes determining aircraft oscillation over a sample period corresponding to the time series. The method also includes evaluating information related to the determined aircraft oscillation using engagement settings associated with a control filter (314). The method also includes engaging the control filter (314) responsive to the information satisfying the engagement settings, where the engaged control filter (314) systematically attenuates future control inputs (302,304,306) in relation to the control axis prior to actuation responsive thereto.

Anmelder

Firma

Bell Helicopter Textron Inc.

Land

🇺🇸 USA

Fachgebiete