Mehrzielige Steurung mit einer Allokierungssteurung

Details

Veröffentlichungs-Nr.

EP3243748

Aktenzeichen

EP17158968

Anmeldetag

2. März 2017

Veröffentlichung

1. Januar 2020

Erteilung

1. Januar 2020

Rechtsraum

EP

IPC

B64C27/80B64C27/10B64C27/00// B64C27/46

Abstract

A flight system (300) for an aircraft (10) and method for controlling a clearance between a first rotor disk (28) and a second rotor disk (32) of an aircraft is disclosed. The flight system (300) includes a sensor for measuring an angle of deviation (320a, 320b) of at least one of a first rotor disk (28) and a second rotor disk (32) of the aircraft to indicate a clearance between the first rotor disk (28) and the second rotor disk (32) as well as sensors (320c, 320d) for measuring a flight condition of the aircraft (10). A control allocation module (306) uses the measured angle of deviation (320a, 320b) and the flight condition of the aircraft to determine an allocation of control settings to axis-controlling devices of the aircraft to attain a selected pitch of the aircraft (10), wherein the allocation is based at least on the measured angle of deviation (320a, 320b) and the flight state of the aircraft.

Anmelder

Firma

Sikorsky Aircraft Corporation

Land

🇺🇸 USA

Fachgebiete