OPTIMIZING AIRCRAFT CONTROL BASED ON NOISE ABATEMENT VOLUMES

An aircraft control system 100 and method to optimize aircraft control based on noise abatement volumes. A noise abatement component 114 computes optimal flight and engine control based on a line-of-sight distance to minimize direct operating cost (DOC) while complying with community noise regulatio...

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Bibliographic Details
Main Authors DARNELL, Mark Lawrence, LAX, David Michael, RHONE, Brandon James
Format Patent
LanguageEnglish
French
German
Published 13.10.2021
Subjects
AEROPLANES
AIRCRAFT
ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT
AVIATION
CONTROLLING
COSMONAUTICS
EQUIPMENT FOR FITTING IN OR TO AIRCRAFT
FLYING SUITS
HELICOPTERS
PARACHUTES
PERFORMING OPERATIONS
PHYSICS
REGULATING
SIGNALLING
SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
TRAFFIC CONTROL SYSTEMS
TRANSPORTING
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Summary:An aircraft control system 100 and method to optimize aircraft control based on noise abatement volumes. A noise abatement component 114 computes optimal flight and engine control based on a line-of-sight distance to minimize direct operating cost (DOC) while complying with community noise regulations.
Bibliography:Application Number: EP20180176117