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Emergency propulsion-based autoland system

Fezans, Nicolas and Gamaleri, Maxence (2012) Emergency propulsion-based autoland system. ICAS 2012, 23.-28. Sep. 2012, Brisbane, Australia.

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Official URL: http://www.icas.org/ICAS_ARCHIVE/ICAS2012/ABSTRACTS/503.HTM

Abstract

In this paper, an emergency autoland system capable of landing automatically with the ATTAS research aircraft only using engine thrust variations is presented. This autoland is intentionally kept as simple as possible, but demonstrates good performance even in the presence of uncertainties and external disturbances. The performance in the presence of wind shears is shown in the paper. It is based on a previously published propulsion-based control law for the inner loops. Implementing this simple emergency autoland in modern aircraft is not challenging. Aircraft already in service could also be retrofitted.

Item URL in elib:https://elib.dlr.de/84416/
Document Type:Conference or Workshop Item (Speech)
Title:Emergency propulsion-based autoland system
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Fezans, Nicolasnicolas.fezans (at) dlr.dehttps://orcid.org/0000-0003-4351-3474
Gamaleri, MaxenceUNSPECIFIEDUNSPECIFIED
Date:September 2012
Refereed publication:Yes
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Status:Published
Keywords:Propulsion-controlled aircraft, autoland, emergency system, fault-tolerant control, ATTAS
Event Title:ICAS 2012
Event Location:Brisbane, Australia
Event Type:international Conference
Event Dates:23.-28. Sep. 2012
Organizer:International Council of Aeronautical Sciences
HGF - Research field:Aeronautics, Space and Transport
HGF - Program:other
HGF - Program Themes:other
DLR - Research area:Aeronautics
DLR - Program:L - no assignment
DLR - Research theme (Project):L - no assignment (old)
Location: Braunschweig
Institutes and Institutions:Institute of Flight Systems > Flight Dynamics and Simulation
Deposited By: Fezans, Nicolas
Deposited On:25 Sep 2013 14:13
Last Modified:23 Mar 2017 14:02

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