DLR-Logo -> http://www.dlr.de
DLR Portal Home | Imprint | Privacy Policy | Contact | Deutsch
Fontsize: [-] Text [+]

Design and Piloted Simulator Evaluation of Adaptive Safe Flight Envelope Protection Algorithm

Lombaerts, Thomas and Looye, Gertjan and Ellerbroek, Joost and Rodriguez y Martin, Mitchell (2017) Design and Piloted Simulator Evaluation of Adaptive Safe Flight Envelope Protection Algorithm. Journal of Guidance, Control, and Dynamics, 40 (8), pp. 1902-1924. American Institute of Aeronautics and Astronautics (AIAA). doi: 10.2514/1.G002525. ISSN 0731-5090.

Full text not available from this repository.

Official URL: https://arc.aiaa.org/doi/abs/10.2514/1.G002525


This paper discusses the design and evaluation of an efficient safe flight envelope protection method for keeping an augmented aircraft with manual flight control laws within the safe envelope bounds. This flight envelope is estimated adaptively, so that configuration changes and possible failures can be taken into account. The updated information of the safe envelope is used in the flight control laws to prevent loss of control in flight. It has been found that a control architecture involving separate pilot command filtering is particularly well suited to incorporate these adaptive protections. Moreover, haptic feedback to the pilot controls can be included as well, based on the same adaptive bounds. This has the potential to further increase the flight crew awareness about the risk of losing control in flight. These algorithms have been evaluated in the Simulation, Motion, and Navigation Research Simulator at Delft University of Technology to investigate the impact on the awareness of the crew. Commercial airline crews flew multiple challenging approach and landing scenarios in a relevant simulated environment. Results show that the algorithms support the flight crew significantly. They contribute to “care-free” flying and to avoiding loss of control in flight.

Item URL in elib:https://elib.dlr.de/118423/
Document Type:Article
Title:Design and Piloted Simulator Evaluation of Adaptive Safe Flight Envelope Protection Algorithm
AuthorsInstitution or Email of AuthorsAuthor's ORCID iD
Looye, GertjanGertjan.Looye (at) dlr.deUNSPECIFIED
Ellerbroek, JoostTU DelftUNSPECIFIED
Rodriguez y Martin, MitchellTU DelftUNSPECIFIED
Date:August 2017
Journal or Publication Title:Journal of Guidance, Control, and Dynamics
Refereed publication:Yes
Open Access:No
Gold Open Access:No
In ISI Web of Science:Yes
DOI :10.2514/1.G002525
Page Range:pp. 1902-1924
Publisher:American Institute of Aeronautics and Astronautics (AIAA)
Keywords:flight control, adaptive control, envelope protection, flight simulator, icing
HGF - Research field:Aeronautics, Space and Transport
HGF - Program:Aeronautics
HGF - Program Themes:fixed-wing aircraft
DLR - Research area:Aeronautics
DLR - Program:L AR - Aircraft Research
DLR - Research theme (Project):L - Systems and Cabin (old)
Location: Oberpfaffenhofen
Institutes and Institutions:Institute of System Dynamics and Control > Aircraft System Dynamics
Deposited By: Looye, Dr. Gertjan
Deposited On:23 Jan 2018 13:33
Last Modified:20 Jun 2021 15:50

Repository Staff Only: item control page

Help & Contact
electronic library is running on EPrints 3.3.12
Copyright © 2008-2017 German Aerospace Center (DLR). All rights reserved.