by Lonbani, Mohammadali Aghakhani, Morandini, Marco, Astori, Paolo and Ghiringhelli, Gianluca
Abstract:
A multiphase approach is considered for the design of an aircraft anti-skid braking control system. A four-phase scheme, based on angular acceleration thresholds and estimated slip rate values, is used to stabilize the aircraft system around an optimal braking condition. The change in vertical load due to variable lift force and the ensuing variable tire deflection are considered in the verification models. A hybrid controller is proposed, designed to achieve a stable wheel slip limit cycle. The simulations confirm that the proposed control scheme is a valid solution for the anti-skid of an aircraft main Landing Gear (LG). The actuator time delay and dynamic bandwidth influence on the aircraft stop distance has been studied.
Reference:
Anti-Skid Braking Control System Design for Aircraft: Multi-phase Schemes Approach (Lonbani, Mohammadali Aghakhani, Morandini, Marco, Astori, Paolo and Ghiringhelli, Gianluca), In 2017 5TH IEEE INTERNATIONAL CONFERENCE ON MODELS AND TECHNOLOGIES FOR INTELLIGENT TRANSPORTATION SYSTEMS (MT-ITS), IEEE, 2017.
Bibtex Entry:
@inproceedings{ ISI:000426813700018, Author = {Lonbani, Mohammadali Aghakhani and Morandini, Marco and Astori, Paolo and Ghiringhelli, Gianluca}, Book-Group-Author = {{IEEE}}, Title = {{Anti-Skid Braking Control System Design for Aircraft: Multi-phase Schemes Approach}}, Booktitle = {{2017 5TH IEEE INTERNATIONAL CONFERENCE ON MODELS AND TECHNOLOGIES FOR INTELLIGENT TRANSPORTATION SYSTEMS (MT-ITS)}}, Year = {{2017}}, Pages = {{104-109}}, Note = {{5th IEEE International Conference on Models and Technologies for Intelligent Transportation Systems (MT-ITS), napoli, ITALY, JUN 26-28, 2017}}, Organization = {{ASPISEK; PTV GRP Mind Movement; UirNet; Transport Simulation Systems; RETE Ferroviaria Italiana; Porto Napoli; Ministerio Infrastrutture dei Transporti; STAR SOSTENGO TERRITORALE ATTMTD RICERCA}}, Abstract = {{A multiphase approach is considered for the design of an aircraft anti-skid braking control system. A four-phase scheme, based on angular acceleration thresholds and estimated slip rate values, is used to stabilize the aircraft system around an optimal braking condition. The change in vertical load due to variable lift force and the ensuing variable tire deflection are considered in the verification models. A hybrid controller is proposed, designed to achieve a stable wheel slip limit cycle. The simulations confirm that the proposed control scheme is a valid solution for the anti-skid of an aircraft main Landing Gear (LG). The actuator time delay and dynamic bandwidth influence on the aircraft stop distance has been studied.}}, Publisher = {{IEEE}}, Address = {{345 E 47TH ST, NEW YORK, NY 10017 USA}}, Type = {{Proceedings Paper}}, Language = {{English}}, Affiliation = {{Lonbani, MA (Corresponding Author), Politecn Milan, Aerosp Sci & Technol Dept, Via La Masa 34, I-20156 Milan, Italy. Lonbani, Mohammadali Aghakhani; Morandini, Marco; Astori, Paolo; Ghiringhelli, Gianluca, Politecn Milan, Aerosp Sci & Technol Dept, Via La Masa 34, I-20156 Milan, Italy.}}, ISBN = {{978-1-5090-6484-7}}, Research-Areas = {{Computer Science; Transportation}}, Web-of-Science-Categories = {{Computer Science, Artificial Intelligence; Computer Science, Information Systems; Transportation Science & Technology}}, Author-Email = {{mohammadali.aghakhani@polimi.it marco.morandini@polimi.it paolo.astori@polimi.it gianluca.ghiringhelli@polimi.it}}, ResearcherID-Numbers = {{Morandini, Marco/E-5117-2012 Ghiringhelli, Gian Luca/E-5797-2012 Astori, Paolo/C-5652-2013}}, ORCID-Numbers = {{Morandini, Marco/0000-0002-1992-9077 Ghiringhelli, Gian Luca/0000-0003-3474-9258 Astori, Paolo/0000-0001-8285-3127}}, Funding-Acknowledgement = {{``TIVANO- Tecnologie Innovative per Velivoli di Aviazione generale di Nuova generaziOne{''} project {[}CTN01_00236_256622]}}, Funding-Text = {{This research was supported by the ``TIVANO- Tecnologie Innovative per Velivoli di Aviazione generale di Nuova generaziOne{''} project, CTN01_00236_256622.}}, Number-of-Cited-References = {{16}}, Times-Cited = {{0}}, Usage-Count-Last-180-days = {{0}}, Usage-Count-Since-2013 = {{5}}, Doc-Delivery-Number = {{BJ6LO}}, Unique-ID = {{ISI:000426813700018}}, DA = {{2020-12-22}}, }
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