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}},
}

Categories:

Tags:

Comments are closed