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Grant: Collaborative Research and Development Grants

Concordia University

$59,500.00

Methodologies and tools for virtual design and testing of advanced flight control systems_x000d_ _x000d_ _x000d_

FY 2020-21

Summary
With the technology of fly-by-wire (FBW) flight controls now well established in the sector of transport aircraft, the next logical evolution is to introduce more multi-functionality in the flight control system. For instance on the CSeries, the first FBW aircraft developed by Bombardier, the ailerons are drooped symmetrically a few degrees down in the take-off configuration to optimize the lift distribution for climb performance. The multi-functional use of flight controls has significant potential of increasing the fuel efficiency of future aircraft and thus contribute to reducing the environmental footprint of aviation. However, such advanced flight control systems feature significantly higher complexity than current systems and are also opening a very large design space of potential architecture options. New methodologies and tools therefore need to be researched to increase the efficiency and effectiveness of the development process for such advanced flight control systems. The presented project with Bombardier will research such new methodologies and tools and will contribute to bringing novel flight control system architectures to fruition in the next generation of aircraft in Canada, by advancing the state-of the art of virtual design and virtual testing in three areas: (1) model-based systems engineering (MBSE), (2) model-based safety assessment (MBSA) and (3) model-based design (MBD). These new methodologies will lead to the development of leading edge flight control systems, reducing the environmental footprint of Canadian designed aircraft and increasing the cost effectiveness of Bombardier's development process to ensure sustained international competitiveness.
Program
Collaborative Research and Development Grants
Location
Quebec, Canada
Recipient Type
Academia
Type
Grant
Source
NSERC's Awards Data

As published

Application id
542298-2019
Name nom
Liscouet-Hanke, Susan
Department département
Mechanical, Industrial and Aerospace Engineering (MIAE)
Organization id
70
Institution établissement
Concordia University
Province en
Québec
Province fr
Québec
Country en
CANADA
Country fr
CANADA
Fiscal year exercice financier
2020
Competition year année de concours
2019
Award amount
59500
Program id
CRDPJ
Program name en
Collaborative Research and Development Grants
Program name fr
Subventions de recherche et développement coopérative
Group en
Research partnerships programs
Group fr
Programmes de partenariat
Committee code
96
Committee name en
RPP Internal Decision Cttee
Committee name fr
Cté de décision interne - PPR
Area of application code
703
Area of application group en
Transportation systems and services
Area of application group fr
Services et systèmes de transport
Area of application en
Aerospace
Area of application fr
Aérospatial
Research subject code
2108
Research subject group en
Mechanical engineering
Research subject group fr
Génie mécanique
Research subject en
Aerospace, aeronautical and automotive engineering
Research subject fr
Génie aérospatial, aéronautique et automobile
Installment
inst:2 - 2
Partie
1
Nb partie
2
Application title
Methodologies and tools for virtual design and testing of advanced flight control systems_x000d_ _x000d_ _x000d_
Keyword
NSERC
Application summary
With the technology of fly-by-wire (FBW) flight controls now well established in the sector of transport aircraft, the next logical evolution is to introduce more multi-functionality in the flight control system. For instance on the CSeries, the first FBW aircraft developed by Bombardier, the ailerons are drooped symmetrically a few degrees down in the take-off configuration to optimize the lift distribution for climb performance. The multi-functional use of flight controls has significant potential of increasing the fuel efficiency of future aircraft and thus contribute to reducing the environmental footprint of aviation. However, such advanced flight control systems feature significantly higher complexity than current systems and are also opening a very large design space of potential architecture options. New methodologies and tools therefore need to be researched to increase the efficiency and effectiveness of the development process for such advanced flight control systems. The presented project with Bombardier will research such new methodologies and tools and will contribute to bringing novel flight control system architectures to fruition in the next generation of aircraft in Canada, by advancing the state-of the art of virtual design and virtual testing in three areas: (1) model-based systems engineering (MBSE), (2) model-based safety assessment (MBSA) and (3) model-based design (MBD). These new methodologies will lead to the development of leading edge flight control systems, reducing the environmental footprint of Canadian designed aircraft and increasing the cost effectiveness of Bombardier's development process to ensure sustained international competitiveness.