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Advanced fault diagnosis for safer flight guidance and control

PROJECTS
Funding
European
European Union
Duration
-
Status
Complete with results
Geo-spatial type
Other
Total project cost
€3 662 669
EU Contribution
€2 608 594
Project website
Project Acronym
ADDSAFE
STRIA Roadmaps
Vehicle design and manufacturing (VDM)
Transport mode
Airborne icon
Transport policies
Safety/Security
Transport sectors
Passenger transport

Overview

Call for proposal
FP7-AAT-2008-RTD-1
Link to CORDIS
Background & Policy context

Recent airliner accident and incident statistics show that about 16% of the accidents between 1993 and 2007 can be attributed to Loss of Control In-flight (LOC-I), caused by a piloting mistake, technical malfunctions or unusual upsets due to external disturbances. Loss of flight control remains the second largest accident category after Controlled Flight Into Terrain (CFIT) accounting for 23% of air accidents worldwide.

Loss of Control (LOC) is intrinsically related to the guidance and control (G&C) system of the aircraft, and includes sensors and actuators failures. The state-of-practice for aircraft manufacturers to diagnose these faults and obtain full flight envelope protection is to provide high levels of hardware redundancy in order to perform coherency tests and ensure sufficient available control action.

This hardware-redundancy based Fault Detection and Diagnosis (FDD) approach fits into current aircraft certification processes while ensuring the highest level of safety standards. On the other hand, FDD solutions increase the aircraft weight and complexity and thus its manufacturing and maintenance costs. The FDD approach is becoming increasingly problematic when used in conjunction with the many innovative technical solutions being developed by the aeronautical sector to satisfy the greener and safety imperatives demanded by society like: more affordable, safer, cleaner, quieter. This is increasingly creating a gap between the scientific methods advocated within the academic and research communities and the technological developments required by the aeronautics industry.

This applicability gap has resulted in a de facto "fault diagnosis bottleneck", a technological barrier constraining the full realization of the next generation of air transport due to the need to ensure the current highest levels of aircraft safety when implementing novel green and efficient technologies.

Objectives

ADDSAFE tries to overcome this technological gap by facing the following two challenges:

  • helping the scientific community to develop the best suited FDD (Fault Detection and Diagnosis) methods capable of handling the real-world challenges raised by industry; and
  • ensuring acceptance and widespread use of these advanced theoretical methods by the aircraft industry.

The overall aim of the project is to develop and apply model-based FDD methods for civil aircraft in order to increase aircraft safety and reduce development/maintenance costs.

From a technological and scientific perspective the main benefits of the project are:

  • identification of a set of guidelines for FDD design and analysis for aircraft G&C;
  • improved FDD methods and understanding of their applicability to aircraft FDD;
  • a step towards a V&V process for advanced aircraft diagnostic systems;
  • demonstration of the most promising model-based FDD designs on industrial state-of-art flight simulation platforms.

From the perspective of the benefits to society, ADDSAFE :

  • supports greener technical solutions;
  • maintains current highest safety standards;
  • improves aircraft transport cost & efficiency.
Methodology

ADDSAFE is divided in 6 work-packages (WP 0 up to WP 5) decomposed into a total of 14 sub-work packages (WP 0.1 up to WP 5.2). The project strives to combine the knowledge and to increase synergies between the scientific and the technological partners at all levels of the project development cycle. Thus, most of the tasks include participation by all partners.

Funding

Parent Programmes
Institution Type
Public institution
Institution Name
The European Commission
Type of funding
Public (EU)
Funding Source
DG RTD

Results

Definition of a set of guidelines for aircraft G&C model-based fault detection and diagnosis.

Improved FDD methods and understanding of their applicability to aircraft G&C.

A step towards a V&V process for advanced diagnostic systems.

Innovation aspects

The results will help achieve the European Vision 2020 challenges related to the “greening” of the aircraft, by supporting the application of already developed sustainable solutions, as well as to “safety”, by opening the door to develop new technologies to maintain the current highest aircraft safety levels regardless of the increase in air traffic.

Strategy targets

1. An efficient and integrated mobility system: 1.3 Secure Transport

Readiness

Further research is necessary

Partners

Lead Organisation
Organisation
Deimos Space S.l.
Address
Ronda de Poniente 19, Portal 2, 2a Planta, 28760 TRES CANTOS (MADRID), Spain
Organisation website
EU Contribution
€393 376
Partner Organisations
Organisation
Airbus Operations Sas
Address
ROUTE DE BAYONNE 316, 31060 TOULOUSE, France
Organisation website
EU Contribution
€240 126
Organisation
Deutsches Zentrum Fr Luft Und Raumfahrt E.v
Address
Linder Hoehe, 51147 KOELN, Germany
Organisation website
EU Contribution
€532 556
Organisation
Magyar Tudomanyos Akademia Szamitastechnikai Es Automatizalasi Kutatointezet
Address
Budapest, Kende Utca 13-17, 1111, Hungary
Organisation website
EU Contribution
€245 400
Organisation
University Of Greenwich
Address
University of Greenwich, Avery Hill Mansion Site, Bexley Road, LONDON, HU6 7RX, United Kingdom
Organisation website
EU Contribution
€327 269
Organisation
University Of Leicester
Address
University Road, Leicester, LE1 7RH, United Kingdom
EU Contribution
€313 846
Organisation
Centre National De La Recherche Scientifique
Address
3 rue Michel-Ange, 75794 PARIS, France
Organisation website
EU Contribution
€259 697
Organisation
Technische Universiteit Delft
Address
STEVINWEG 1, 2628 CN DELFT, Netherlands
Organisation website
EU Contribution
€296 324

Technologies

Technology Theme
Sensor technologies
Technology
Integrated sensors for structural components
Development phase
Research/Invention

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