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Airbus Flight Control Systems and future evolutions
Journée Nationale de réflexion et prospective sur les systèmes embarqués Presented by Jean-Philippe BEAUJARD Fight Control System Team Leader on A400M program Airbus Flight Control Systems and future evolutions c AIRBUS FRANCE All rights reserved
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AIRBUS FLIGHT CONTROL SYSTEMS
Contents Evolution of Airbus Flight Controls A view of the future system architecture avionics specifications software c AIRBUS FRANCE All rights reserved 17 JUIN 2003
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Evolution of Airbus Flight Controls
In the Early Days ... FARMAN F60 GOLIATH 1st flight 1919 c AIRBUS FRANCE All rights reserved 17 JUIN 2003
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Evolution of Airbus Flight Controls
Mechanical Flight Controls ARMAGNAC 1st flight 1949 c AIRBUS FRANCE All rights reserved 17 JUIN 2003
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CARAVELLE 1st flight May 1955
Evolution of Airbus Flight Controls 1st Hydro-mechanical servo controls CARAVELLE 1st flight May 1955 Hy c AIRBUS FRANCE All rights reserved 17 JUIN 2003
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Evolution of Airbus Flight Controls
Bloc diagrams Written by ELLIOTT AVIONICS (equipment supplier) and Sud Aviation (automatic pilot and manual flight controls) 1st Electrical Flight Controls CONCORDE 1st flight 1969 Hy Analogic computers Analogic computers c AIRBUS FRANCE All rights reserved 17 JUIN 2003
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Written by AIRBUS (aircraft manufacturer)
Evolution of Airbus Flight Controls Written by AIRBUS (aircraft manufacturer) formal specs (automatic pilot and manual flight controls) 2nd generation of Electrical Flight Controls March 1984 S.A.O. Hy HY3 HY1 A st flight Feb 1987 Digital computers c AIRBUS FRANCE All rights reserved 17 JUIN 2003
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Flare Law S.A.O. Evolution of Airbus Flight Controls SINCE EARLY 80 ’s
c AIRBUS FRANCE All rights reserved 17 JUIN 2003
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Evolution of Airbus Flight Controls
Written by AIRBUS (aircraft manufacturer) formal specs Full Electrical Flight Controls 1997 Hy Hy SCADE S.A.O. HY3 HY1 Digital computers A st flight Apr 2001 c AIRBUS FRANCE All rights reserved 17 JUIN 2003
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Evolution of Airbus Flight Controls
Written by AIRBUS (aircraft manufacturer) formal specs A380 “SPACE SHIP” 2001 Hy SCADE Hy Digital computers HY1 c AIRBUS FRANCE All rights reserved 17 JUIN 2003
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Written by ELLIOTT AVIONICS
These bloc diagrams were the genetical origin of SAO/SCADE Flare Law dated 1972 Written by ELLIOTT AVIONICS (equipment supplier) c AIRBUS FRANCE All rights reserved 17 JUIN 2003
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Evolution of Airbus Flight Controls
1st Airbus aircraft May 1969 Written by SFENA (equipment supplier) Bloc diagrams (automatic pilot) HY3 HY2 HY1 Hy A300 B1 1st flight Oct 1972 Analogic computers c AIRBUS FRANCE All rights reserved 17 JUIN 2003
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Evolution of Airbus Flight Controls
1st Embedded Software 1982 Written by AEROSPATIALE (aircraft manufacturer) Bloc diagrams (automatic pilot) Hy HY3 HY2 HY1 A st flight 1984 First Digital computers c AIRBUS FRANCE All rights reserved 17 JUIN 2003
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(aircraft manufacturer)
Flare Law dated 1984 Written by AIRBUS (aircraft manufacturer) c AIRBUS FRANCE All rights reserved 17 JUIN 2003
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Reduce weight again and again
A view of the future Reduce weight again and again Electronic Volumes COMPLEXITY smart actuator smart side-stick HY1 active control laws c AIRBUS FRANCE All rights reserved 17 JUIN 2003
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Blue input is used in laws every d +j1 seconds (j1 is variable)
A view of the future Minimize interfaces d Blue input is used in laws every d +j1 seconds (j1 is variable) multiplexed buses minimize input-output jitters minimize delays c AIRBUS FRANCE All rights reserved 17 JUIN 2003
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Move from specification reviews to analysis
A view of the future Move from specification reviews to analysis MATHEMATICAL PROOF CAN BE REPEATED AND CHECKED BY OTHERS A380 FLARE LAW FCTL SPECIFICATION 3000 SCADE sheets Prooved component Prooved Flare law component uses a set of prooved components Prooved Flare law component 17 c AIRBUS FRANCE All rights reserved 17 JUIN 2003
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AUTOMATIC CODE GENERATOR
A view of the future Get your software in the box within a day AUTOMATIC CODE GENERATOR NODES QUALIFIED CODE c AIRBUS FRANCE All rights reserved 17 JUIN 2003
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A view of the future Theory
We need a theory to support the design of complex systems mixing sampled booleans, integers and real values, So, our designs can integrate structures that are easier to analyse automatically, And use structures that ease determinism. Keep your complex system safe and simple. c AIRBUS FRANCE All rights reserved 17 JUIN 2003
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Ce document et son contenu sont la propriété d’AIRBUS FRANCE S. A. S
Ce document et son contenu sont la propriété d’AIRBUS FRANCE S.A.S. Aucun droit de propriété intellectuelle n’est accordé par la communication du présent document ou son contenu. Ce document ne doit pas être reproduit ou communiqué à un tiers sans l’autorisation expresse et écrite d’AIRBUS FRANCE S.A.S. Ce document et son contenu ne doivent pas être utilisés à d’autres fins que celles qui sont autorisées. Les déclarations faites dans ce document ne constituent pas une offre commerciale. Elles sont basées sur les postulats indiqués et sont exprimées de bonne foi. Si les motifs de ces déclarations n’étaient pas démontrés, AIRBUS FRANCE S.A.S serait prêt à en expliquer les fondements. c AIRBUS FRANCE All rights reserved 17 JUIN 2003
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