FR3124257B1 - Procédé et système de test d’un calculateur avionique. - Google Patents

Procédé et système de test d’un calculateur avionique. Download PDF

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Publication number
FR3124257B1
FR3124257B1 FR2106634A FR2106634A FR3124257B1 FR 3124257 B1 FR3124257 B1 FR 3124257B1 FR 2106634 A FR2106634 A FR 2106634A FR 2106634 A FR2106634 A FR 2106634A FR 3124257 B1 FR3124257 B1 FR 3124257B1
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France
Prior art keywords
computer
avionics computer
software
internal parameters
test
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FR2106634A
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English (en)
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FR3124257A1 (fr
Inventor
Arnaud Chevalier
Hacen Abdeslem
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Airbus Operations SAS
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Airbus Operations SAS
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Priority to FR2106634A priority Critical patent/FR3124257B1/fr
Priority to US17/842,847 priority patent/US11994981B2/en
Publication of FR3124257A1 publication Critical patent/FR3124257A1/fr
Application granted granted Critical
Publication of FR3124257B1 publication Critical patent/FR3124257B1/fr
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    • GPHYSICS
    • G06COMPUTING; CALCULATING OR COUNTING
    • G06FELECTRIC DIGITAL DATA PROCESSING
    • G06F11/00Error detection; Error correction; Monitoring
    • G06F11/36Preventing errors by testing or debugging software
    • G06F11/3668Software testing
    • G06F11/3696Methods or tools to render software testable
    • GPHYSICS
    • G06COMPUTING; CALCULATING OR COUNTING
    • G06FELECTRIC DIGITAL DATA PROCESSING
    • G06F11/00Error detection; Error correction; Monitoring
    • G06F11/36Preventing errors by testing or debugging software
    • G06F11/3668Software testing
    • G06F11/3672Test management
    • G06F11/3688Test management for test execution, e.g. scheduling of test suites
    • GPHYSICS
    • G06COMPUTING; CALCULATING OR COUNTING
    • G06FELECTRIC DIGITAL DATA PROCESSING
    • G06F11/00Error detection; Error correction; Monitoring
    • G06F11/30Monitoring
    • G06F11/32Monitoring with visual or acoustical indication of the functioning of the machine
    • G06F11/323Visualisation of programs or trace data
    • GPHYSICS
    • G06COMPUTING; CALCULATING OR COUNTING
    • G06FELECTRIC DIGITAL DATA PROCESSING
    • G06F11/00Error detection; Error correction; Monitoring
    • G06F11/36Preventing errors by testing or debugging software
    • G06F11/3664Environments for testing or debugging software
    • GPHYSICS
    • G06COMPUTING; CALCULATING OR COUNTING
    • G06FELECTRIC DIGITAL DATA PROCESSING
    • G06F11/00Error detection; Error correction; Monitoring
    • G06F11/36Preventing errors by testing or debugging software
    • G06F11/3668Software testing
    • GPHYSICS
    • G06COMPUTING; CALCULATING OR COUNTING
    • G06FELECTRIC DIGITAL DATA PROCESSING
    • G06F11/00Error detection; Error correction; Monitoring
    • G06F11/36Preventing errors by testing or debugging software
    • G06F11/3668Software testing
    • G06F11/3672Test management
    • G06F11/3692Test management for test results analysis

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  • Engineering & Computer Science (AREA)
  • Theoretical Computer Science (AREA)
  • Quality & Reliability (AREA)
  • Physics & Mathematics (AREA)
  • General Engineering & Computer Science (AREA)
  • General Physics & Mathematics (AREA)
  • Computer Hardware Design (AREA)
  • Data Mining & Analysis (AREA)
  • Test And Diagnosis Of Digital Computers (AREA)

Abstract

Procédé et système de test d’un calculateur avionique. Le procédé de test d’un calculateur avionique (12) comprenant un ensemble de paramètres internes parmi lesquels seul un sous-ensemble de paramètres internes sont accessibles par un banc de test (20), comprend les étapes suivantes : - raccorder (E1) le calculateur avionique au banc de test ; - équiper (E2) le banc de test d’un calculateur de test (14) doté d’un logiciel (15) similaire au logiciel (13) du calculateur avionique (12), dont tous les paramètres internes sont accessibles par le banc de test ; - exécuter (E3) le logiciel du calculateur avionique en interaction avec le banc de test et exécuter (E4) le logiciel du calculateur de test simultanément au logiciel du calculateur avionique ; - visualiser (E5) des paramètres internes appartenant au sous-ensemble de paramètres internes du calculateur avionique et visualiser (E6) des paramètres internes du calculateur de test, correspondant à des paramètres internes du calculateur avionique n’appartenant pas au sous-ensemble de paramètres internes du calculateur avionique, de façon à vérifier la conformité du fonctionnement du logiciel (13). Figure pour l’abrégé : Fig. 1
FR2106634A 2021-06-22 2021-06-22 Procédé et système de test d’un calculateur avionique. Active FR3124257B1 (fr)

Priority Applications (2)

Application Number Priority Date Filing Date Title
FR2106634A FR3124257B1 (fr) 2021-06-22 2021-06-22 Procédé et système de test d’un calculateur avionique.
US17/842,847 US11994981B2 (en) 2021-06-22 2022-06-17 Method and system for testing an avionic computer

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR2106634 2021-06-22
FR2106634A FR3124257B1 (fr) 2021-06-22 2021-06-22 Procédé et système de test d’un calculateur avionique.

Publications (2)

Publication Number Publication Date
FR3124257A1 FR3124257A1 (fr) 2022-12-23
FR3124257B1 true FR3124257B1 (fr) 2023-05-12

Family

ID=77411845

Family Applications (1)

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FR2106634A Active FR3124257B1 (fr) 2021-06-22 2021-06-22 Procédé et système de test d’un calculateur avionique.

Country Status (2)

Country Link
US (1) US11994981B2 (fr)
FR (1) FR3124257B1 (fr)

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6502102B1 (en) * 2000-03-27 2002-12-31 Accenture Llp System, method and article of manufacture for a table-driven automated scripting architecture
FR2918759B1 (fr) * 2007-07-13 2009-09-18 Eurocopter France Procede de test d'un systeme electronique
EP2329376A1 (fr) * 2008-08-15 2011-06-08 Verum Holding B.V. Procédé et système destiné à tester un logiciel de commande de machine complexe
FR2950449A1 (fr) * 2009-09-23 2011-03-25 Eurocopter France Simulation en temps reel hautement representative d'un systeme avionique
FR3019920B1 (fr) * 2014-04-14 2017-10-06 Thales Sa Equipement de substitution d'un equipement avionique d'affichage; systeme et module associes
US9842045B2 (en) * 2016-02-19 2017-12-12 International Business Machines Corporation Failure recovery testing framework for microservice-based applications

Also Published As

Publication number Publication date
US20230008659A1 (en) 2023-01-12
FR3124257A1 (fr) 2022-12-23
US11994981B2 (en) 2024-05-28

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