ETTC'2003 - SEE

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PARAMETER DESCRIPTION This array describes in detail parameter types and the structure associated. Parameter type ID DELAY DATA PARAMETER commentary Analog parameter Optional Optional 1 word The more often the delay and ID are not used. In this case, the arrangement of parameters is ARINC 429 Bus standard parameter ARINC 429 Bus FIFO parameter ARINC standard parameter PROCESSING mode ARINC message parameter PROCESSING mode RS232/422/485 bus PROCESSING mode RS message parameter PROCESSING mode Mandatory Mandatory 2 words Mandatory Mandatory 2 words static Mandatory Mandatory 1 up to 8 words The number of data words depends of the processing application Mandatory Optional The number of data words is dynamic. In this case the length field shall be used. Mandatory Optional 1 up to 8 words The delay is included in one of data words. Mandatory Optional The number of data words is dynamic. In this case the length field shall be used. CAN parameter Mandatory Mandatory 6 words Frequency Count Period parameter Mandatory Mandatory 2 words DISCRETE parameter Mandatory Mandatory AFDX parameter Queuing mode AFDX parameter Sampling mode (single or multi PAYLOAD) AFDX parameter Not acquired data Mandatory Optional Mandatory Optional 1 Word STATUS 4 bits STATUS 8 bits LABEL 8 bits AFDX Payload Left justified AFDX Payload Left justified ARINC DATA 24 bits ARINC DATA 24 bits 12 bits ( 12 Discretes ) right justified PADDING byte PADDING byte Mandatory Optional Statistic & network quality information’s The acquisition time of a given frame shall be written in the IENA header field. The acquisition time of a given frame shall be written in the IENA header field. 6
Conclusion : The ‘IENA Packets’ is the standard AIRBUS for flight and ground test installations. This data format answers to the new request of asynchronous time tagged data produced by the test equipments. The characteristics of ‘IENA Packets’ optimize the tests means and the tools decoding for analysis. . 7
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SÉANCE D'OUVERTURE / OPENING SESSI
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A l’aube de ce siècle, Airbus s
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Etape 4 : L’avion réel une fois
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C’est, sur l’exemple des essais
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parfois même sous la forme de plat
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oth the system and the manufacturin
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Such an interdependence between tes
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eference books, but it is as fundam
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BACK MANAGEMENT DES ESSAIS SYSTEME
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BACK ESSAIS D’ENSEMBLE LANCEURS C
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Elle ne doit cependant pas être me
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- le plan de mesures est conséquen
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4.2 MAQUETTE DYNAMIQUE ARIANE 5 Dan
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Les points délicats liés à l’o
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Processus Commande Architecture Int
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BACK 1 Introduction AIRBUS AIRCRAFT
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So, different test tools shall be d
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3.4 Architecture of A380 Simulators
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3.6 A380: Models In order to suppor
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GENERAL PRESENTATION OF JUZZLE GENE
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Figure 3 : Graphic User Interface o
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IMPLEMENTATION AND SIMULATION OF A
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REFERENCES [1] Space engineering, R
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Client Compliance Matrix (par rappo
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SESSION 2 : TECHNIQUES ET MOYENS D'
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POSTE INE A380 Les besoins fonction
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Les principes de l’architecture :
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Les éléments de l’architecture
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BACK Trajectographie temps réel DG
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Deux précisions temps réel sont p
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4.00 3.00 2.00 1.00 0.00 -1.00 -2.0
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CONCLUSION La phase d'essais en vol
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RÉSUMÉ: Osiris est une gamme de m
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1. INTRODUCTION Dassault Aviation e
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Exemple de modules banc d'intégrat
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éduction de durée des essais par
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5. EXEMPLE L'OSIRIS MULTIFONCTION U
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6. LA MODULARITÉ DE LA GAMME OSIRI
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• JBUILDER • ORACLE Cette modul
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• VX Wxorks reste l'OS de la part
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6.5 Exemple d'interconnexion avec d
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PRINCIPE 7.3 Exemple de réalisatio
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8. LA NOUVELLE GAMME SUR PC: VÉNUS
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• Un IHM de sélection des param
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9. CONCLUSION OSIRIS a maintenant g
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TABLE DES MATIERES 1. LE DATA-LINK
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AVIONS appartenant au réseau 25_P_
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• Les données à émettre sur le
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• 25_P_2/04 PCM émis par l'avion
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3.2 Le temps différé • En temps
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4. CONCLUSION • Toutes les IHM in
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INTRODUCTION Pour définir des proc
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- Ecarts de position en temps réel
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ANNEXE 1 CONSTITUTION CONSTITUTION
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They however incorporate some eleme
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As technology evolves, the boundary
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shown below together with the AGE c
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BACK ESSAIS SYSTEME SUR LES PROJETS
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3 qui contient le logiciel de vol.
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5 • essais en station « in vivo
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Avis, options et recommandations (5
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BACK Automatic Validation of Flight
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− The second level provides all d
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The operational flexibility of SINU
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• Test duration is reduced : for
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mimics from CCS ones. The objective
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1. Introduction ...................
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2. Présentation Le segment sol Ste
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AUS Station STA TM/TC Station STS T
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• La Commission de Revue d’Essa
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Certains essais particuliers liés
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Id Nom flux EXP37 Plan de vol Annex
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TTC’2003 Stentor 10/06/2003 QUALI
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TTC’2003 Le Programme Stentor 10/
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TTC’2003 Satellite GEO TM/TC/Rang
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TTC’2003 •Equipes CNES : Qualif
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TTC’2003 •L’organisation mise
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TTC’2003 Interfaces Externes :
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TTC’2003 Les Contraintes de Déve
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TTC’2003 Contient ontient la la m
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TTC’2003 10/06/2003 Qualification
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TTC’2003 10/06/2003 Qualification
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BACK Résumé : Outil de traitement
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1 Principes généraux de l’outil
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1.2.3 Valise de piste L’outil peu
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2 Capacités fonctionnelles 2.1 Arc
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Vue f(t) 2.3.1 Vues y=f(t) Ces vues
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Maquette aéronef Alarmes Bar-graph
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2.3.3 Représentation trajectograph
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2.3.5 Vidéo Par ailleurs, si le ma
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3 Concept de structure d’accueil
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4 Exemples d’utilisation 4.1.1 HB
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SESSION 3 : Capteurs et dispositifs
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BACK THE NEXT GENERATION AIRBORNE D
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3. DC SPECIFICATIONS - SEEING THE W
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For the purposes of this paper it i
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hardware down and led to widely acc
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mechanism. In a system where a late
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0 X Y X' Y' 0 X Y Sampling Cycle X
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- Perform the exchange in a rigorou
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GLOSSARY AFDX Avionics Full DupleX
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The complete message is recorded by
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The L3 switches allow forwarding da
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Furthermore, the configuration of t
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BACK LOGICIEL JAVA D’ACQUISITION
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ISA ISA Interface utilisateur Objet
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CONCLUSION La première version de
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; ( ( + & 2+5. . & & , & . + & +2(
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( +, & + < 0 9& - & = (( + 1 - + +,
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BACK Telemetry Recording Workstatio
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Figure 1: Real-time pen tip display
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establishing different socket conne
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73 64 63 61 60 48 45 40 35 Level (d
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SESSION 5 : TELEMESURE (SPECTRE - M
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Currently various avenues are explo
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Binary X Binary to RNS and RNS to B
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The index multiplier block will be
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The current implementation consists
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Spécificité de la télémesure AI
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Technique COFDM : La modulation COF
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La réception s’effectue par une
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BACK ETCC'2003 European Test and Te
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ETCC'2003 European Test and Telemet
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SESSION 6 : SYSTEMES DE TELEMESURE
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f f p IF = R b = 4R b ∆f = 0. 7R
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2.3 ADC Fig.5 (a) y (t) and its spe
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2.5 FM demodulation Fig.9 I ‘(nT1
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References 1. Gardner FM. A BPSK/QP
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L/S/C /X/Ku /Ka band Spacelink Syst
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Spacelink System - The solution for
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SPOT Σ ∆ X band feed Data LNA Tr
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défilant. Le cahier des charges d
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TOURELLE HEXAPODE La tourelle hexap
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Ci après, tableau des spécificati
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BACK CRISTAUX PHOTONIQUES ET METAMA
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BACK Systems, Design & Tests Direct
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1. INTRODUCTION Cette communication
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Figure 2-1 Vue générale de la Bas
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3. ETALONNAGE DE LA BASE 3.1 PRINCI
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Par définition, le taux de polaris
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This document is the property of EA
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amplitude (dB) 10 0 -10 -20 -30 -40
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amplitude (dB) 10 0 -10 -20 -30 -40
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V1=K1.GVV.E.{[cos()-.sin()] + 1_vra
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Quelques calculs d’incertitude so
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- 21 - Amplitude polarisation verti
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- 23 - Amplitude composante vertica
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- 25 - Amplitude composante vertica
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3.4 SYNTHESE DES RESULTATS CONCERNA
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4.2 DEFINITION DE L'ANTENNE DE MISE
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4.4 DEFINITION DE L'ANTENNE DE REFE
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5.1.2 Diagrammes de rayonnement 5.1
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5.2 ANTENNE DE REFERENCE BANDE P 5.
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Gain (dBi) 5.2.2.2 Résultats Ils s
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Comme attendu, la coupe xOz présen
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Gain (dBi) 5.3.2 diagramme de rayon
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Gain (dBi) 15 10 5 0 -5 -10 -15 -20
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BACK INTRODUCTION MESURE DE CHAMP P
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MESURE DE CHAMP PAR SYSTEME PORTABL
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MESURE DE CHAMP PAR SYSTEME PORTABL
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Abstract Helicopters are relatively
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Au sol, la station réceptionne le
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BACK Résumé Architecture d’une
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Architecture type lanceur lourd ARI
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Architecture petit lanceur L’arch
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Diagramme de l’UCTM Voies analogi
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Exemples de capteurs utilisés Type
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SESSION 8 : COMPATIBILITE ELECTROMA
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1. CONTEXTE GENERAL Le durcissement
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Figure 1 : Actions de qualification
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5. LES PARAMETRES D’OPTIMISATION
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7. PERFORMANCE ET OPTIMISATION DU P
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La qualification du durcissement re
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UNIT Unit EMC documents : - groundi
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At equipment level EMC TEST PROGRAM
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BACK ETTC 2003. Le rôle de la simu
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comprenant des objets complexes, n
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Cette approche permet, avec les mê
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Les Thèses ONERA UPS Prise en comp
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Pression Ligne bifilaire non blind
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1.8 1,8 Tension continue V 1.6 1.4
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270 Ω I0 IL 2,7 kΩ (b) Alimenta
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What is the budget of the statistic
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Monte Carlo approach: This is a thr
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2 Etat de l’art des standards de
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2.1.6 Emissions standards 61967 par
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- Limites pour l’immunité DPI (e
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PRESENTATIONS POSTER / POSTER PRESE
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BACK LA TELEMESURE SUR AIRBUS JC GH
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Dans le cycle d ’essais en vol ,
Page 386 and 387: CONCLUSION - NOS BESOINS FUTURS AIR
Page 388 and 389: LOGICIELS DE MESURE ET DE TRAITEMEN
Page 394 and 395: In order to optimize the phase nois
Page 396 and 397: Photo-oscillator active device Opti
Page 398 and 399: the inverse of N×N correlation mat
Page 400 and 401: quasi-synchronous multiuser detecto
Page 402 and 403: Multiuser Interference Canceler ”
Page 404 and 405: the inverse of N×N correlation mat
Page 406 and 407: quasi-synchronous multiuser detecto
Page 408 and 409: Multiuser Interference Canceler ”
Page 410 and 411: All these sub-systems can be easily
Page 412 and 413: 3.5 ACPR RACK Gateway and satellite
Page 414 and 415: 4.2 COMPONENT DEGRADATION MEASUREME
Page 416 and 417: Indeed, when the objective of the t
Page 418 and 419: All the five points can be achieved
Page 420 and 421: M r Mmax (0 dB, -180°) b = 0 a ωc
Page 422 and 423: 2 - Test devices at ENSICA Souffler
Page 424 and 425: Soufflerie à Densité Variable (SD
Page 426 and 427: Capacité : - pour la charge axiale
Page 428 and 429: Machine d’essai de fatigue en fle
Page 430 and 431: torsion. - asservissement de chaque
Page 432 and 433: KEY 1 WORD IENA PACKET format An IE
Page 434 and 435: TD: “0” means that the paramete
Page 438 and 439: BACK UTILISATION de CAMERAS NUMERIQ
Page 440 and 441: TABLE DES MATIÈRES 1. INTRODUCTION
Page 442 and 443: 2. CONTEXTE DES ESSAIS Le but des e
Page 444 and 445: 3. LES BESOINS ET LES CONTRAINTES 3
Page 446 and 447: 4. CHOIX DE LA CAMERA 4.1 Démarche
Page 448 and 449: 5.1.4 Adaptations Les deux principa
Page 450 and 451: Tir d'un missile AIR/AIR éjecté T
Page 452 and 453: 6. CONCLUSION Cette évaluation mon
Page 454 and 455: Capteur Intelligent IEEE 1451.4 Pri
Page 456 and 457: pC/g Piezo Accelerometer mV/g Piezo
Page 458 and 459: BACK F. Mailly et Al. ETTC 2003 MIC
Page 460 and 461: 4.2. Sensitivity according to the h
Page 462 and 463: BACK STUDY OF 3∆t PASSIVE LOCATIN
Page 464 and 465: ∆t 1 ∆t ∆t 2 = t = t M N −1
Page 466 and 467: For the speed of the reentry vehicl
Page 468 and 469: BACK TITLE In orbit satellite Gain
Page 470 and 471: dBm dBm Results obtain with the con
Page 472 and 473: 3. NEW METHOD DEVELOPPED FOR IOT SA
Page 474 and 475: The following figures present the g
Page 476 and 477: 3.2 Analysis of the contribution Th
Page 478 and 479: ETSC Annual Activities Gerhard Maye
Page 480 and 481: BACK Abstract European Telemetry St
Page 482 and 483: The file structure is also adopted
Page 484 and 485: BACK The statistical Evaluation Of
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BACK Abstract Vendor Independent Da
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