ETTC'2003 - SEE
ETTC'2003 - SEE ETTC'2003 - SEE
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
# ' & (+ + 7+ + + 6 +,,. & 2+5. & 0 + + & + . & * . + &,* & ( ?+ , ( + & + & / - . +, & (( + ( * ,- & 0 + . + & 1 ( , + & 1 + 0 + C • . ( :; + '
- Page 168 and 169: 1 Principes généraux de l’outil
- Page 170 and 171: 1.2.3 Valise de piste L’outil peu
- Page 172 and 173: 2 Capacités fonctionnelles 2.1 Arc
- Page 174 and 175: Vue f(t) 2.3.1 Vues y=f(t) Ces vues
- Page 176 and 177: Maquette aéronef Alarmes Bar-graph
- Page 178 and 179: 2.3.3 Représentation trajectograph
- Page 180 and 181: 2.3.5 Vidéo Par ailleurs, si le ma
- Page 182 and 183: 3 Concept de structure d’accueil
- Page 184 and 185: 4 Exemples d’utilisation 4.1.1 HB
- Page 186 and 187: SESSION 3 : Capteurs et dispositifs
- Page 188 and 189: BACK THE NEXT GENERATION AIRBORNE D
- Page 190 and 191: 3. DC SPECIFICATIONS - SEEING THE W
- Page 192 and 193: For the purposes of this paper it i
- Page 194 and 195: hardware down and led to widely acc
- Page 196 and 197: mechanism. In a system where a late
- Page 198 and 199: 0 X Y X' Y' 0 X Y Sampling Cycle X
- Page 200 and 201: - Perform the exchange in a rigorou
- Page 202 and 203: GLOSSARY AFDX Avionics Full DupleX
- Page 204 and 205: The complete message is recorded by
- Page 206 and 207: The L3 switches allow forwarding da
- Page 208 and 209: Furthermore, the configuration of t
- Page 210 and 211: BACK LOGICIEL JAVA D’ACQUISITION
- Page 212 and 213: ISA ISA Interface utilisateur Objet
- Page 214 and 215: CONCLUSION La première version de
- Page 216 and 217: ; ( ( + & 2+5. . & & , & . + & +2(
- Page 220 and 221: BACK Telemetry Recording Workstatio
- Page 222 and 223: Figure 1: Real-time pen tip display
- Page 224 and 225: establishing different socket conne
- Page 226 and 227: 73 64 63 61 60 48 45 40 35 Level (d
- Page 228 and 229: SESSION 5 : TELEMESURE (SPECTRE - M
- Page 230 and 231: Currently various avenues are explo
- Page 232 and 233: Binary X Binary to RNS and RNS to B
- Page 234 and 235: The index multiplier block will be
- Page 236 and 237: The current implementation consists
- Page 238 and 239: Spécificité de la télémesure AI
- Page 240 and 241: Technique COFDM : La modulation COF
- Page 242 and 243: La réception s’effectue par une
- Page 244 and 245: BACK ETCC'2003 European Test and Te
- Page 246 and 247: ETCC'2003 European Test and Telemet
- Page 248 and 249: ETCC'2003 European Test and Telemet
- Page 250 and 251: ETCC'2003 European Test and Telemet
- Page 252 and 253: SESSION 6 : SYSTEMES DE TELEMESURE
- Page 254 and 255: f f p IF = R b = 4R b ∆f = 0. 7R
- Page 256 and 257: 2.3 ADC Fig.5 (a) y (t) and its spe
- Page 258 and 259: 2.5 FM demodulation Fig.9 I ‘(nT1
- Page 260 and 261: References 1. Gardner FM. A BPSK/QP
- Page 262 and 263: L/S/C /X/Ku /Ka band Spacelink Syst
- Page 264 and 265: Spacelink System - The solution for
- Page 266 and 267: SPOT Σ ∆ X band feed Data LNA Tr
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