Integrated and Modular Systems for Commercial ... - Nonstop Systems

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1 System Reliability λunit = 5x10-5 Example: /h MTBFunit = 20,000 hrs N-Parallel Redundancy 0.5 0 20k (=MTBF) 40k Operating time (hrs) 100k 15 - brute <strong>for</strong>ce: inefficient to achieve very high system reliability - 40 37 10 5 Number of redundant units 3 0.5 1 ©1995-1997 F.M.G. Dörenberg
1 System Reliability λunit = 5x10-5 Example: /h MTBFunit = 20,000 hrs N-Parallel Redundancy 0.5 0 20k (=MTBF) 40k Operating time (hrs) 100k 15 - goals: low cost & low redundancy but high rel. & safety - 41 38 10 5 60k Number of redundant units 3 Desired region 0.5 100k 1 0.9 - 0.95 ©1995-1997 F.M.G. Dörenberg
Page 1 and 2: Integrated and Modular Systems for
Page 3 and 4: Integrated and Modular Systems for
Page 5 and 6: Integrated and Modular Avionics •
Page 7 and 8: Engine thrust Structure & Gear Comp
Page 9 and 10: Why change avionics? • Airline/Op
Page 11 and 12: Operators seek revenue enhancement
Page 13 and 14: Why change avionics? (cont’d) •
Page 15 and 16: Why change avionics? (cont’d) •
Page 17 and 18: Avionics business • high-tech but
Page 19 and 20: Changing airtransport environment 1
Page 21 and 22: 5000 Pax-km (billions, log-scale) 1
Page 23 and 24: Billions of 1995 US $ 80 60 40 20 9
Page 25 and 26: 24% 23% 23% 30% 737-300 ($1834/hr)
Page 27 and 28: Big $ numbers life-time maintenance
Page 29 and 30: Save now and save later • increas
Page 31 and 32: Average schedule deviation costs de
Page 33 and 34: Integrated Modular Avionics Archite
Page 35 and 36: Fault Avoidance - prevent (by const
Page 37 and 38: Fault Tolerance Taxonomy Fault Tole
Page 39 and 40: Redundancy • Attributes: � form
Page 41: Basic ways to increase system relia
Page 45 and 46: Note: log-log scale F (t) 2-out-of-
Page 47 and 48: System architecture and design deci
Page 49 and 50: 1.0 Rconfig(t) 0.9 0.8 dual Redunda
Page 51 and 52: Simplex Dual Triplex Quad Dual-Dual
Page 53 and 54: Integration is necessary because...
Page 55 and 56: Integration trend: Multi-Mode Recei
Page 57 and 58: Integration issues • “integrate
Page 59 and 60: Fault Tolerance for Safety, Reliabi
Page 61 and 62: Quant. Prob. 1 10-3 10-5 10-7 10-9
Page 63 and 64: Failure System Condition Design Ass
Page 65 and 66: Electro-Magnetic Interference (EMI)
Page 67 and 68: Req's for Fault Avoidance (incl. Co
Page 69 and 70: Standardization issues • “gener
Page 71 and 72: Resources Hardware Software Standar
Page 73 and 74: Integration & Modularization • LR
Page 75 and 76: O/S I/O Maint. BIT Appl. Total CPU
Page 77 and 78: Effect of integrating additional fu
Page 79 and 80: assumes integration of related func
Page 81 and 82: Integration & Modularization • Ot
Page 83 and 84: German “WW II” radios • Modul
Page 85 and 86: German “WW II” radios • Recei
Page 87 and 88: Modular Electronics: Not a New Conc
Page 89 and 90: Modular Electronics: Not a New Conc
Page 91 and 92: IMA - Integrated Modular Avionics L
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IMA Level-1 • LRUs re-packaged as
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IMA Level-4 & -5 • Level-4: funct
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Major Areas of Systems Integration
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ATC/ATM FMS Functional Integration
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ATC/ATM FMS Functional Integration
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Integrated Flight & Thrust Control
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Modular Flight Control & Guidance C
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FCGC redundancy management - exampl
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FCGC redundancy management - exampl
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lliedSignal A E R O S P A C E Allie
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lliedSignal A E R O S P A C E Berie
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lliedSignal A E R O S P A C E Kiev
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AlliedSignal h/w AlliedSignal h/w +
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lliedSignal A E R O S P A C E ARIA-
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minus database flash memory minus D
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lliedSignal A E R O S P A C E Two I
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lliedSignal A E R O S P A C E Hazar
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lliedSignal A E R O S P A C E Hazar
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lliedSignal A E R O S P A C E 12,00
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lliedSignal A E R O S P A C E 20 15
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lliedSignal A E R O S P A C E CFIT
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lliedSignal A E R O S P A C E Terra
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lliedSignal A E R O S P A C E ref.:
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lliedSignal A E R O S P A C E Pink:
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lliedSignal A E R O S P A C E ≤
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lliedSignal A E R O S P A C E IHAS:
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lliedSignal A E R O S P A C E Stick
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lliedSignal A E R O S P A C E Advan
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lliedSignal A E R O S P A C E $ $$
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lliedSignal A E R O S P A C E a/c d
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lliedSignal A E R O S P A C E IHAS
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lliedSignal A E R O S P A C E Parti
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lliedSignal A E R O S P A C E Proce
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lliedSignal A E R O S P A C E Proce
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lliedSignal A E R O S P A C E Backp
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lliedSignal A E R O S P A C E sets
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lliedSignal A E R O S P A C E Growt
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lliedSignal A E R O S P A C E Fligh
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lliedSignal A E R O S P A C E Unifi
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lliedSignal A E R O S P A C E Typic
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lliedSignal A E R O S P A C E Integ
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lliedSignal A E R O S P A C E - Com
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Related utilities sub-systems that
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A/C Loads lliedSignal A E R O S P A
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lliedSignal A E R O S P A C E Integ
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lliedSignal A E R O S P A C E MAFT/
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lliedSignal A E R O S P A C E Globa
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from all other nodes + wrap from ow
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lliedSignal A E R O S P A C E RTEM
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lliedSignal A E R O S P A C E MAFT/
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1 Integrated and Modular Avionics
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3 FANS: Future Air Navigation Syste
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5 Component and System Performance
Page 215 and 216:
7 Component and System Performance
Page 217 and 218:
9 Future ........ (cont’d) • im
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11 150 k ↑ Total airplane signal
Page 221 and 222:
13 100 MB 80 MB 20 MB 10 MB 747-200
Page 223 and 224:
15 System Complexity and Size Typic
Page 225 and 226:
17 Given: Extrapolation ...... •
Page 227 and 228:
19 Enabling technologies - componen
Page 229 and 230:
Enabling technologies - drivers for
Page 231 and 232:
23 Enabling technologies - design /
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25 236-pin connector Example: PC mo
Page 235 and 236:
27 Example: integrated X-band power
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29 Cold-Cathode Field Emission Disp
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31 Enabling technologies - componen
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33 Resource Partitioning - part of
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35 Enabling technologies - communic
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37 High Medium Low Enabling technol
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39 Enabling technologies � s/w
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1 BOOKS BIBLIOGRAPHY F.J. Redmill (
Page 251 and 252:
3 M.L. Shooman: "A study of occurre
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