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

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Modular Flight Control & Guidance Computer 2x CPM (identical) X-puter + PowerPC 4x IOM PowerPC + GP µP BGT Bodenseewerk Gerätetechnik GmbH FCGC (x2) FC FG (FC) A A B B - FCGC internal architecture - ref.: R. Reichel: “Modular flight control and guidance computer”, Proc. 6th ERA Avionics Conf., London/UK, Dec. ‘92, 9 pp. 110 ©1995-1997 F.M.G. Dörenberg
FCGC redundancy management - examples FC FG (FC) A A B B Fault Free BGT Bodenseewerk Gerätetechnik GmbH FC FG (FC) A A B B A A B B FG (FC) FC FG (FC) A A B B - elevator control reconfiguration in response to module failures - - CPM failure - 111 ©1995-1997 F.M.G. Dörenberg
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Integrated and Modular Systems for
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Integrated and Modular Systems for
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Integrated and Modular Avionics •
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Engine thrust Structure & Gear Comp
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Why change avionics? • Airline/Op
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Operators seek revenue enhancement
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Why change avionics? (cont’d) •
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Why change avionics? (cont’d) •
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Avionics business • high-tech but
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Changing airtransport environment 1
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5000 Pax-km (billions, log-scale) 1
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Billions of 1995 US $ 80 60 40 20 9
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24% 23% 23% 30% 737-300 ($1834/hr)
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Big $ numbers life-time maintenance
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Save now and save later • increas
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Average schedule deviation costs de
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Integrated Modular Avionics Archite
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Fault Avoidance - prevent (by const
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Fault Tolerance Taxonomy Fault Tole
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Redundancy • Attributes: � form
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Basic ways to increase system relia
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1 System Reliability λunit = 5x10-
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Note: log-log scale F (t) 2-out-of-
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System architecture and design deci
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1.0 Rconfig(t) 0.9 0.8 dual Redunda
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Simplex Dual Triplex Quad Dual-Dual
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Integration is necessary because...
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Integration trend: Multi-Mode Recei
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Integration issues • “integrate
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Fault Tolerance for Safety, Reliabi
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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
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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
Page 93 and 94: IMA Level-1 • LRUs re-packaged as
Page 95 and 96: IMA Level-4 & -5 • Level-4: funct
Page 97 and 98: Major Areas of Systems Integration
Page 99 and 100: ATC/ATM FMS Functional Integration
Page 101 and 102: ATC/ATM FMS Functional Integration
Page 103 and 104: Integrated Flight & Thrust Control
Page 105 and 106: Modular Flight Control & Guidance C
Page 111: Modular Flight Control & Guidance C
Page 115 and 116: FCGC redundancy management - exampl
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Page 123 and 124: AlliedSignal h/w AlliedSignal h/w +
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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 Allie
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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
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7 Component and System Performance
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9 Future ........ (cont’d) • im
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11 150 k ↑ Total airplane signal
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13 100 MB 80 MB 20 MB 10 MB 747-200
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15 System Complexity and Size Typic
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17 Given: Extrapolation ...... •
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19 Enabling technologies - componen
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Enabling technologies - drivers for
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23 Enabling technologies - design /
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25 236-pin connector Example: PC mo
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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 (
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3 M.L. Shooman: "A study of occurre
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