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Aircraft Systems Classifications: A Handbook of Characteristics and Design Guidelines [Kõva köide]

Series edited by (MIT), (Cranfield University, UK), Series edited by (University of Liverpool, UK), (BAE Systems, UK)
  • Formaat: Hardback, 384 pages, kõrgus x laius x paksus: 10x10x10 mm, kaal: 454 g
  • Sari: Aerospace Series
  • Ilmumisaeg: 10-May-2022
  • Kirjastus: John Wiley & Sons Inc
  • ISBN-10: 1119771846
  • ISBN-13: 9781119771845
Teised raamatud teemal:
Aircraft Systems Classifications: A Handbook of Characteristics and Design GuidelinesSuurem pilt
  • Formaat: Hardback, 384 pages, kõrgus x laius x paksus: 10x10x10 mm, kaal: 454 g
  • Sari: Aerospace Series
  • Ilmumisaeg: 10-May-2022
  • Kirjastus: John Wiley & Sons Inc
  • ISBN-10: 1119771846
  • ISBN-13: 9781119771845
Teised raamatud teemal:
Püsilink: https://www.kriso.ee/db/9781119771845.html
Märksõnad:
Aircraft Systems Classifications Enables aerospace professionals to quickly and accurately reference key information about all types of aircraft systems Aircraft Systems Classifications: A Handbook of Characteristics and Design Guidelines provides comprehensive information on aircraft systems delivered in a concise, direct, and standardized way, allowing readers to easily find the information they need. The book presents a full set of characteristics and requirements for all types of aircraft systems, including avionic, mission, and supporting ground systems, in a single volume. Readers can delve further into specific topics by referencing the detailed glossary and bibliography. To aid in reader comprehension, each aircraft system is broken down according to various criteria, such as: Purpose, description, and safety Integration with other systems Key interfaces and design drivers Modeling and simulation Best practices and future trends Written for aerospace professionals, researchers, and advanced students with some existing knowledge of the aircraft industry, this book allows readers to quickly reference information on every aspect of aircraft systems.
About the Authors ix
Acknowledgements xi
Sources of Background Information xiii
Glossary xv
1 Introduction
1(4)
Further Reading
4(1)
2 The Airframe and Systems Overview
5(32)
2.1 Introduction
5(1)
2.2 The Airframe
6(4)
2.3 The Aircraft Systems
10(4)
2.4 Classification of Aircraft Roles
14(11)
2.5 Classification of Systems
25(1)
2.6 Stakeholders
26(1)
2.7 Example Architectures
27(2)
2.8 Data Bus
29(5)
2.9 Summary and Conclusions
34(1)
References
34(1)
Exercises
35(2)
3 Vehicle Systems
37(90)
3.1 Propulsion System
38(6)
3.2 Fuel System
44(5)
3.3 Electrical Power Generation and Distribution
49(4)
3.4 Hydraulic Power Generation and Distribution
53(3)
3.5 Bleed Air System
56(3)
3.6 Secondary Power Systems
59(2)
3.7 Emergency Power Systems
61(4)
3.8 Flight Control System
65(3)
3.9 Landing Gear
68(3)
3.10 Brakes and Anti-skid
71(2)
3.11 Steering System
73(3)
3.12 Environmental Control System
76(3)
3.13 Fire Protection System
79(3)
3.14 Ice Detection
82(2)
3.15 Ice Protection
84(2)
3.16 External Lighting
86(3)
3.17 Probe Heating
89(2)
3.18 Vehicle Management System (VMS)
91(2)
3.19 Crew Escape
93(4)
3.20 Canopy Jettison
97(2)
3.21 Oxygen
99(3)
3.22 Biological and Chemical Protection
102(2)
3.23 Arrestor Hook
104(3)
3.24 Brake Parachute
107(3)
3.25 Anti-spin Parachute
110(2)
3.26 Galley
112(3)
3.27 Passenger Evacuation
115(2)
3.28 In-Flight Entertainment
117(2)
3.29 Toilet and Water Waste
119(3)
3.30 Cabin and Emergency Lighting
122(1)
References
123(3)
Exercise
126(1)
4 Avionic Systems
127(64)
4.1 Displays and Controls
127(4)
4.2 Communications
131(3)
4.3 Navigation
134(1)
4.4 Example Navigation System Architecture
135(3)
4.5 Flight Management System (FMS)
138(2)
4.6 Weather Radar
140(3)
4.7 Air Traffic Control (ATC) Transponder
143(3)
4.8 Traffic Collision and Avoidance System (TCAS)
146(3)
4.9 Terrain Avoidance and Warning System (TAWS)
149(3)
4.10 Distance Measuring Equipment (DME)/TACAN
152(2)
4.11 VHF Omni-Ranging (VOR)
154(2)
4.12 Automatic Flight Control System
156(4)
4.13 Radar Altimeter (Rad Alt)
160(3)
4.14 Automated Landing Aids
163(5)
4.15 Air Data System (ADS)
168(4)
4.16 Accident Data Recording System (ADRS)
172(2)
4.17 Electronic Flight Bag (EFB)
174(4)
4.18 Prognostics and Health Management System (PHM)
178(3)
4.19 Internal Lighting
181(2)
4.20 Integrated Modular Architecture (IMA)
183(2)
4.21 Antennas
185(4)
References
189(2)
5 Mission Systems
191(50)
5.1 Radar System
192(5)
5.2 Electro-optical System
197(3)
5.3 Electronic Support Measures (ESM)
200(2)
5.4 Magnetic Anomaly Detection (MAD)
202(3)
5.5 Acoustic System
205(2)
5.6 Mission Computing System
207(2)
5.7 Defensive Aids
209(3)
5.8 Station Keeping System
212(2)
5.9 Electronic Warfare System
214(3)
5.10 Camera System
217(3)
5.11 Head Up Display (HUD)
220(2)
5.12 Helmet Mounted Systems
222(2)
5.13 Data Link
224(3)
5.14 Weapon System
227(3)
5.15 Mission System Displays and Controls
230(4)
5.16 Mission System Antennas
234(3)
References
237(2)
Further Reading
239(1)
Exercises
239(2)
6 Supporting Ground Systems
241(16)
6.1 Flight Test Data Analysis
243(3)
6.2 Maintenance Management System
246(2)
6.3 Accident Data Recording
248(2)
6.4 Mission Data Management (Mission Support System)
250(2)
6.5 UAV Control
252(2)
References
254(1)
Exercises
255(2)
7 Modelling of Systems Architectures
257(48)
7.1 Introduction
257(2)
1.2 Literature Survey of Methods
259(18)
7.3 Avionics Integration Architecture Methodology
277(15)
7.4 Avionics Integration Modelling of Optimisation
292(5)
7.5 Simulations and Results for a Sample Architecture
297(3)
7.6 Conclusion
300(1)
References
300(5)
8 Summary and Future Developments
305(24)
8.1 Introduction
305(1)
8.2 Systems of Systems
305(9)
8.3 Architectures
314(1)
8.4 Other Considerations
315(8)
8.5 Conclusion
323(1)
8.6 What's Next?
323(4)
Exercise
327(2)
Index 329
Allan Seabridge is a member of the BAE Systems Heritage Department at Warton and retired as Head of Flight Systems Engineering after a long career with BAE Systems. He has over 50 years' experience in aerospace systems engineering, business development, and research & development, working on major projects including Canberra, Jaguar, Tornado, EAP, Typhoon, and Nimrod. Since retiring he has developed an interest in engineering education leading to the design and delivery of systems and engineering courses at a number of UK universities at the undergraduate and postgraduate level.

Mohammad Radaei has a PhD from Cranfield University in aerospace engineering, specializing in avionics systems integration. He obtained a BSc in aeronautical engineering from Air University, and MSc in aerospace engineering from National University of Iran in Tehran. He also holds a commercial pilot's license. His research interests include aircraft systems design, avionics systems integration, systems architecting, aircraft and systems flight testing, applied mathematics, flight dynamics and control of manned and unmanned aircraft, as well as human machine interactions. He is currently lecturing in avionics systems at a number of universities.