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El. knyga: Systems Engineering for Commercial Aircraft: A Domain-Specific Adaptation

(Principla Engineer, Burnham Systems, CA)
  • Formatas: 314 pages
  • Išleidimo metai: 10-Sep-2020
  • Leidėjas: Routledge
  • Kalba: eng
  • ISBN-13: 9781000152050
Kitos knygos pagal šią temą:
Systems Engineering for Commercial Aircraft: A Domain-Specific AdaptationDidesnis paveikslėlis
  • Formatas: 314 pages
  • Išleidimo metai: 10-Sep-2020
  • Leidėjas: Routledge
  • Kalba: eng
  • ISBN-13: 9781000152050
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The key principle of systems engineering is that an aircraft should be considered as a whole and not as a collection of parts. Another principle is that the requirements for the aircraft and its subsystems emanate from a logical set of organized functions and from economic or customer-oriented requirements as well as the regulatory requirements for certification. The resulting process promises to synthesize and validate the design of aircraft which are higher in quality, better meet customer requirements and are most economical to operate. This book is more of a how to and a why to rather than a what to guide. It stresses systems engineering is an integrated technical-managerial process that can be adapted without sacrificing quality in which risk handling and management is a major part. It explains that the systems view applies to both the aircraft and the entire air transport system. The book emphasizes that system engineering is not an added layer of processes on top of the existing design processes; it is the glue that holds all the other processes together. The readership includes the aircraft industry, suppliers and regulatory communities, especially technical, program and procurement managers; systems, design and specialty engineers (human factors, reliability, safety, etc.); students of aeronautical and systems engineering and technical management; and government agencies such as FAA and JAA.

Recenzijos

In this update Scott Jackson emphasizes and amplifies why systems engineering is critical for engineers and project managers, and how to apply it to developing modern commercial aircraft. His additional emphasis on organizational effects bridges the traditional gaps between engineering and project management and manifests the power of systems engineering to integrate across boundaries among products, services, people, and organizations. Ronald S. Carson, Missouri University of Science & Technology, USA and The Boeing Company (retired) This book addresses the subject respecting the characteristics of each organization, always showing the advantages of implementing the SE focused on the results. Scott Jackson efficiently and objectively presents how to address the life cycle of the aircraft in a functional vision. He concentrates on the application of the vision of the development of the whole as distinct from the parts and furnishes an objective way to facilitate the understanding of the roles and responsibilities within the organization when using Systems Engineering. Wellington M. Oliveira, Systems Engineering - EMBRAER S.A.

List of Figures xi
List of Tables xiii
Acknowledgments xv
Acronyms and Abbreviations xvii
Symbols xxiii
Preface xxv
1 Introduction 1(8)
1.1 Definition of a System
1(1)
1.2 Definition of Systems Engineering
2(1)
1.3 Historical Background
3(1)
1.4 Overview of this Book
4(1)
1.5 Roadmap for Applying Systems Engineering to Commercial Aircraft
5(1)
1.6 Summary of Themes
6(3)
2 Commercial Aircraft 9(12)
2.1 The Commercial Aircraft Industry
9(1)
2.2 Levels of SE Application
10(1)
2.3 Aircraft Architecture
11(4)
2.4 Advanced Technologies on Aircraft
15(4)
2.5 Aircraft Manufacturing Processes
19(1)
2.6 Trends in Commercial Aviation
19(2)
3 Functional Analysis 21(22)
3.1 The SE Life-Cycle Functions
23(5)
3.2 Aircraft System-Level Functions
28(1)
3.3 Aircraft-Level Functions
29(11)
3.4 Functional Aspects of Safety
40(1)
3.5 The Cluster Model
40(2)
3.6 The Swim Lane Model
42(1)
4 Requirements and Needs 43(24)
4.1 Requirements Definition
43(1)
4.2 Requirements Types
43(3)
4.3 Requirements Development
46(4)
4.4 Requirements Sources
50(3)
4.5 Requirements Allocation to System Elements
53(1)
4.6 Derived Requirements
53(1)
4.7 The Principle of Top-Down Allocation
54(4)
4.8 Requirements Trade-Offs
58(2)
4.9 Requirements Categories for Certification
60(1)
4.10 Requirement Validation
61(2)
4.11 Avoiding Requirement Creep
63(4)
5 Constraints and Specialty Requirements 67(20)
5.1 Regulatory Requirements
67(1)
5.2 Mass Properties
68(2)
5.3 Dimensions
70(1)
5.4 Reliability
70(1)
5.5 Human Factors
71(5)
5.6 Environments
76(5)
5.7 Maintainability
81(3)
5.8 Design Standards
84(1)
5.9 Emitted Noise
84(1)
5.10 Emitted Electromagnetic Interference (EMI)
84(1)
5.11 Cost
85(1)
5.12 Transportability
85(1)
5.13 Flexibility and Expansion
85(1)
5.14 Permissibility
86(1)
6 Interfaces 87(10)
6.1 Functional Interfaces
88(3)
6.2 Physical Interfaces
91(1)
6.3 External Interfaces
91(1)
6.4 Internal Interfaces
92(1)
6.5 Operational Interfaces
93(1)
6.6 Interface Management
94(1)
6.7 The Interface Control Drawing (ICD)
94(1)
6.8 Development Fixtures (DFs)
95(1)
6.9 The N2 Diagram
95(1)
6.10 Interface Requirements
95(1)
6.11 Interface Verification
96(1)
7 Synthesis 97(10)
7.1 Aircraft Architecture
98(1)
7.2 Initial Concept
99(1)
7.3 Trade-Off Studies
99(1)
7.4 Quality Function Deployment (QFD)
100(3)
7.5 Safety Features
103(1)
7.6 Introduction of New Technologies
103(1)
7.7 Preliminary Design
104(3)
8 Top-Level Synthesis 107(16)
8.1 The Aircraft System
107(2)
8.2 Top-Level Aircraft Sizing
109(4)
8.3 Other Top-Level Requirements
113(1)
8.4 System Architecture
114(1)
8.5 Top-Level Constraints
114(1)
8.6 Economic Constraints
115(6)
8.7 Top-Level Trade-Offs
121(2)
9 Subsystem Synthesis 123(20)
9.1 Environmental Segment
124(2)
9.2 Avionics Segment
126(5)
9.3 Electrical Segment
131(1)
9.4 Interiors Segment
132(2)
9.5 Mechanical Segment
134(2)
9.6 Propulsion Segment
136(3)
9.7 Auxiliary Segment (ATA 49)
139(1)
9.8 Airframe Segment
139(2)
9.9 Allocation to Software
141(1)
9.10 Subsystem Constraints
141(2)
10 Certification, Safety, and Software 143(16)
10.1 Certification
144(1)
10.2 Safety
144(3)
10.3 Software Development and Certification
147(3)
10.4 Commercial Aviation Safety Team (CAST)
150(8)
10.5 Fatality Rate History
158(1)
11 Verification and Validation 159(6)
11.1 The Verification Matrix
159(1)
11.2 Traditional SE Verification
160(2)
11.3 Verification of Regulatory Requirements
162(1)
11.4 Verification of Customer Requirements
162(1)
11.5 Verification Sequence
162(1)
11.6 System Validation
163(1)
11.7 Qualification
163(2)
12 Systems Engineering Management and Control 165(18)
12.1 Management Responsibilities
165(3)
12.2 The Chief Systems Engineer (CSE)
168(1)
12.3 Integrated Product Development (IPD)
168(2)
12.4 Design Reviews
170(5)
12.5 Documentation
175(2)
12.6 Automated Requirements Tools
177(1)
12.7 Technical Performance Measurement (TPM)
177(1)
12.8 Software Management
178(1)
12.9 Supplier Management
178(2)
12.10 Configuration Management
180(1)
12.11 Integration Planning
181(2)
13 Adapting Systems Engineering to the Commercial Aircraft Domain 183(18)
13.1 Adapting the Process
183(4)
13.2 Adapting the SE Process to the Existing Organization
187(14)
14 Large-Scale System Integration 201(14)
14.1 The System of Systems View
201(1)
14.2 Outsourcing
201(2)
14.3 Complexity and How It Increases Risks
203(4)
14.4 Managing the Risks of a Large-Scale System (LSS)
207(5)
14.5 Other Large-Scale System (LSS) Principles to Apply to Commercial Aircraft
212(1)
14.6 Summary
212(3)
15 Risk Management 215(14)
15.1 Overview of Risk Management
215(4)
15.2 Types of Consequences
219(1)
15.3 Root Causes of Risks
219(3)
15.4 Risk Mitigation Steps
222(1)
15.5 Issues
223(1)
15.6 Independent Review
223(2)
15.7 The Risk Management Process
225(1)
15.8 Risk Management Tools
225(1)
15.9 Opportunities
226(1)
15.10 Challenges for Risk Management
227(2)
16 Resilience of the Aircraft System 229(16)
16.1 The History of Resilience
229(1)
16.2 The Definition of Resilience
230(1)
16.3 Is Resilience Measureable?
231(1)
16.4 Design Rules and Example Solutions
231(11)
16.5 Other Rules
242(1)
16.6 A Final Word on Interdependency
242(3)
Final Comments 245(2)
The Systems Mindset
245(1)
The Risk Mindset
245(1)
The Resilience Mindset
246(1)
Reference
246(1)
Appendix 1 The Mathematics of Reliability Allocation 247(4)
Appendix 2 Example Commercial Specification Outline 251(8)
Appendix 3 Systems Engineering Automated Tools 259(2)
Bibliography 261(8)
Glossary 269(10)
Index 279
Scott Jackson is a lecturer in Systems Architecting and Engineering at the University of Southern California. He is also Principal Engineer for Burnham Systems Consulting, currently working with Embraer in Brazil on systems engineering. Scott received his BS degree in Aeronautical Engineering from the University of Texas in 1957 and an MS degree from UCLA in 1966 in fluid mechanics. He also holds an MA in Liberal Arts from CSU Long Beach. Scott is currently a PhD candidate in systems engineering at the University of South Australia. Since 1965, Scotts work has been dedicated to systems engineering, culminating in a focus on its application to commercial aircraft at Boeing. He is a Fellow of the International Council on Systems Engineering (INCOSE) and a Boeing Associate Technical Fellow in Systems Engineering. In 2006, Scott was awarded the Distinguished Engineer Award by Orange County Engineering Council.
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