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Design and Development of Aircraft Systems

Design and Development of Aircraft Systems (Hardcover, 3)

Allan Seabridge (지은이)
John Wiley and Sons Ltd
266,240원

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Design and Development of Aircraft Systems
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· 제목 : Design and Development of Aircraft Systems (Hardcover, 3) 
· 분류 : 외국도서 > 기술공학 > 기술공학 > 우주공학
· ISBN : 9781119611509
· 쪽수 : 400쪽
· 출판일 : 2020-04-06

목차

About the Authors

Acknowledgements

Glossary of Terms

Chapter 1 – Introduction

1.1. General

1.2. System development

1.3. Skills

1.4. Human aspects

1.4.1. Introduction

1.4.2. Design considerations

1.4.3. Legislation

1.4.4. Summary of legal threats

1.4.5. Conclusions

1.5 Overview

References

Further Reading

Exercises

Chapter 2 – The Aircraft Systems

2.1. Introduction

2.2. Definitions

2.3. Everyday examples of systems

2.4. Aircraft Systems of Interest

2.4.1. Airframe systems

2.4.2. Vehicle systems

2.4.3. Interface characteristics of vehicle systems

2.4.4. Avionic systems

2.4.5. Interface characteristics of vehicle and avionic systems

2.4.6. Mission systems

2.4.7. Interface characteristics of mission systems

2.5. Ground systems

2.6. Generic System Definitions

References

Further Reading

Exercises

Chapter 3 – The Design and Development Process

3.1. Introduction

3.2. Definitions

3.3. The Product lifecycle

3.4. Concept phase

3.4.1. Engineering process

3.4.2. Engineering skills

3.5. Definition phase

3.5.1. Engineering process

3.5.2. Engineering skills

3.6. Design phase.

3.6.1. Engineering process

3.6.2. Engineering skills

3.7. Build phase

3.7.1. Engineering process

3.7.2. Engineering skills

3.8. Test Phase

3.8.1. Engineering process

3.8.2. Engineering skills

3.9. Operate phase

3.9.1. Engineering process

3.9.2. Engineering skills

3.10. Disposal or retirement phase

3.10.1. Engineering process

3.10.2. Engineering skills

3.11. Refurbishment phase

3.11.1. Engineering process

3.11.2. Engineering skills

3.12. Whole life cycle tasks

References

Further Reading

Exercises

Chapter 4 - Design Drivers

4.1. Introduction

4.2. Design drivers in the business environment

4.2.1. Customer

4.2.2. Market and competition

4.2.3. Capacity

4.2.4. Financial issues

4.2.5. Defence policy

4.2.6. Leisure and business interests

4.2.7. Politics

4.2.8. Technology

4.3. Design drivers in the project environment

4.3.1. Standards and regulations

4.3.2. Availability

4.3.3. Cost

4.3.4. Programme

4.3.5. Performance

4.3.6. Skills and resources

4.3.7. Health, safety and environment issues

4.3.8. Risk

4.4. Design drivers in the product environment

4.4.1. Functional performance

4.4.2. Human machine interface

4.4.3. Crew and passengers

4.4.4. Stores and cargo

4.4.5. Structure

4.4.6. Safety

4.4.7. Quality

4.4.8. Environmental conditions

4.5. Drivers in the product operating environment

4.5.1. Heat

4.5.2. Noise

4.5.3. RF radiation

4.5.4. Solar energy

4.5.5. Altitude

4.5.6. Temperature

4.5.7. Contaminants/destructive substances

4.5.8. Lightning

4.5.9. Nuclear, biological and chemical

4.5.10. Vibration

4.5.11. Shock

4.6. Interfaces with the sub-system environment

4.6.1. Physical interfaces

4.6.2. Power interfaces

4.6.3. Data communication interfaces

4.6.4. Input/output interfaces

4.6.5. Status/discrete interfaces

4.7. Obsolescence

4.7.1. Introduction

4.7.2. The threat of obsolescence in the product lifecycle

4.7.3. Managing obsolescence

4.8. Ageing Aircraft

4.8.1. Introduction

4.8.2. Some examples

4.8.3. Systems issues

4.8.4. Certification issues.

References

Further Reading

Chapter 5 - Systems Architectures

5.1. Introduction

5.2. Definitions

5.3. Systems architectures

5.3.1. Vehicle systems

5.3.2. Avionic systems

5.3.3. Mission systems

5.3.4. Cabin systems

5.3.5. Data bus

5.4. Architecture modelling and trade-off

5.5. Example of a developing architecture

5.6. Evolution of avionics architectures

5.6.1. Distributed analogue architecture

5.6.2. Distributed digital architecture

5.6.3. Federated digital architecture

5.6.4. Integrated modular architecture

5.7. Example architectures

5.7.1. Example 1 - The Systems architecture

5.7.2. Example 2 – Fight control system

5.7.3. Example 3 – Radar system

5.7.4. Example 4 – Vehicle systems management

References

Further Reading

Chapter 6 - Systems Integration

6.1. Introduction

6.2. Definitions

6.3. Examples of systems integration

6.3.1. Integration at the component level

6.3.2. Integration at the system level

6.3.3. Integration at the process level

6.3.4. Integration at the functional level

6.3.5. Integration at the information level

6.3.6. Integration at the prime contractor level

6.3.7. Integration arising from emergent properties

6.3.8. Further examples of integrated systems

6.4. System integration skills

6.5. Management of systems integration

6.5.1. Major activities

6.5.2. Major milestones

6.5.3. Decomposition and definition process

6.5.4. Integration and verification process

6.5.5. Component engineering

6.6. Highly integrated systems

6.7. Discussion

References

Further Reading

Chapter 7 – Verification of System Requirements

7.1. Introduction

7.2. Gathering qualification evidence in the lifecycle

7.3. Test methods

7.3.1. Inspection of design

7.3.2. Calculation

7.3.3. Analogy

7.3.4. Modelling and simulation

7.3.5. Test rigs

7.3.6. Environmental testing

7.3.7. Integration test rigs

7.3.8. Aircraft ground testing

7.3.9. Flight test

7.3.10. Trials

7.3.11. Operational test

7.3.12. Demonstrations.

7.4 An example using a radar system.

References

Further Reading

Chapter 8 - Practical Considerations

8.1. Introduction

8.2. Stakeholders

8.2.1. Identification of stakeholders

8.2.2. Classification of stakeholders

8.3. Communications

8.3.1. The nature of communication

8.3.2. Examples of organisation communication media

8.3.3. The cost of poor communication

8.3.4. A lesson learned

8.4. Giving and Receiving Criticism

8.4.1. The need for criticism in the design process

8.4.2. The nature of criticism

8.4.3. Behaviours associated with criticism

8.4.4. Conclusions

8.5. Supplier relationships

8.6. Engineering judgement

8.7. Complexity

8.8. Emergent properties

8.9. Wiring and connectors

8.9.1. Aircraft wiring

8.9.2. Aircraft breaks

8.9.3. Wiring bundle definitions

8.9.4. Wiring routing

8.9.5. Wiring sizing

8.9.6. Aircraft electrical signal types

8.9.7. Electrical segregation

8.9.8. The nature of aircraft wiring and connectors

8.9.9. Use of twisted pairs and quads

8.10 Bonding and grounding

References

Further Reading

Exercises

Chapter 9 – Configuration Control

9.1. Introduction

9.2. Configuration control process

9.3. A Simple portrayal of a system

9.4. Varying system configurations

9.4.1. System configuration A

9.4.2. System configuration B

9.4.3. System configuration C

9.5. Forwards and backwards compatibility

9.5.1. Forwards compatibility

9.5.2. Backwards compatibility

9.6. Factors Affecting Compatibility

9.6.1. Hardware

9.6.2. Software

9.6.3. Wiring

9.7. System evolution

9.8. Configuration control

9.9. Interface control

9.9.1. Interface control document

9.9.2. Aircraft level data bus data

9.9.3. System internal data bus data

9.9.4. Internal system input/output data

9.9.5. Fuel component interfaces

9.10. Control of day to day documents

Chapter 10 – Aircraft System Examples

10.1. Introduction

10.2. Design considerations

10.3. Safety and economic considerations

10.4. Failure severity categorisation

10.5. Design assurance levels

10.6 Redundancy

10.6.1. Architecture options

10.6.2. Systems examples

10.7. Integration of aircraft systems

10.7.1. Engine control system

10.7.2. Flight control system

10.7.3. Attitude measurement system

10.7.4. Air data system

10.7.5. Electrical power system

10.7.6. Hydraulic power system

10.8. Integration of avionics systems

Chapter 11 – Integration & complexity: the potential impact on flight safety

11.1. Introduction

11.2. Integration

11.3. Complexity

11.4. Automation

11.5. Impact on flight safety

11.6. Single pilot operation

11.7. Postscript – chaos discussion

References

Further Reading

Exercises

Chapter 12 – Key characteristics of aircraft systems

12.1. Introduction

12.2. Aircraft systems

12.3. Avionic systems

12.4. Mission systems

12.5. Sizing and scoping of systems

12.6. Analysis of the fuel penalties of aircraft systems

12.6.1. Introduction

12.6.2. Basic formulation of fuel weight penalties

12.6.3. Application of fuel weight penalty formulation to multi-phase flight.

12.6.4. Analysis of Fuel Weight Penalties Formulation for Multi-phase Flight

12.6.5. Use of fuel weight penalties to compare systems

12.6.6. Determining Input Data for Systems Weight Penalties Analysis

References

Chapter 13 - Conclusions

Index

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