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Design and Development of Aircraft Systems

By: Material type: TextTextPublication details: New Delhi Wiley 2013Edition: 2ndDescription: 312pISBN:
  • 9788126560301
Subject(s): DDC classification:
  • 629.133 MOI-D
Online resources:
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Reference Book Reference Book Amity Central Library ASET Aerospace Reference 629.133 MOI-D (Browse shelf(Opens below)) Link to resource Not For Loan 27505

1 Introduction

1.1 General

1.2 Systems Development

1.3 Skills

1.4 Overview



2 The Aircraft Systems

2.1 Introduction

2.2 Definitions

2.3 Everyday Examples of Systems

2.4 Aircraft Systems of Interest

2.5 Ground Systems

2.6 Generic System Definition



3 The Design and Development Process

3.1 Introduction

3.2 Definitions

3.3 The Product Life Cycle

3.4 Concept Phase

3.5 Definition Phase

3.6 Design Phase

3.7 Build Phase

3.8 Test Phase

3.9 Operate Phase

3.10 Disposal or Retirement Phase

3.11 Refurbishment Phase

3.12 Whole Life Cycle Tasks



4 Design Drivers

4.1 Introduction

4.2 Design Drivers in the Business Environment

4.3 Design Drivers in the Project Environment

4.4 Design Drivers in the Product Environment

4.5 Drivers in the Product Operating Environment

4.6 Interfaces with the Sub-System Environment

4.7 Obsolescence



5 Systems Architectures

5.1 Introduction

5.2 Definitions

5.3 Systems Architectures

5.4 Architecture Modelling and Trade-off

5.5 Example of a Developing Architecture

5.6 Evolution of Avionics Architectures



6 Systems Integration

6.1 Introduction

6.2 Definitions

6.3 Examples of Systems Integration

6.4 System Integration Skills

6.5 Management of Systems Integration

6.6 Highly Integrated Systems

6.7 Discussion



7 Verification of System Requirements

7.1 Introduction

7.2 Gathering Qualification Evidence in the Life Cycle

7.3 Test Methods

7.4 An Example Using a Radar System



8 Practical Considerations

8.1 Introduction

8.2 Stakeholders

8.3 Communications

8.4 Giving and Receiving Criticism

8.5 Supplier Relationships

8.6 Engineering Judgement

8.7 Complexity

8.8 Emergent Properties

8.9 Aircraft Wiring and Connectors

8.10 Bonding and Grounding



9 Configuration Control

9.1 Introduction

9.2 Configuration Control Process

9.3 A Simple Portrayal of a System

9.4 Varying System Configurations

9.5 Forwards and Backwards Compatibility

9.6 Factors Affecting Compatibility

9.7 System Evolution

9.8 Configuration Control

9.9 Interface Control



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

10.7 Integration of Aircraft Systems

10.8 Integration of Avionics Systems



11 Power Systems Issues

11.1 Introduction

11.2 Electrical System Description

11.3 Electrical Power Distribution System

11.4 Electrical System Design Issues

11.5 Hydraulic System Description

11.6 Hydraulic System Design Considerations

11.7 Aircraft System Energy Losses

11.8 Electrical System Power Dissipation

11.9 Hydraulic System Power Dissipation

11.10 More-Electric Aircraft Considerations



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 Systems

12.6 Analysis of the Fuel Penalties of Aircraft Systems



13 Conclusions

A Historical Footnote

References

Index

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