ABSTRACT

The key principle of systems engineering, a process now becoming widely applied in the commercial aircraft industry, 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 aims to provide the reader with the information to apply the systems engineering process to the design of new aircraft, derivative aircraft and to change-based designs. The principles of this book are applicable to passenger and cargo carrying aircraft and to commuter and business aircraft. It explains the principles of systems engineering in understandable terms, but does not attempt to educate the reader in the details of the process. Incorporating the latest thinking by FAA and JAA to utilize the systems engineering in the aircraft certification process, the author shows how current guidelines for certification of systems with software are in agreement with its main principles. These in turn can be applied at three levels: the aviation system, the aircraft as a whole and the aircraft subsystem levels. By providing guidelines for managing a commercial aircraft development using the principles of systems engineering, the book will enable engineers and managers to see the work they do in a new light. Whether developing a new aircraft from scratch or simply modifying a subsystem, they will be assisted to see their product from a functional point of view and thus to develop new vehicles which are better, cheaper and safer than before. The readership includes the aircraft industry, suppliers and regulatory communities: especially technic

chapter 1|8 pages

Introduction

chapter 2|12 pages

Commercial Aircraft

chapter 3|22 pages

Functional Analysis

chapter 4|24 pages

Requirements and Needs

chapter 5|20 pages

Constraints and Specialty Requirements

chapter 6|10 pages

Interfaces

chapter 7|10 pages

Synthesis

chapter 8|16 pages

Top-Level Synthesis

chapter 9|20 pages

Subsystem Synthesis

chapter 10|16 pages

Certification, Safety, and Software

chapter 11|6 pages

Verification and Validation

chapter 12|18 pages

Systems Engineering Management and Control

chapter 14|14 pages

Large-Scale System Integration

chapter 15|14 pages

Risk Management

chapter 16|16 pages

Resilience of the Aircraft System