Written by a Federal Aviation Administration (FAA) consultant designated engineering representative (DER) and an electronics hardware design engineer who together taught the DO-254 class at the Radio Technical Commission for Aeronautics, Inc. (RTCA) in Washington, District of Columbia, USA, Airborne Electronic Hardware Design Assurance: A Practitioner's Guide to RTCA/DO-254 is a testimony to the lessons learned and wisdom gained from many years of first-hand experience in the design, verification, and approval of airborne electronic hardware. This practical guide to the use of RTCA/DO-254 in the development of airborne electronic hardware for safety critical airborne applications: Describes how to optimize engineering processes and practices to harmonize with DO-254 Addresses the single most problematic aspect of engineering and compliance to DO-254—poorly written requirements Includes a tutorial on how to write requirements that will minimize the cost and effort of electronic design and verification Discusses the common pitfalls encountered by practitioners of DO-254, along with how those pitfalls occur and what can be done about them Settles the ongoing debate and misconceptions about the true definition of a derived requirement Promotes embracing DO-254 as the best means to achieve compliance to it, as well as the best path to high-quality electronic hardware Airborne Electronic Hardware Design Assurance: A Practitioner's Guide to RTCA/DO-254 offers real-world insight into RTCA/DO-254 and how its objectives can be satisfied. It provides engineers with valuable information that can be applied to any project to make compliance to DO-254 as easy and problem-free as possible.

Written by a Federal Aviation Administration (FAA) consultant designated engineering representative (DER) and an electronics hardware design engineer who together taught the DO-254 class at the Radio Technical Commission for Aeronautics, Inc. (RTCA) in Washington, District of Columbia, USA, Airborne Electronic Hardware Design Assurance: A Practitioner's Guide to RTCA/DO-254 is a testimony to the lessons learned and wisdom gained from many years of first-hand experience in the design, verification, and approval of airborne electronic hardware. This practical guide to the use of RTCA/DO-254 in the development of airborne electronic hardware for safety critical airborne applications: Describes how to optimize engineering processes and practices to harmonize with DO-254 Addresses the single most problematic aspect of engineering and compliance to DO-254—poorly written requirements Includes a tutorial on how to write requirements that will minimize the cost and effort of electronic design and verification Discusses the common pitfalls encountered by practitioners of DO-254, along with how those pitfalls occur and what can be done about them Settles the ongoing debate and misconceptions about the true definition of a derived requirement Promotes embracing DO-254 as the best means to achieve compliance to it, as well as the best path to high-quality electronic hardware Airborne Electronic Hardware Design Assurance: A Practitioner's Guide to RTCA/DO-254 offers real-world insight into RTCA/DO-254 and how its objectives can be satisfied. It provides engineers with valuable information that can be applied to any project to make compliance to DO-254 as easy and problem-free as possible.

The amount of software used in safety-critical systems is increasing at a rapid rate. At the same time, software technology is changing, projects are pressed to develop software faster and more cheaply, and the software is being used in more critical ways. Developing Safety-Critical Software: A Practical Guide for Aviation Software and DO-178C Compliance equips you with the information you need to effectively and efficiently develop safety-critical, life-critical, and mission-critical software for aviation. The principles also apply to software for automotive, medical, nuclear, and other safety-critical domains. An international authority on safety-critical software, the author helped write DO-178C and the U.S. Federal Aviation Administration’s policy and guidance on safety-critical software. In this book, she draws on more than 20 years of experience as a certification authority, an avionics manufacturer, an aircraft integrator, and a software developer to present best practices, real-world examples, and concrete recommendations. The book includes: An overview of how software fits into the systems and safety processes Detailed examination of DO-178C and how to effectively apply the guidance Insight into the DO-178C-related documents on tool qualification (DO-330), model-based development (DO-331), object-oriented technology (DO-332), and formal methods (DO-333) Practical tips for the successful development of safety-critical software and certification Insightful coverage of some of the more challenging topics in safety-critical software development and verification, including real-time operating systems, partitioning, configuration data, software reuse, previously developed software, reverse engineering, and outsourcing and offshoring An invaluable reference for systems and software managers, developers, and quality assurance personnel, this book provides a wealth of information to help you develop, manage, and approve safety-critical software more confidently.

Here's a unique resource that provides you with an up-to-date understanding of how to plan, analyze, and design next-generation broadband wireless networks. This comprehensive book includes all the necessary background information needed to fully understand the material and places emphasis on practical engineering know-how that can be readily applied to designing OFDM-based systems. You find detailed discussions on everything from the physical and media access control layers, to QoS and security functions. Rather than just offering simple explanations of standards, this invaluable book takes a close look at live, real-world systems, explaining how the technical features work and why they were adopted. Moreover, the author includes his own design frameworks and rules that have been developed through his own extensive research and experience. This comprehensive reference is supported with over 170 illustrations and more than 250 equations.

Until this book, aviation developers were frantically forced to search thousand of aviation standards for relevant information on aircraft, systems, software, and hardware development. Similar to designing a skyscraper by searching through a hardware store for parts, the results were chaotic and disconnected at best. But Today, aviation systems are increasingly integrated, complex, and inter-related; indeed, a new Ecosystem approach is required to succeed in aviation development. In his latest book Aviation Development Ecosystem, one of the world's foremost authorities on aviation development and certification clearly describes and explains in detail the true "Ecosystem" of aviation Safety, Systems, Hardware, and Software and "How To" apply the related standards and guidelines TOGETHER, including the following for aircraft, ground systems, eVTOL, rotorcraft, civil aviation, and military aircraft: DO-178C for Airborne Software: ARP4754A for Aircraft & Systems Development ARP4761 for Safety & Assessments DO-254 for Airborne Hardware DO-278A for Ground & Satellite Based Systems TSO's, TC/STC's, & PMA's DO-330 for Software Tool Qualification DO-331 for Model-Based Development DO-332 for Object Oriented Technology DO-160 for Environmental Testing DO-200B for Aeronautical Data DO-326A for Cyber-Security Multi-Core Processing Requirements, Design and Logic/Code Implementation Validation & Verification Traceability & Transition Criteria Aviation Plans, Standards, & Checklists Quality Assurance & Certification Mitigating Common Mistakes Reducing Engineering / Certification Costs & Risks Best Practices and How-To-Succeed in Aviation Development & Certification The author, Mr. Vance Hilderman, was the principal founder/CTO of three of the world's most significant aviation development/certification companies including TekSci, HighRely, and AFuzion. Hilderman has trained over 25,500 engineers in 700 aviation companies and 30 countries the above topics. His intellectual property is in use by 70% of the world's top 300 aviation and systems developers worldwide, and he has employed and personally presided over 500 of the world's foremost aviation engineers on 300+ projects the past thirty-five years. This book is the Capstone of his career and he readily provides the practical knowledge gained via tens of thousands of hours personally designing and certifying the aviation systems relied upon today for civil aircraft, military aircraft, UAV's, eVTOL, satellites, ground systems, and UAS's.

Agent Technology, or Agent-Based Approaches, is a new paradigm for developing software applications. It has been hailed as 'the next significant breakthrough in software development', and 'the new revolution in software' after object technology or object-oriented programming. In this context, an agent is a computer system which is capable of acting autonomously in its environment in order to meet its design objectives. So in the area of concurrent design and manufacturing, a manufacturing resource, namely a machine or an operator, may cooperate and negotiate with other agents for task assignment; and an existing engineering software can be integrated with a distributed integrated engineering design and manufacturing system. Hence in agent-based systems, there is no centralized system control structure, and no pre-defined agenda for the system execution, as exist in traditional systems. This book systematically describes the principles, key issues, and applications of agent technology in relation to concurrent engineering design and manufacturing. It introduces the methodology, standards, frameworks, tools, and languages of agent-based approaches and presents a general procedure for building agent-based concurrent engineering design and manufacturing systems. Both professional and university researchers and postgraduates should find this an invaluable presentation of the corresponding theories and methods, with some practical examples for developing multi-agent systems in the domain.

Civil Aircraft Electrical Power System Safety Assessment: Issues and Practices provides guidelines and methods for conducting a safety assessment process on civil airborne systems and equipment. As civil aircraft electrical systems become more complicated, electrical wiring failures have become a huge concern in industry and government—especially on aging platforms. There have been several accidents (most recently battery problems on the Boeing 777) with some of these having a relationship to wiring and power generation. Featuring a case study on the continuous safety assessment process of the civil airborne electrical power system, this book addresses problems, issues and troubleshooting techniques such as single event effects (SEE), the failure effects of electrical wiring interconnection systems (EWIS), formal theories and safety analysis methods in civil aircrafts. - Introduces how to conduct assignment of development assurance levels for the electrical power system - Includes safety assessments of aging platforms and their respective Electrical Wiring Interconnection System (EWIS) - Features material on failure mechanisms for wiring systems and discussion of Failure Modes and Effects Analysis (FMEA) sustainment