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The purpose of this paper is to present a definition of modern configuration for a medium-altitude long-endurance unmanned aerial vehicle (MALE UAV) and its on-board systems to obtain a suitable basis for future definitions such as a possible logistic support configuration first hypothesis.

Starting from high-level requirements, both the UAV conceptual design and on-board systems preliminary design have been carried out through proprietary tools. Then, some peculiarities from previous studies, such as systems advanced UAV alternative energy, have been maintained and confirmed (diesel propulsion and energy storage system).

The improvement of a component of an aircraft can play a relevant role in the whole system. In the paper, it is considered how a concept of MALE UAV can evolve (this topic is considered by the authors since many years) by incorporating advanced on-board systems concepts.

The numerical results promote and support the use of advanced on-board system solutions and architectures to improve the effectiveness, efficiency and performance of MALE UAVs.

Usually, conceptual and preliminary design phases analyze in-depth the aerodynamic and structural solutions and aircraft performance. In this study, the authors aim to focus on the advanced on-board systems for MALE UAVs. This kind of aircraft is not yet a mature concept, with very few operating machines and many projects in the development phase.

The main objective of this paper is to investigate the role of knowledge management in aerospace industries and to provide a framework for knowledge management efforts specially designed for aerospace industries towards a knowledge‐based organization.

This is a conceptual article examining current perspectives of knowledge management regarding aerospace industries requirements. It provides a general framework for knowledge management applied in Iran Aerospace Industries Organization (AIO).

Providing a conceptual knowledge management framework can be applied to organizations practically. This framework has been applied in a large case study in Iran and is supported by practical implementation in AIO, one of the most important high‐tech industries in Iran.

This paper provides a very helpful guideline for practitioners in implementing knowledge management throughout the organizations and especially in large scale ones.

The paper may be of high value to researchers in the knowledge management field and to practitioners involved with KM adoption in the organizations. This study further opens up new lines of research and highlights implications for knowledge management efforts, including change management programs through KM tools. The paper also provides a synthesis and analysis of the viewpoints and the main factors as reflected in the literature on various dimensions of knowledge management.

This paper aims to unravel the technological innovation pattern in China’s aerospace industry. The technological innovation pattern of China’s aerospace industry is identified and its theoretical foundation, structure, philosophy, formation and effects on the development of China’s aerospace industry are explored.

First, the theoretical foundation of synergy innovation of China’s aerospace industry is reviewed to further identify the technological innovation pattern. Second, Chinese ancient philosophy (dialectical thinking) is used to explain the structure and process of synergy innovation in China’s aerospace industry. Third, the formation process of synergy innovation is introduced, and, finally, the effects of synergy innovation are discussed.

The technological innovation pattern of China’s aerospace industry has undergone an evolutionary process. During this process, China’s aerospace firms have formed a unique technological innovation pattern, synergy innovation, under China’s special political and economic background. The synergy innovation has three characteristics, including original, integrated and application-based. The synergy innovation pattern application is one of the most important reasons behind the great achievements of China’s aerospace industry.

A unique technological innovation pattern, synergy innovation, is proposed for the first time. A new perspective for understanding innovation is provided by applying the Chinese dialectical thinking to decipher the philosophy of the technological innovation pattern. Based on this, this paper suggests that China’s aerospace industry should follow the situation and apply the synergy innovation pattern to achieve development and growth. This paper also illustrates a multi-method approach and emphasizes the different levels of organizing for innovation.

The purpose of this paper is to explore the emergence of innovation in smart service systems to conceptualize how actor’s relationships through technology-enabled interactions can give birth to novel technologies, processes, strategies and value. The objectives of the study are: to detect the different enablers that activate innovation in smart service systems; and to explore how these can lead dynamically to the emergence of different innovation patterns.

The empirical research adopts an approach based on constructivist grounded theory, performed through observation and semi-structured interviews to investigate the development of innovation in the Italian CTNA (Italian acronym of National Cluster for Aerospace Technology).

The identification and re-elaboration of the novelties that emerged from the analysis of the Cluster allow the elaboration of a diagram that classifies five different shades of innovation, introduced through some related theoretical propositions: technological; process; business model and data-driven; social and eco-sustainable; and practice-based.

The paper embraces a synthesis view that detects the enabling structural and systems dimensions for innovation (the “what”) and the way in which these can be combined to create new technologies, resources, values and social rules (the “how” dimension). The classification of five different kinds of innovation can contribute to enrich extant research on value co-creation and innovation and can shed light on how given technologies and relational strategies can produce varied innovation outcomes according to the diverse stakeholders engaged.

Military technology is traditionally shrouded in secrecy. Even joint research between allies can be a marriage of convenience. But with the end of the Cold War and greater European integration, the technological landscape is changing, and a closer interface is emerging between military and civilian technologies. A worldwide stagnation in defence spending is accelerating the take‐up of commercial off‐the‐shelf technologies, while in the aerospace sector, the factors of safety and the environment are becoming at least as important as cost.

This article surveys the literature dealing with theory and applications of life cycle costing (LCC). It deals with the literature published in the last 25 years and provides 667 references.

Fluids management may be defined as the routeing and confinement of fluids, often under extremes of temperature, pressure and working environment. One of the most critical areas of this technology is the supply and transfer of liquids in aerospace fuel systems. Development of fluids management components for aerospace applications is driven by the requirement for total system integrity within the constraints of cost, space, mass, service conditions and material properties. Designers are challenged to produce novel solutions involving 3D simulation and modelling, finite element analysis and rapid prototyping. Simultaneous engineering is now an integral part of the process and designers must be aware of the latest manufacturing techniques and materials, both metallic and non‐metallic. Final design optimization is confirmed by prototype evaluation, followed by rigorous qualification testing. Explores design concepts and introduces some fluids management components in widespread use today. Reviews recent helicopter and non‐metallic material developments and discusses the future of the technology.

The purpose of this paper is to discuss the methodology in building an integrated domain information system with illustrations that provide proof of concept

The present work studies the usual search engine approach to information and its pitfalls. A methodology was adopted for construction of a domain‐based information system, known as Aerospace Information System (AERIS), comprising six distinct steps in identifying and sourcing, evaluating and then technically integrating resources into the information system. AERIS is an integrated gateway for resources in the domain of aerospace science and technology. AERIS is designed to provide information from varied sources such as formal publications (e.g. articles), aggregators (e.g. harvesters) and also informal resources such as blogs and discussion fora. Interaction is provided through a simple user interface.

The domain‐based information system with focussed collection and services serves patrons with more precision than general web search engines.

At present the AERIS system is populated with a limited number of resources. A fully‐fledged system may be developed based on the same model.

This original research work provides a model for a comprehensive integrated gateway to domain‐based information using open‐source tools.

Two high‐powered satellites built by Hughes Space and Communications Company (HSC) will bring true direct broadcast satellite (DBS) service to homes throughout North America starting in early 1994.

The purpose of this paper is to evaluate the health‐states of unit under test (UUT) in aerospace systems by means of unreliable test outcomes, and the evaluation results can provide a guide for engineers to carry out proper maintenance prior to total failure.

In this paper, the authors formulate the health‐state evaluation (HSE) problem with unreliable test outcomes based on Bayes rule, and develop the Lagrangian relaxation and adaptive genetic algorithm (LRAGA) to solve it. The solution scheme can be viewed as a two‐level coordinated solution framework for the HSE problem. At the top level, the Lagrange multipliers are updated by using AGA. At the bottom level, each of the sub‐problems is solved by using AGA.

The experimental results show that the HSE model appears promising and the LRAGA can obtain the higher quality solution and converge to it at a faster rate than conventional methods (i.e. Lagrangian relaxation (LR), genetic algorithm (GA), simulated annealing (SA) and Lagrangian relaxation and genetic algorithm (LRGA).

The proposed method for the HSE problem of large‐scale systems which include thousands of faults and tests needs to be verified further.

The HSE results for aerospace systems can help engineers to carry out a schedule for prompt maintenance prior to UUTs' failure, to avoid the consequences of total failure. It is important to improve aerospace systems' safety, reliability, maintainability, affordability, and reduce life cycle cost.

This paper constructs the HSE model with unreliable test outcomes based on the Bayes rule and proposes a method based on LRAGA to solve the HSE problem.