portada An Algorithm for Integrated Subsystem Embodiment and System Synthesis (en Inglés)

An Algorithm for Integrated Subsystem Embodiment and System Synthesis (en Inglés)

Formato

Libro Físico

Autor

National Aeronautics and Space Administr

Kemper Lewis

Editorial

Biblioscholar

Idioma

Inglés

N° páginas

536

Encuadernación

Tapa Blanda

Dimensiones

24.6x18.9x2.7 cm

Peso

0.95 kg.

ISBN13

9781288916085

Categorías

Educación

An Algorithm for Integrated Subsystem Embodiment and System Synthesis (en Inglés)

National Aeronautics and Space Administr (Autor) · Kemper Lewis (Autor) · Biblioscholar · Tapa Blanda

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Reseña del libro "An Algorithm for Integrated Subsystem Embodiment and System Synthesis (en Inglés)"

Consider the statement, 'A system has two coupled subsystems, one of which dominates the design process. Each subsystem consists of discrete and continuous variables, and is solved using sequential analysis and solution.' To address this type of statement in the design of complex systems, three steps are required, namely, the embodiment of the statement in terms of entities on a computer, the mathematical formulation of subsystem models, and the resulting solution and system synthesis. In complex system decomposition, the subsystems are not isolated, self-supporting entities. Information such as constraints, goals, and design variables may be shared between entities. But many times in engineering problems, full communication and cooperation does not exist, information is incomplete, or one subsystem may dominate the design. Additionally, these engineering problems give rise to mathematical models involving nonlinear functions of both discrete and continuous design variables. In this dissertation an algorithm is developed to handle these types of scenarios for the domain-independent integration of subsystem embodiment, coordination, and system synthesis using constructs from Decision-Based Design, Game Theory, and Multidisciplinary Design Optimization. Implementation of the concept in this dissertation involves testing of the hypotheses using example problems and a motivating case study involving the design of a subsonic passenger aircraft