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    Design Space Exploration for Quantifying a System Model’s Feasible Domain

    Source: Journal of Mechanical Design:;2012:;volume( 134 ):;issue: 004::page 41010
    Author:
    Brad J. Larson
    ,
    Christopher A. Mattson
    DOI: 10.1115/1.4005861
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: A major challenge in multidisciplinary system design is predicting the effects of design decisions at the point these decisions are being made. Because decisions at the beginning of system design, when the least is known about the new system, have the greatest impact on its final behavior, designers are increasingly interested in using compositional system models (system models created from independent models of system components) to validate design decisions early in and throughout system design. Compositional system models, however, have several failure modes that often result in infeasible or failed model evaluation. In addition, these models change frequently as designs are refined, changing the model domain (set of valid inputs and states). To compute valid results, the system model inputs and states must remain within this domain throughout simulation. This paper develops an algorithm to efficiently quantify the system model domain. To do this, we (1) present a formulation for system model feasibility and identify types of system model failures, (2) develop a design space exploration algorithm that quantifies the system model domain, and (3) illustrate this algorithm using a solar-powered unmanned aerial vehicle model. This algorithm enables systematic improvements of compositional system model feasibility.
    keyword(s): Design , Failure , Unmanned aerial vehicles AND Algorithms ,
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      Design Space Exploration for Quantifying a System Model’s Feasible Domain

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    http://yetl.yabesh.ir/yetl1/handle/yetl/149801
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    contributor authorBrad J. Larson
    contributor authorChristopher A. Mattson
    date accessioned2017-05-09T00:53:14Z
    date available2017-05-09T00:53:14Z
    date copyrightApril, 2012
    date issued2012
    identifier issn1050-0472
    identifier otherJMDEDB-27961#041010_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/149801
    description abstractA major challenge in multidisciplinary system design is predicting the effects of design decisions at the point these decisions are being made. Because decisions at the beginning of system design, when the least is known about the new system, have the greatest impact on its final behavior, designers are increasingly interested in using compositional system models (system models created from independent models of system components) to validate design decisions early in and throughout system design. Compositional system models, however, have several failure modes that often result in infeasible or failed model evaluation. In addition, these models change frequently as designs are refined, changing the model domain (set of valid inputs and states). To compute valid results, the system model inputs and states must remain within this domain throughout simulation. This paper develops an algorithm to efficiently quantify the system model domain. To do this, we (1) present a formulation for system model feasibility and identify types of system model failures, (2) develop a design space exploration algorithm that quantifies the system model domain, and (3) illustrate this algorithm using a solar-powered unmanned aerial vehicle model. This algorithm enables systematic improvements of compositional system model feasibility.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleDesign Space Exploration for Quantifying a System Model’s Feasible Domain
    typeJournal Paper
    journal volume134
    journal issue4
    journal titleJournal of Mechanical Design
    identifier doi10.1115/1.4005861
    journal fristpage41010
    identifier eissn1528-9001
    keywordsDesign
    keywordsFailure
    keywordsUnmanned aerial vehicles AND Algorithms
    treeJournal of Mechanical Design:;2012:;volume( 134 ):;issue: 004
    contenttypeFulltext
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    DSpace software copyright © 2002-2015  DuraSpace
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