A Multidisciplinary Design Optimization Tool for Spacecraft Equipment Layout Conception

Detalhes bibliográficos
Autor(a) principal: Lau,Valentino
Data de Publicação: 2014
Outros Autores: Sousa,Fabiano Luis de, Galski,Roberto Luiz, Rocco,Evandro Marconi, Becceneri,José Carlos, Santos,Walter Abrahão dos, Sandri,Sandra Aparecida
Tipo de documento: Artigo
Idioma: eng
Título da fonte: Journal of Aerospace Technology and Management (Online)
Texto Completo: http://old.scielo.br/scielo.php?script=sci_arttext&pid=S2175-91462014000400431
Resumo: ABSTRACT: One issue the design team has to face in the process of building a new spacecraft, is to define its mechanical and electrical architecture. The choice of where to place the spacecraft´s electronic equipment is a complex task, since it involves simultaneously many factors, such as the spacecraft's required position of center of mass, moments of inertia, equipment heat dissipation, integration and servicing issues, among others. Since this is a multidisciplinary task, the early positioning of the spacecraft´s equipment is usually done "manually" by a group of system engineers, heavily based on their experience. It is an interactive process that takes time and hence, as soon as a feasible design is found, it becomes the baseline. This precludes a broader exploration of the design space, which may lead to a suboptimal solution, or worse to a design that will have to be modified later. Recently, it has been shown the potential benefits of automating the process of spacecraft´s equipment layout using optimization techniques. In this paper, a prototype of an Excel® based tool for multidisciplinary spacecraft equipment layout conception is described. Provided the geometric dimensions, mass and heat dissipation of the equipment, and the available positioning area, the tool can automatically generate many possible trade-off solutions for the layout. It allows the user to set specific equipment to specific areas of positioning, and different combinations of objective functions can be used to drive the design. The features of the tool are shown in a simplified three dimensional problem.
id DCTA-1_2951421dbc4b05a7f8ab286d96610c2b
oai_identifier_str oai:scielo:S2175-91462014000400431
network_acronym_str DCTA-1
network_name_str Journal of Aerospace Technology and Management (Online)
repository_id_str
spelling A Multidisciplinary Design Optimization Tool for Spacecraft Equipment Layout ConceptionLayout optimizationSpacecraftConceptual designElectronic equipmentABSTRACT: One issue the design team has to face in the process of building a new spacecraft, is to define its mechanical and electrical architecture. The choice of where to place the spacecraft´s electronic equipment is a complex task, since it involves simultaneously many factors, such as the spacecraft's required position of center of mass, moments of inertia, equipment heat dissipation, integration and servicing issues, among others. Since this is a multidisciplinary task, the early positioning of the spacecraft´s equipment is usually done "manually" by a group of system engineers, heavily based on their experience. It is an interactive process that takes time and hence, as soon as a feasible design is found, it becomes the baseline. This precludes a broader exploration of the design space, which may lead to a suboptimal solution, or worse to a design that will have to be modified later. Recently, it has been shown the potential benefits of automating the process of spacecraft´s equipment layout using optimization techniques. In this paper, a prototype of an Excel® based tool for multidisciplinary spacecraft equipment layout conception is described. Provided the geometric dimensions, mass and heat dissipation of the equipment, and the available positioning area, the tool can automatically generate many possible trade-off solutions for the layout. It allows the user to set specific equipment to specific areas of positioning, and different combinations of objective functions can be used to drive the design. The features of the tool are shown in a simplified three dimensional problem.Departamento de Ciência e Tecnologia Aeroespacial2014-12-01info:eu-repo/semantics/articleinfo:eu-repo/semantics/publishedVersiontext/htmlhttp://old.scielo.br/scielo.php?script=sci_arttext&pid=S2175-91462014000400431Journal of Aerospace Technology and Management v.6 n.4 2014reponame:Journal of Aerospace Technology and Management (Online)instname:Departamento de Ciência e Tecnologia Aeroespacial (DCTA)instacron:DCTA10.5028/jatm.v6i4.399info:eu-repo/semantics/openAccessLau,ValentinoSousa,Fabiano Luis deGalski,Roberto LuizRocco,Evandro MarconiBecceneri,José CarlosSantos,Walter Abrahão dosSandri,Sandra Aparecidaeng2017-05-26T00:00:00Zoai:scielo:S2175-91462014000400431Revistahttp://www.jatm.com.br/ONGhttps://old.scielo.br/oai/scielo-oai.php||secretary@jatm.com.br2175-91461984-9648opendoar:2017-05-26T00:00Journal of Aerospace Technology and Management (Online) - Departamento de Ciência e Tecnologia Aeroespacial (DCTA)false
dc.title.none.fl_str_mv A Multidisciplinary Design Optimization Tool for Spacecraft Equipment Layout Conception
title A Multidisciplinary Design Optimization Tool for Spacecraft Equipment Layout Conception
spellingShingle A Multidisciplinary Design Optimization Tool for Spacecraft Equipment Layout Conception
Lau,Valentino
Layout optimization
Spacecraft
Conceptual design
Electronic equipment
title_short A Multidisciplinary Design Optimization Tool for Spacecraft Equipment Layout Conception
title_full A Multidisciplinary Design Optimization Tool for Spacecraft Equipment Layout Conception
title_fullStr A Multidisciplinary Design Optimization Tool for Spacecraft Equipment Layout Conception
title_full_unstemmed A Multidisciplinary Design Optimization Tool for Spacecraft Equipment Layout Conception
title_sort A Multidisciplinary Design Optimization Tool for Spacecraft Equipment Layout Conception
author Lau,Valentino
author_facet Lau,Valentino
Sousa,Fabiano Luis de
Galski,Roberto Luiz
Rocco,Evandro Marconi
Becceneri,José Carlos
Santos,Walter Abrahão dos
Sandri,Sandra Aparecida
author_role author
author2 Sousa,Fabiano Luis de
Galski,Roberto Luiz
Rocco,Evandro Marconi
Becceneri,José Carlos
Santos,Walter Abrahão dos
Sandri,Sandra Aparecida
author2_role author
author
author
author
author
author
dc.contributor.author.fl_str_mv Lau,Valentino
Sousa,Fabiano Luis de
Galski,Roberto Luiz
Rocco,Evandro Marconi
Becceneri,José Carlos
Santos,Walter Abrahão dos
Sandri,Sandra Aparecida
dc.subject.por.fl_str_mv Layout optimization
Spacecraft
Conceptual design
Electronic equipment
topic Layout optimization
Spacecraft
Conceptual design
Electronic equipment
description ABSTRACT: One issue the design team has to face in the process of building a new spacecraft, is to define its mechanical and electrical architecture. The choice of where to place the spacecraft´s electronic equipment is a complex task, since it involves simultaneously many factors, such as the spacecraft's required position of center of mass, moments of inertia, equipment heat dissipation, integration and servicing issues, among others. Since this is a multidisciplinary task, the early positioning of the spacecraft´s equipment is usually done "manually" by a group of system engineers, heavily based on their experience. It is an interactive process that takes time and hence, as soon as a feasible design is found, it becomes the baseline. This precludes a broader exploration of the design space, which may lead to a suboptimal solution, or worse to a design that will have to be modified later. Recently, it has been shown the potential benefits of automating the process of spacecraft´s equipment layout using optimization techniques. In this paper, a prototype of an Excel® based tool for multidisciplinary spacecraft equipment layout conception is described. Provided the geometric dimensions, mass and heat dissipation of the equipment, and the available positioning area, the tool can automatically generate many possible trade-off solutions for the layout. It allows the user to set specific equipment to specific areas of positioning, and different combinations of objective functions can be used to drive the design. The features of the tool are shown in a simplified three dimensional problem.
publishDate 2014
dc.date.none.fl_str_mv 2014-12-01
dc.type.driver.fl_str_mv info:eu-repo/semantics/article
dc.type.status.fl_str_mv info:eu-repo/semantics/publishedVersion
format article
status_str publishedVersion
dc.identifier.uri.fl_str_mv http://old.scielo.br/scielo.php?script=sci_arttext&pid=S2175-91462014000400431
url http://old.scielo.br/scielo.php?script=sci_arttext&pid=S2175-91462014000400431
dc.language.iso.fl_str_mv eng
language eng
dc.relation.none.fl_str_mv 10.5028/jatm.v6i4.399
dc.rights.driver.fl_str_mv info:eu-repo/semantics/openAccess
eu_rights_str_mv openAccess
dc.format.none.fl_str_mv text/html
dc.publisher.none.fl_str_mv Departamento de Ciência e Tecnologia Aeroespacial
publisher.none.fl_str_mv Departamento de Ciência e Tecnologia Aeroespacial
dc.source.none.fl_str_mv Journal of Aerospace Technology and Management v.6 n.4 2014
reponame:Journal of Aerospace Technology and Management (Online)
instname:Departamento de Ciência e Tecnologia Aeroespacial (DCTA)
instacron:DCTA
instname_str Departamento de Ciência e Tecnologia Aeroespacial (DCTA)
instacron_str DCTA
institution DCTA
reponame_str Journal of Aerospace Technology and Management (Online)
collection Journal of Aerospace Technology and Management (Online)
repository.name.fl_str_mv Journal of Aerospace Technology and Management (Online) - Departamento de Ciência e Tecnologia Aeroespacial (DCTA)
repository.mail.fl_str_mv ||secretary@jatm.com.br
_version_ 1754732531196887040