A Multidisciplinary Design Optimization Tool for Spacecraft Equipment Layout Conception
Autor(a) principal: | |
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Data de Publicação: | 2014 |
Outros Autores: | , , , , , |
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. |
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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 |
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1754732531196887040 |