@Article{LauSoGaRoBeSaSa:2014:MuDeOp,
author = "Lau, Valentino and Sousa, Fabiano Luis de and Galski, Roberto Luiz
and Rocco, Evandro Marconi and Becceneri, Jos{\'e} Carlos and
Santos, Walter Abrah{\~a}o dos and Sandri, Sandra Aparecida",
affiliation = "{Instituto Nacional de Pesquisas Espaciais (INPE)} and {Instituto
Nacional de Pesquisas Espaciais (INPE)} and {Instituto Nacional de
Pesquisas Espaciais (INPE)} and {Instituto Nacional de Pesquisas
Espaciais (INPE)} and {} and {Instituto Nacional de Pesquisas
Espaciais (INPE)} and {Instituto Nacional de Pesquisas Espaciais
(INPE)}",
title = "A multidisciplinary design optimization tool for spacecraft
equipment layout conception",
journal = "Journal of Aerospace Technology and Management",
year = "2014",
volume = "6",
number = "4",
pages = "431--446",
keywords = "Conceptual design, Design aids, Economic and social effects,
Electronic equipment, Equipment, Oscillators (electronic),
Spacecraft, Geometric dimensions, Layout optimization, Mechanical
and electrical, Multidisciplinary design optimization, Objective
functions, Optimization techniques, Suboptimal solution,
Three-dimensional problems, Spacecraft equipment.",
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 ExcelŽ
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.",
doi = "10.5028/jatm.v6i4.399",
url = "http://dx.doi.org/10.5028/jatm.v6i4.399",
issn = "1984-9648",
label = "scopus 2015-01 LauSoGaRoBeSaSa:2014:MuDeOp",
language = "en",
urlaccessdate = "27 abr. 2024"
}