@InProceedings{FrancoSant:2016:SYReMo,
author = "Franco, Ricardo and Santos, Walter Abrah{\~a}o dos",
affiliation = "{Instituto Nacional de Pesquisas Espaciais (INPE)} and {Instituto
Nacional de Pesquisas Espaciais (INPE)}",
title = "A SYSML reference model to satellite/launcher interface and its
instantiation to a CUBESAT project",
year = "2016",
organization = "Latin American IAA CubeSat Workshop, 2.",
abstract = "Every satellite project needs to take into account all the
concerns im-posed to its interface to a real launcher vehicle, as
it is the main inter-face of the satellite to the outer world
during its launch lifecycle phase. This interface generates
constraints that the satellite needs to comply. In this work a
Model-Based Systems Engineering (MBSE) approach is tak-en to
define a reference model to this interface which is later on
instan-tiated to a CubeSat mission as a case study. MBSE is an
emerging tech-nology that provides many advantages to the
classical and document-oriented Systems Engineering (SE) process.
One advantage to this ap-proach is solving the integration problem
that each one of the individual systems domain disciplines have in
the variety of their own well-established modelling methods and
tools to support design, analysis, verification and validation.
Since these disciplines are not, a priori, well connected, data
exchange and sharing may become cumbersome. This is where MBSE
comes into place as it primarily models the whole system from a
holistic problem point-of-view. MBSE can support tools for early
system verification and validation and can provide means to
simulate and execute many parts or the whole system. Models are
here written in SysML (Systems Modeling Language) which is a
general-purpose graph-ical modeling language for specifying,
analyzing, designing, and verify-ing complex systems that may
include hardware, software, information, personnel, procedures,
and facilities and can model systems architecture and behavior.
Finally, this paper shows how the launcher-satellite inter-face
reference model is effectively used during a launch lifecycle
Sys-tems Engineering (SE) process, how it supports many Systems
Engineering (SE) processes and how it meets the constraints
imposed to a Cu-beSat project taken as a satellite case study.",
conference-location = "Florian{\'o}polis, SC",
conference-year = "28 Feb. - 02 Mar.",
ibi = "8JMKD3MGP3W34P/3L9KR22",
url = "http://urlib.net/ibi/8JMKD3MGP3W34P/3L9KR22",
targetfile = "Franco.pdf",
urlaccessdate = "27 abr. 2024"
}