@InProceedings{JulioFoCoViCaLoTrMe:2014:CoSyEn,
               author = "Julio Filho, Antonio Cassiano and Corr{\^e}a Junior, Fl{\'a}vio 
                         Azevedo and Vieira, Fernando Putarov and Catarino, Luis Carlos and 
                         Loureiro, Geilson and Trentim, M{\'a}rio Henrique and Mendes, 
                         Wagner Schalch",
          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 {Instituto Nacional de Pesquisas Espaciais 
                         (INPE)} and {Institute of Aeronautics and Space (IAE)} and {Alstom 
                         Brazil Energy and Transport}",
                title = "Concurrent Systems Engineering of a CubeSat System",
            booktitle = "Proceedings...",
                 year = "2014",
         organization = "Global Space Applications Conference.",
             abstract = "The paper presents a method combining traditional systems 
                         engineering with the concepts of the concurrent systems 
                         engineering to develop a CubeSat system in a case study. The 
                         method consists of Mission Definition, Lifecycle Processes 
                         Analysis, Stakeholder Analysis, Stakeholder Requirements, 
                         Functional Analysis, Architecture Design and Detailed Design. The 
                         approach was exemplified by modeling requirements, functions and 
                         implementation elements, simultaneously, for the CubeSat product 
                         and for the organizations that implement the CubeSat life cycle 
                         processes. With the increase of complexity of systems, traditional 
                         systems engineering methods are failing to anticipate all 
                         requirements needed to secure a solution that satisfies the 
                         stakeholders' needs. The concurrent systems engineering is a 
                         multidisciplinary and collaborative approach to derive, evolve and 
                         verify a system solution, composed of products and the 
                         organization implementing the products' life cycle processes, 
                         balanced throughout the system's life cycle to satisfy 
                         stakeholders' needs and get public acceptance and the products and 
                         the organization composing the system solution for the CubeSat 
                         system will be developed concurrently. Picosatellites class, by 
                         definition, are extremely small, lightweight satellites, the 
                         progenitor of the pico class is the CubeSat, an open source 
                         satellite architecture for space research that usually has a 
                         volume of exactly one liter and typically uses commercial 
                         off-the-shelf electronics components. Those miniaturized 
                         satellites have as core components: an antenna, a radio 
                         transmitter for up-linking commands and down-linking data, an 
                         onboard computer, an electric power system, and payloads. The 
                         CubeSat specification accomplishes several high-level goals. 
                         Simplification of the satellite's infrastructure makes it possible 
                         to design and produce a workable satellite at low cost.",
  conference-location = "Paris, Fran{\c{c}}a",
      conference-year = "jun. 2-4, 2014",
                label = "self-archiving-INPE-MCTI-GOV-BR",
             language = "en",
           targetfile = ".htaccess",
        urlaccessdate = "26 abr. 2024"
}