@InProceedings{SilvaJrLour:2011:InDeSp,
               author = "Silva Jr, Adalberto Coelho da and Loureiro, Geilson",
          affiliation = "{Instituto Nacional de Pesquisas Espaciais (INPE)} and {Instituto 
                         Nacional de Pesquisas Espaciais (INPE)}",
                title = "Integrated Development of Space Systems - Design for AIT - Design 
                         for assembly, integration and testing of satellites - D4AIT",
            booktitle = "Proceedings...",
                 year = "2011",
         organization = "2011. IEEE International Conference on Industrial Engineering and 
                         Engineering Management",
            publisher = "IEEE",
                 note = "{Setores de Atividade: Pesquisa e desenvolvimento 
                         cient{\'{\i}}fico.}",
             keywords = "Montagem, Integra{\c{c}}{\~a}o e Testes.",
             abstract = "The Satellite Assembly, Integration and Testing (AIT) activities 
                         are a logical and interrelated sequence of events. The main 
                         objective in this phase of a space program development is to 
                         achieve a high degree of confidence that the satellite complies 
                         with its specified performance parameters. Traditional 
                         simultaneous engineering space systems (e.g. satellite) 
                         development can have a better approach for taking into 
                         consideration AIT requirements during the initial phases of 
                         satellite conception and project detailing. By combining model 
                         driven system design approach with simultaneous engineering 
                         concepts for process modeling, AIT requirements at system level 
                         can be dealt with during satellite conceptual and detailed design. 
                         AIT requirements comprise electrical, mechanical and environmental 
                         requirements. This paper aims to present a new process for the 
                         development of satellites, that includes - electrical, mechanical 
                         and environmental requirements of assembly, integration and 
                         testing (AIT) of satellites, at the system level, already at the 
                         design stage of the satellite project.",
  conference-location = "Singapore Piscataway",
      conference-year = "2011",
                label = "lattes: 1016652214853378 1 SilvaJrLour:2011:InDeSp",
             language = "en",
           targetfile = "silva_integrated.pdf",
        urlaccessdate = "20 maio 2024"
}