@InProceedings{FleurySouzCard:1987:AsCoBa,
               author = "Fleury, Agenor de Toledo and Souza, Petr{\^o}nio Noronha and 
                         Cardieri, L. Victor C.",
                title = "Aspectos construtivos de bancadas para simula{\c{c}}{\~a}o de 
                         sistemas de controle de atitude de sat{\'e}lites artificiais",
                 year = "1987",
                pages = "927--930",
         organization = "Congresso Brasileiro de Engenharia Mec{\^a}nica, 9. / Brazilian 
                         Congress of Mechanical Engineering, (COBEM).",
             keywords = "ENGENHARIA E TECNOLOGIA ESPACIAL, SPACECRAFT DESIGN, TESTING AND 
                         PERFORMANCE, bancadas para simula{\c{c}}{\~a}o, projeto 
                         eletromec{\^a}nica, Sistemas de Controle de Atitude e {\'O}rbita 
                         (SCAO), satellite attitude control, test equipment, satellite 
                         orbits, satellite orientation.",
             abstract = "Este trabalho apresenta as principais considera{\c{c}}{\~o}es 
                         relativas {\`a} constru{\c{c}}{\~a}o de duas bancadas para 
                         simula{\c{c}}{\~a}o de sistemas de Controle de Atitude e 
                         {\'O}rbita (SCAO)de sat{\'e}lites, com utiliza{\c{c}}{\~a}o de 
                         equipamentos na malha. O objetivo dessas bancadas {\'e} permitir 
                         acompanhamento r{\'a}pido em laborat{\'o}rio, das diversas fases 
                         envolvidas no projeto. Apresentam-se os projetos integrados das 
                         bancadas desenvolvidas no INPE e seus diversos componentes onde se 
                         utiliza basicamente tecnologia/nacional na fabrica{\c{c}}{\~a}o. 
                         Discutem-se os principais par{\^a}metros de desempenho desses 
                         equipamentos e resultados experimentais obtidos. ABSTRACT: This 
                         work presents the basic aspects concerning the construction of two 
                         test beds for satellite Attitude and Orbit Control Systems 
                         (AOCS)hardware-in-the-loop tests. The main goal to be reached with 
                         these test beds is the fast accomplishment of laboratory results 
                         in the various phaess of an AOCS development, from its initial 
                         conceptual definition to a prequalification phase. The central 
                         equipment of these test beds consists of a one-degree-of-freedom 
                         air bearing table and a two-degree-of-freedom servo rate table 
                         Various AOCS components such as reaction wheels, cold gas jet 
                         propulsion system, telemetry/telecommand system and celestial 
                         simulators were also developed at INPE. The designs of the test 
                         beds as integrated equipments are presented. The main performance 
                         parameters and associated experimental results are presented and 
                         discussed as well.",
  conference-location = "Florian{\'o}polis",
      conference-year = "7-11 dez. 1987",
                label = "5630",
         organisation = "ABCM",
           targetfile = "INPE-4283.pdf",
        urlaccessdate = "12 maio 2024"
}