@TechReport{MilaniSilv:2006:SiTeRe,
               author = "Milani, Paulo Gi{\'a}como and Silva, Suely",
                title = "Simula{\c{c}}{\~a}o em tempo real do comportamento din{\^a}mico 
                         da plataforma suborbital 1 durante per{\'{\i}}odo de 
                         Estabiliza{\c{c}}{\~a}o",
          institution = "Instituto Nacional de Pesquisas Espaciais",
                 year = "2006",
                 type = "RPQ",
               number = "INPE-14198-RPQ/260",
              address = "S{\~a}o Jos{\'e} dos Campos",
             keywords = "simula{\c{c}}{\~a}o de sistemas, plataforma suborbital, controle 
                         autom{\'a}tica.",
             abstract = "The suborbital platforms launch program, besides providing stand 
                         to experiment devices that will be used in satellites beeing 
                         developed within the Brazilian Spacial Program, has the objective 
                         to offer to scientific community an available microgravity 
                         enviroment to be used in experiments of interest to National 
                         Industry. Aiming to visualize and analyze the platform's behavior 
                         after its separation from the launch vehicle, a software was 
                         designed to simulate in real time the platform's motions and 
                         commands a three axis simulator to follow the velocities attained 
                         from the simulation. The software, written in C language, was 
                         developed to be executed in Linux Systems and gets access to the 
                         simulator using a package of routines designed to control it. The 
                         integration of the suborbital platform's dynamic equations is 
                         accomplished applying a 4th order Runge Kutta algorithm. 
                         Simulation results are evaluated through the analysis of graphics 
                         that show the velocities and control torques applied in the three 
                         axix.",
          affiliation = "{Instituto Nacional de Pesquisas Espaciais (INPE)} and {Instituto 
                         Nacional de Pesquisas Espaciais (INPE)}",
           copyholder = "SID/SCD",
             language = "pt",
                pages = "19",
                  ibi = "6qtX3pFwXQZGivnK2Y/SsfPU",
                  url = "http://urlib.net/ibi/6qtX3pFwXQZGivnK2Y/SsfPU",
        urlaccessdate = "03 maio 2024"
}