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		<reportnumber>INPE-14198-RPQ/260</reportnumber>
		<citationkey>MilaniSilv:2006:SiTeRe</citationkey>
		<title>Simulação em tempo real do comportamento dinâmico da plataforma suborbital 1 durante período de Estabilização</title>
		<year>2006</year>
		<type>RPQ</type>
		<numberofpages>19</numberofpages>
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		<author>Milani, Paulo Giácomo,</author>
		<author>Silva, Suely,</author>
		<group>DMC-INPE-MCT-BR</group>
		<affiliation>Instituto Nacional de Pesquisas Espaciais (INPE)</affiliation>
		<affiliation>Instituto Nacional de Pesquisas Espaciais (INPE)</affiliation>
		<electronicmailaddress>milani@dem.inpe.br</electronicmailaddress>
		<institution>Instituto Nacional de Pesquisas Espaciais</institution>
		<city>São José dos Campos</city>
		<transferableflag>1</transferableflag>
		<keywords>simulação de sistemas, plataforma suborbital, controle automática.</keywords>
		<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.</abstract>
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