Mesa COM Mancais Aerostaticos Para Simulacao Em Um Grau de Liberdade de Sistemas de Controle de Atitude de Satelite Artificiais (Table with Aerostatic Bearings for Simulation in One Degree of Freedom Attitude Control Systems of Ar

摘要

The design is presented of a table supported by thrust and journal aerostatic bearings, which were dimensioned for simulation of the attitude movement of artificial satellites. The most important parameters for this design and the construction problems are emphasized. The air supply facility is shown along with the results of the first prototype performance tests and the instrumented platform for tests with the Attitude Control System.