@MastersThesis{Cardieri:1986:MeMaAe,
author = "Cardieri, Luiz Victor Carone",
title = "Mesa com mancais aerost{\'a}ticos para simula{\c{c}}{\~a}o em
um grau de liberdade de sistemas de controle de atitude de
sat{\'e}lites artificiais",
school = "Instituto Nacional de Pesquisas Espaciais (INPE)",
year = "1986",
address = "S{\~a}o Jos{\'e} dos Campos",
month = "1986-06-27",
keywords = "mancais aerostaticos, sistema de controle de atitude,
simula{\c{c}}{\~a}o din{\^a}mica, satellite attitude control,
simulators, equipment simulation.",
abstract = "Para simula{\c{c}}{\~a}o din{\^a}mica completa em um grau de
liberdade Sistemas de Controle de Atitude de sat{\'e}lites
artificiais, utiliza-se uma plataforma que permite girar com
precis{\~a}o tal sistema, sujeitando-o a baixos torques
perturbadores (da ordem de 10-4 N.m), compar{\'a}veis com aqueles
aos quais o sat{\'e}lite estar{\'a} submetido quando em
{\'o}rbita. Esta caracter{\'{\i}}stica pode ser atingida com o
uso de mancais aerost{\'a}ticos com boa estabilidade
din{\^a}mica. Este trabalho apresenta o projeto e a
constru{\c{c}}{\~a}o desta mesa de simula{\c{c}}{\~a}o, com
{\^e}nfase na modelagem e no dimensionamento dos mancais para
m{\'{\i}}nima perturba{\c{c}}{\~a}o. S{\~a}o, tamb{\'e}m,
levantadas experimentalmente algumas caracter{\'{\i}}sticas da
mesa (capacidade de carga, rigidez axial, precis{\~a}o de giro e
torque perturbador) e escolhida a instrumenta{\c{c}}{\~a}o
necess{\'a}ria para proceder a simula{\c{c}}{\~a}o de modo
aut{\^o}nomo, a saber, sistema de medida de posi{\c{c}}{\~a}o e
velocidade angular, suprimento de energia e esta{\c{c}}{\~a}o de
transmiss{\~a}o e recebimento de dados. ABSTRACT: For a dynamic
simulation in one degree of freedon of complete Attitude Control
Systems of artificial satellites, one utilizes a platform which
allows to rotate this system with high accuracy, subjecting it to
low disturbance torques (in the arder of 10-4 N.m), comparable to
the ones to which the satellite will be submitted when in orbit.
This characteristic can be reached with the use of aerostatic
bearings with good dynamic stability. This work presents the
design and construction of this simulation table, with emphasis on
modelling and dimensioning of the bearings for minimal
disturbance. In addition, some characteristics of the table are
experimentally verified (load capacity, axial stiffness, axis
accuracy and disturbance torque) and the necessary instrumentation
is chosen in order to proceed with the autonomous simulation, that
is, angular position and velocity measurement system, power
supply, and data transmission and receiving station.",
committee = "Rios Neto, Atair (presidente) and Chien, Ching-tu Carlos
(orientador) and Fleury, Agenor de Toledo (orientador) and Alves,
Valter Francisco Arruda and Purquerio, Benedito de Moraes",
copyholder = "SID/SCD",
englishtitle = "Table with aerostatic bearings for simulation in one degree of
freedom of Attitude Control Systems of artificial satellites",
label = "5653",
language = "pt",
pages = "155",
ibi = "6qtX3pFwXQZ3r59YCT/GTcpC",
url = "http://urlib.net/ibi/6qtX3pFwXQZ3r59YCT/GTcpC",
targetfile = "publicacao.pdf",
urlaccessdate = "16 jun. 2024"
}