@InProceedings{HassmannFeli:2007:AtViCo,
author = "Hassmann, Carlos Henrique Gustavo and Felini, Andr{\'e}",
affiliation = "{Instituto Nacional de Pesquisas Espaciais (INPE)} and {Instituto
Nacional de Pesquisas Espaciais (INPE)}",
title = "Attitude and vibration control of a satellite with a flexible
solar panel using LQR tracking with infinite time",
booktitle = "Anais...",
year = "2007",
organization = "International Congress of Mechanical Engineering, 19. (COBEM).",
keywords = "attitude control, vibration control, flexible structures, LQR
satellites.",
abstract = "The objective of this work is to investigate the control of the
attitude angles and the suppression of the vibration of the solar
panel of a satellite in circular orbit around Earth. It is
considered only the maneuver of the satellite around is center of
mass. The mathematical model for the complete system is derived
using the lagrangean formalism. The control law considered is the
LQR with infinite time (algebraic Ricatti equation) and the states
are controlled in order to stay as close as possible of a specific
set of reference states (tracking problem). The optimal gains are
obtained considering only the linear part of the governing
equations. The gains obtained in this way are then used to control
the complete nonlinear model. Since LQR is a linear controller
(and besides its robustness), one does not consider have great
velocities and deflections which can transform the nonlinear
mathematical model into a strongly nonlinear are.",
conference-location = "Bras{\'{\i}}lia, DF",
conference-year = "5-9 Nov.",
targetfile = "Comut 29358.pdf",
urlaccessdate = "27 jun. 2024"
}