Add to ORKGAbstract. This paper deals with the problem of 3-axis attitude stabilization of a satellite subjected to dynamics perturbations. The controller is based on the Linear Quadratic Gaussian control theory (LQG). The main purpose of the work is to synthesize a control law characterized by simplicity on implementation. The study considers the specific case of the Brazilian satellite PMM. The article presents the system modelling, the proposed control, and analysis of simulation results
This paper deals with three-axis stabilization of a gravity gradient low earth orbit satellite. The ...
International audienceThis study is dedicated to the problem of non linear attitude control for a ri...
The increasing interest of private companies in the aerospace sector has produced a growth of space ...
Abstract. In this paper are investigated multivariable control methods for attitude control of an ar...
This paper investigates a new strategy for geostationary satellite attitude control using Linear Qua...
This work deals with the analysis and design of a reaction thruster attitude control for the Brazili...
Abstract—In this article, design and analysis of an optimal orbit control for a communication satell...
This paper analyses the problem of the autonomous control of a satellite in Low Earth Orbit (LEO) us...
In this thesis, application of linear control methods to control the attitude of a Low-Earth Orbit s...
Different attitude control strategies of a small satellite are presented in this paper as well as th...
Attitude control and stabilization of a micro-satellite is a nontrivial problem due to the highly no...
In this paper two nonlinear control techniques are developed and compared for the satellite attitude...
The challenging problem of controlling the attitude of satellites subject to actuator failures has b...
The purpose of this paper is the design and the performance analysis of a control technique that all...
This paper analyses the problem of the autonomous control of a satellite in Low Earth Orbit (LEO) u...
This paper deals with three-axis stabilization of a gravity gradient low earth orbit satellite. The ...
International audienceThis study is dedicated to the problem of non linear attitude control for a ri...
The increasing interest of private companies in the aerospace sector has produced a growth of space ...
Abstract. In this paper are investigated multivariable control methods for attitude control of an ar...
This paper investigates a new strategy for geostationary satellite attitude control using Linear Qua...
This work deals with the analysis and design of a reaction thruster attitude control for the Brazili...
Abstract—In this article, design and analysis of an optimal orbit control for a communication satell...
This paper analyses the problem of the autonomous control of a satellite in Low Earth Orbit (LEO) us...
In this thesis, application of linear control methods to control the attitude of a Low-Earth Orbit s...
Different attitude control strategies of a small satellite are presented in this paper as well as th...
Attitude control and stabilization of a micro-satellite is a nontrivial problem due to the highly no...
In this paper two nonlinear control techniques are developed and compared for the satellite attitude...
The challenging problem of controlling the attitude of satellites subject to actuator failures has b...
The purpose of this paper is the design and the performance analysis of a control technique that all...
This paper analyses the problem of the autonomous control of a satellite in Low Earth Orbit (LEO) u...
This paper deals with three-axis stabilization of a gravity gradient low earth orbit satellite. The ...
International audienceThis study is dedicated to the problem of non linear attitude control for a ri...
The increasing interest of private companies in the aerospace sector has produced a growth of space ...