Control of an Aerospace Launcher
Author(s) -
Nabila Zbiri,
Zohra Z. Manseur,
Lotfi Béji,
Samir Otmane,
Azgal Abichou
Publication year - 2009
Publication title -
aip conference proceedings
Language(s) - English
Resource type - Conference proceedings
SCImago Journal Rank - 0.177
H-Index - 75
eISSN - 1551-7616
pISSN - 0094-243X
DOI - 10.1063/1.3106507
Subject(s) - aerospace , linear quadratic gaussian control , attitude control , control (management) , aeronautics , computer science , control system , space (punctuation) , aerospace engineering , control engineering , systems engineering , engineering , control theory (sociology) , artificial intelligence , electrical engineering , operating system
International audienceThis research is within the framework of the PERSEUS project proposed by the CNES (Centre National d'Etudes Spatiales). Its aim is to develop new concepts for the attitude control of space modules. This article presents a first study as well as the results of a robust LQG control system that allows stable and satisfactory performance for the attitude of a rigid launcher
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