Zobrazeno 1 - 4
of 4
pro vyhledávání: '"L. C. G. De Souza"'
Autor:
L. C. G. de Souza, M. A. Drumond
Publikováno v:
International Journal of Environmental Science and Technology. 19:12679-12700
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::071e0694641e7b5a4a64215d86896d26
https://doi.org/10.1007/s13762-022-04504-1
https://doi.org/10.1007/s13762-022-04504-1
Publikováno v:
Aerospace Science and Technology. 29:403-412
This paper is devoted to the attitude and vibration control of spacecraft containing flexible appendages. It entails an investigation of a passive control strategy which consists in connecting piezoelectric transducers bonded to the flexible elements
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::a6893d7ac373b6881cd6ee2bf18f8e1c
https://doi.org/10.1016/j.ast.2013.05.001
https://doi.org/10.1016/j.ast.2013.05.001
Autor:
F. O. Ramos, L. C. G. De Souza
Publikováno v:
Journal of Aerospace Engineering, Sciences and Applications. 2:47-52
This work presents the embedding of Computational Intelligence (CI) mechanisms in well-known techniques available for control system design, applied to satellite attitude control by using a reaction wheel. It is shown that effective search and scorin
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::214abc7c79e55ad8bdc835489ebea500
https://doi.org/10.7446/jaesa.0201.05
https://doi.org/10.7446/jaesa.0201.05
Autor:
A G de Souza, L C G de Souza
Publikováno v:
Journal of Physics: Conference Series. 641:012030
The satellite attitude control system (ACS) design becomes more complex when the satellite structure has components like, flexible solar panels, antennas and mechanical manipulators. These flexible structures can interact with the satellite rigid par
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::ebd73feadf0d2941b83eff91db75ef8e
https://doi.org/10.1088/1742-6596/641/1/012030
https://doi.org/10.1088/1742-6596/641/1/012030