Zobrazeno 1 - 10
of 114
pro vyhledávání: '"Domingos A. Rade"'
Autor:
Valder Steffen Jr, Domingos A. Rade
Publikováno v:
Shock and Vibration, Vol 13, Iss 4-5, Pp 217-217 (2006)
Externí odkaz:
https://doaj.org/article/0f5884025939429a846d20046ae40ce5
Autor:
Domingos A. Rade, Luciano J. Pedrote dos Santos, Jose A. Pomilio, Roberto G. Annes da Silva, Carlos Henrique C. Ribeiro, Alfredo Rocha de Faria, Emilia Villani
Publikováno v:
2023 IEEE International Conference on Electrical Systems for Aircraft, Railway, Ship Propulsion and Road Vehicles & International Transportation Electrification Conference (ESARS-ITEC).
Publikováno v:
Acta Astronautica. 191:41-54
The present study addresses the problem of automatic path planning of a manipulator-like spacecraft in orbit. Based on the concept of optimal control and off-line establishment of optimal trajectories, the study proposes a formulation of multiobjecti
Publikováno v:
Journal of Control, Automation and Electrical Systems. 33:333-344
A comparative analysis of machine learning techniques for fault diagnosis of rotating machines based on images of vibration spectra is presented. The feature extraction of different types of faults, including unbalance, misalignment, shaft crack, rot
Autor:
Ana Cristina Neves Carloni, Kevin Eduardo de Conde, Aluisio Viais Pantaleão, João Luiz F. de Azevedo, Domingos Alves Rade
Publikováno v:
Journal of the Brazilian Society of Mechanical Sciences and Engineering. 44
Autor:
João Luiz F. Azevedo, Ricardo Galdino da SIlva, J Allan A. Lyrio, Domingos A. Rade, Carlos Breviglieri
Publikováno v:
AIAA AVIATION 2021 FORUM.
Autor:
Domingos A. Rade, Antônio B. Guimarães Neto, Thiago de Souza Siqueira Versiani, Gefferson C. Silva, Roberto Gil Annes da Silva, Maurício Vicente Donadon, Flavio J. Silvestre, Rafael M. Bertolin
Publikováno v:
Aerospace Science and Technology. 86:762-774
Among the aeroelastic phenomena most commonly affecting flexible and very flexible aircraft, those caused by gusts deserve special attention due to their potential either in degrading flying qualities and ride comfort or in increasing structural load
Publikováno v:
Mechanical Systems and Signal Processing. 116:900-915
In this work, viscoelastic materials are adopted for handling aeroelastic features of typical section models with three degrees-of-freedom, which present non-smooth, free-play type nonlinearities in their control surface. A rotational viscoelastic da