Aeroelastic functional approximation via an artificial neural network reduced-order model (2003)
- Authors:
- USP affiliated authors: MARQUES, FLAVIO DONIZETI - EESC ; BELO, EDUARDO MORGADO - EESC
- Unidade: EESC
- Subjects: AEROELASTICIDADE DE AERONAVES; REDES NEURAIS
- Language: Inglês
- Imprenta:
- Source:
- Título: Proceedings of COBEM
- Conference titles: International Congress of Mechanical Engineering
-
ABNT
FERREIRA, Ana Paula Carvalho da Silva e MARQUES, Flavio Donizeti e BELO, Eduardo Morgado. Aeroelastic functional approximation via an artificial neural network reduced-order model. 2003, Anais.. São Paulo: ABCM, 2003. . Acesso em: 03 jan. 2026. -
APA
Ferreira, A. P. C. da S., Marques, F. D., & Belo, E. M. (2003). Aeroelastic functional approximation via an artificial neural network reduced-order model. In Proceedings of COBEM. São Paulo: ABCM. -
NLM
Ferreira APC da S, Marques FD, Belo EM. Aeroelastic functional approximation via an artificial neural network reduced-order model. Proceedings of COBEM. 2003 ;[citado 2026 jan. 03 ] -
Vancouver
Ferreira APC da S, Marques FD, Belo EM. Aeroelastic functional approximation via an artificial neural network reduced-order model. Proceedings of COBEM. 2003 ;[citado 2026 jan. 03 ] - Redes neurais artificiais recorrentes na identificação de resposta de diferentes manobras de uma aeronave regional
- Aplication of feedforward and recurrent neural networks for flapping and torsion identification of a helicopter blade
- Simulation and identification of a flight envelope using neural networks
- Projeto de um controlador para supressão de flutter
- Um controlador baseado em lógica difusa para a supressão de Flutter
- Previsão da velocidade de flutter utilizando redes neurais
- Aplication of feedforward and recurrent neural networks for flapping and torsion identification of a helicopter blade
- Aeroelastic response neural model using the Levenberg-Marquardt algorithm
- Application of time-delay neural and recurrent neural networks for the identification of a hingeless helicopter blade flapping and torsion motions
- Numerical model for the simulation of fixed wings aeroelastic response
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