Aplication of feedforward and recurrent neural networks for flapping and torsion identification of a helicopter blade (2003)
- Authors:
- USP affiliated authors: BELO, EDUARDO MORGADO - EESC ; MARQUES, FLAVIO DONIZETI - EESC
- Unidade: EESC
- Subjects: REDES NEURAIS; HELICÓPTEROS
- Language: Inglês
- Imprenta:
- ISBN: 8585769149
- Source:
- Título do periódico: Proceedings : COBEM 2003
- Conference titles: International Congress of Mechanical Engineering
-
ABNT
SOUZA, Luciane de Fátima Rodrigues de et al. Aplication of feedforward and recurrent neural networks for flapping and torsion identification of a helicopter blade. 2003, Anais.. São Paulo: ABCM, 2003. . Acesso em: 01 out. 2024. -
APA
Souza, L. de F. R. de, Rebolho, D. C., Caporali, A. S., Belo, E. M., & Marques, F. D. (2003). Aplication of feedforward and recurrent neural networks for flapping and torsion identification of a helicopter blade. In Proceedings : COBEM 2003. São Paulo: ABCM. -
NLM
Souza L de FR de, Rebolho DC, Caporali AS, Belo EM, Marques FD. Aplication of feedforward and recurrent neural networks for flapping and torsion identification of a helicopter blade. Proceedings : COBEM 2003. 2003 ;[citado 2024 out. 01 ] -
Vancouver
Souza L de FR de, Rebolho DC, Caporali AS, Belo EM, Marques FD. Aplication of feedforward and recurrent neural networks for flapping and torsion identification of a helicopter blade. Proceedings : COBEM 2003. 2003 ;[citado 2024 out. 01 ] - Um controlador baseado em lógica difusa para a supressão de Flutter
- Projeto de um controlador para supressão de flutter
- Simulation and identification of a flight envelope using neural networks
- Previsão da velocidade de flutter utilizando redes neurais
- Aeroelastic functional approximation via an artificial neural network reduced-order model
- Redes neurais artificiais recorrentes na identificação de resposta de diferentes manobras de uma aeronave regional
- Aeroelastic functional approximation via an artificial neural network reduced-order model
- Numerical model for aeroelastic analysis in time domain
- Aeroelastic response neural model using the Levenberg-Marquardt algorithm
- Numerical model for the simulation of fixed wings aeroelastic response
How to cite
A citação é gerada automaticamente e pode não estar totalmente de acordo com as normas