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Trabalho de evento
Flight dynamics modeling and trim curves of a conceptual semi-tandem wing VTOL UAV (2018)
Daud Filho, Antonio Carlos; Belo, Eduardo Morgado
Source: Proceedings. Conference titles: International Congress of the Aeronautical Sciences - ICAS. Unidade: EESC
Subjects: DINÂMICA DE VOO, ENGENHARIA AERONÁUTICA
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ABNT
DAUD FILHO, Antonio Carlos e BELO, Eduardo Morgado. Flight dynamics modeling and trim curves of a conceptual semi-tandem wing VTOL UAV. 2018, Anais.. Edinburgh, UK: ICAS, 2018. Disponível em: https://repositorio.usp.br/directbitstream/987dd969-af4d-49be-a001-64ec8719b596/trabalho%2001%20-%20FLIGHT%20DYNAMICS%20MODELING%20AND%20TRIM%20CURVES%20OF%20A%20CONCEPTUAL%20SEMI-TANDEM%20WING%20VTOL%20UAV%20%2831st%20Congress%20of%20the%20International%20Council%20of%20the%20Aeronautical%20Sciences%29_removed.pdf. Acesso em: 02 nov. 2024.
APA
Daud Filho, A. C., & Belo, E. M. (2018). Flight dynamics modeling and trim curves of a conceptual semi-tandem wing VTOL UAV. In Proceedings. Edinburgh, UK: ICAS. Recuperado de https://repositorio.usp.br/directbitstream/987dd969-af4d-49be-a001-64ec8719b596/trabalho%2001%20-%20FLIGHT%20DYNAMICS%20MODELING%20AND%20TRIM%20CURVES%20OF%20A%20CONCEPTUAL%20SEMI-TANDEM%20WING%20VTOL%20UAV%20%2831st%20Congress%20of%20the%20International%20Council%20of%20the%20Aeronautical%20Sciences%29_removed.pdf
NLM
Daud Filho AC, Belo EM. Flight dynamics modeling and trim curves of a conceptual semi-tandem wing VTOL UAV [Internet]. Proceedings. 2018 ;[citado 2024 nov. 02 ] Available from: https://repositorio.usp.br/directbitstream/987dd969-af4d-49be-a001-64ec8719b596/trabalho%2001%20-%20FLIGHT%20DYNAMICS%20MODELING%20AND%20TRIM%20CURVES%20OF%20A%20CONCEPTUAL%20SEMI-TANDEM%20WING%20VTOL%20UAV%20%2831st%20Congress%20of%20the%20International%20Council%20of%20the%20Aeronautical%20Sciences%29_removed.pdf
Vancouver
Daud Filho AC, Belo EM. Flight dynamics modeling and trim curves of a conceptual semi-tandem wing VTOL UAV [Internet]. Proceedings. 2018 ;[citado 2024 nov. 02 ] Available from: https://repositorio.usp.br/directbitstream/987dd969-af4d-49be-a001-64ec8719b596/trabalho%2001%20-%20FLIGHT%20DYNAMICS%20MODELING%20AND%20TRIM%20CURVES%20OF%20A%20CONCEPTUAL%20SEMI-TANDEM%20WING%20VTOL%20UAV%20%2831st%20Congress%20of%20the%20International%20Council%20of%20the%20Aeronautical%20Sciences%29_removed.pdf
Trabalho de evento
Pio susceptibility in fly-by-wire systems (2018)
Moura, Herlandson Cardoso de; Porto Alegre, Gabriel Setim; Bidinotto, Jorge Henrique ; Belo, Eduardo Morgado
Source: Proceedings. Conference titles: International Congress of the Aeronautical Sciences - ICAS. Unidade: EESC
Subjects: PILOTAGEM DE AERONAVES, DINÂMICA DE VOO, ENGENHARIA AERONÁUTICA
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ABNT
MOURA, Herlandson Cardoso de et al. Pio susceptibility in fly-by-wire systems. 2018, Anais.. Edinburgh, UK: ICAS, 2018. Disponível em: https://repositorio.usp.br/directbitstream/41346355-4d19-4c4b-9df3-fe68c5983997/trabalho%2002%20-%20PIO%20Susceptibility%20in%20Fly-by-Wire%20Systems%20%2831st%20Congress%20of%20the%20International%20Council%20of%20the%20Aeronautical%20Sciences%29_removed.pdf. Acesso em: 02 nov. 2024.
APA
Moura, H. C. de, Porto Alegre, G. S., Bidinotto, J. H., & Belo, E. M. (2018). Pio susceptibility in fly-by-wire systems. In Proceedings. Edinburgh, UK: ICAS. Recuperado de https://repositorio.usp.br/directbitstream/41346355-4d19-4c4b-9df3-fe68c5983997/trabalho%2002%20-%20PIO%20Susceptibility%20in%20Fly-by-Wire%20Systems%20%2831st%20Congress%20of%20the%20International%20Council%20of%20the%20Aeronautical%20Sciences%29_removed.pdf
NLM
Moura HC de, Porto Alegre GS, Bidinotto JH, Belo EM. Pio susceptibility in fly-by-wire systems [Internet]. Proceedings. 2018 ;[citado 2024 nov. 02 ] Available from: https://repositorio.usp.br/directbitstream/41346355-4d19-4c4b-9df3-fe68c5983997/trabalho%2002%20-%20PIO%20Susceptibility%20in%20Fly-by-Wire%20Systems%20%2831st%20Congress%20of%20the%20International%20Council%20of%20the%20Aeronautical%20Sciences%29_removed.pdf
Vancouver
Moura HC de, Porto Alegre GS, Bidinotto JH, Belo EM. Pio susceptibility in fly-by-wire systems [Internet]. Proceedings. 2018 ;[citado 2024 nov. 02 ] Available from: https://repositorio.usp.br/directbitstream/41346355-4d19-4c4b-9df3-fe68c5983997/trabalho%2002%20-%20PIO%20Susceptibility%20in%20Fly-by-Wire%20Systems%20%2831st%20Congress%20of%20the%20International%20Council%20of%20the%20Aeronautical%20Sciences%29_removed.pdf
Trabalho de evento
An application of digital imaging processing for UAV's automatic landing system AID (2014)
Degrande, Mateus Pereira; Moreira, Emilio Eduardo Tressoldi; Belo, Eduardo Morgado
Source: Proceedings. Conference titles: International Congress of the Aeronautical Sciences - ICAS. Unidade: EESC
Subjects: PROCESSAMENTO DIGITAL DE IMAGENS, AERONAVES, ENGENHARIA AERONÁUTICA
A citação é gerada automaticamente e pode não estar totalmente de acordo com as normas
ABNT
DEGRANDE, Mateus Pereira e MOREIRA, Emilio Eduardo Tressoldi e BELO, Eduardo Morgado. An application of digital imaging processing for UAV's automatic landing system AID. 2014, Anais.. Edinburgh, UK: Optimage Ltd/International Council of Aeronautical Sciences - ICAS, 2014. . Acesso em: 02 nov. 2024.
APA
Degrande, M. P., Moreira, E. E. T., & Belo, E. M. (2014). An application of digital imaging processing for UAV's automatic landing system AID. In Proceedings. Edinburgh, UK: Optimage Ltd/International Council of Aeronautical Sciences - ICAS.
NLM
Degrande MP, Moreira EET, Belo EM. An application of digital imaging processing for UAV's automatic landing system AID. Proceedings. 2014 ;[citado 2024 nov. 02 ]
Vancouver
Degrande MP, Moreira EET, Belo EM. An application of digital imaging processing for UAV's automatic landing system AID. Proceedings. 2014 ;[citado 2024 nov. 02 ]
Trabalho de evento
Hardware-in-the-loop simulation of an H∞ controller on the stabilization of a 2-dof quadrotor (2011)
Breganon, Ricardo; Sampaio, Rafael Coronel Bueno; Souza, Mateus Moreira de; De Salvi, Fabio Toledo Bonemer; Belo, Eduardo Morgado; Becker, Marcelo
Source: Proceedings. Conference titles: International Symposium on Dynamic Problems of Mechanics - DINAME. Unidade: EESC
Subjects: H∞ CONTROLLER, AERONAVES QUADRIMOTORAS, ENGENHARIA MECÂNICA
A citação é gerada automaticamente e pode não estar totalmente de acordo com as normas
ABNT
BREGANON, Ricardo et al. Hardware-in-the-loop simulation of an H∞ controller on the stabilization of a 2-dof quadrotor. 2011, Anais.. Rio de Janeiro, RJ: ABCM, 2011. Disponível em: https://repositorio.usp.br/directbitstream/45fe6e7e-5114-425a-8cec-9147454114a6/trabalho%2015%20-%20HARDWARE-IN-THE-LOOP%20SIMULATION%20OF%20AN%20H%E2%88%9E%20CONTROLLER%20ON%20THE%20STABILIZATION%20OF%20A%202-DOF%20QUADROTOR%20%28DINAME%202011%29.pdf. Acesso em: 02 nov. 2024.
APA
Breganon, R., Sampaio, R. C. B., Souza, M. M. de, De Salvi, F. T. B., Belo, E. M., & Becker, M. (2011). Hardware-in-the-loop simulation of an H∞ controller on the stabilization of a 2-dof quadrotor. In Proceedings. Rio de Janeiro, RJ: ABCM. Recuperado de https://repositorio.usp.br/directbitstream/45fe6e7e-5114-425a-8cec-9147454114a6/trabalho%2015%20-%20HARDWARE-IN-THE-LOOP%20SIMULATION%20OF%20AN%20H%E2%88%9E%20CONTROLLER%20ON%20THE%20STABILIZATION%20OF%20A%202-DOF%20QUADROTOR%20%28DINAME%202011%29.pdf
NLM
Breganon R, Sampaio RCB, Souza MM de, De Salvi FTB, Belo EM, Becker M. Hardware-in-the-loop simulation of an H∞ controller on the stabilization of a 2-dof quadrotor [Internet]. Proceedings. 2011 ;[citado 2024 nov. 02 ] Available from: https://repositorio.usp.br/directbitstream/45fe6e7e-5114-425a-8cec-9147454114a6/trabalho%2015%20-%20HARDWARE-IN-THE-LOOP%20SIMULATION%20OF%20AN%20H%E2%88%9E%20CONTROLLER%20ON%20THE%20STABILIZATION%20OF%20A%202-DOF%20QUADROTOR%20%28DINAME%202011%29.pdf
Vancouver
Breganon R, Sampaio RCB, Souza MM de, De Salvi FTB, Belo EM, Becker M. Hardware-in-the-loop simulation of an H∞ controller on the stabilization of a 2-dof quadrotor [Internet]. Proceedings. 2011 ;[citado 2024 nov. 02 ] Available from: https://repositorio.usp.br/directbitstream/45fe6e7e-5114-425a-8cec-9147454114a6/trabalho%2015%20-%20HARDWARE-IN-THE-LOOP%20SIMULATION%20OF%20AN%20H%E2%88%9E%20CONTROLLER%20ON%20THE%20STABILIZATION%20OF%20A%202-DOF%20QUADROTOR%20%28DINAME%202011%29.pdf
Trabalho de evento
Fuzzy sliding mode control of a flight simulator motion base (2010)
Becerra-Vargas, Mauricio; Belo, Eduardo Morgado
Source: Proceedings. Conference titles: International Congress of the Aeronautical Sciences - ICAS. Unidade: EESC
Subjects: ESTABILIDADE DE LIAPUNOV, SIMULADORES DE VOO, ENGENHARIA AERONÁUTICA
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ABNT
BECERRA-VARGAS, Mauricio e BELO, Eduardo Morgado. Fuzzy sliding mode control of a flight simulator motion base. 2010, Anais.. Edinburgh, UK: Optimage Ltd/International Council of Aeronautical Sciences - ICAS, 2010. . Acesso em: 02 nov. 2024.
APA
Becerra-Vargas, M., & Belo, E. M. (2010). Fuzzy sliding mode control of a flight simulator motion base. In Proceedings. Edinburgh, UK: Optimage Ltd/International Council of Aeronautical Sciences - ICAS.
NLM
Becerra-Vargas M, Belo EM. Fuzzy sliding mode control of a flight simulator motion base. Proceedings. 2010 ;[citado 2024 nov. 02 ]
Vancouver
Becerra-Vargas M, Belo EM. Fuzzy sliding mode control of a flight simulator motion base. Proceedings. 2010 ;[citado 2024 nov. 02 ]
Trabalho de evento
Genetic optimization applied in conceptual and preliminary aircraft design (2008)
Oliveira, Rafael Fernandes de; Cortellazzi Filho, Anselmo Eduardo Jorge; Nakamura, Paulo Henrique lengo; Oioli Neto, Reynaldo; Belo, Eduardo Morgado; Abdalla, Alvaro Martins
Source: Proceedings. Conference titles: International Conference on Genetic and Evolutionary Methods. Unidade: EESC
Subjects: AERONAVES (PROJETO), MULTIDISCIPLINARIDADE, ALGORITMOS GENÉTICOS
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ABNT
OLIVEIRA, Rafael Fernandes de et al. Genetic optimization applied in conceptual and preliminary aircraft design. 2008, Anais.. Las Vegas: Escola de Engenharia de São Carlos, Universidade de São Paulo, 2008. . Acesso em: 02 nov. 2024.
APA
Oliveira, R. F. de, Cortellazzi Filho, A. E. J., Nakamura, P. H. lengo, Oioli Neto, R., Belo, E. M., & Abdalla, A. M. (2008). Genetic optimization applied in conceptual and preliminary aircraft design. In Proceedings. Las Vegas: Escola de Engenharia de São Carlos, Universidade de São Paulo.
NLM
Oliveira RF de, Cortellazzi Filho AEJ, Nakamura PH lengo, Oioli Neto R, Belo EM, Abdalla AM. Genetic optimization applied in conceptual and preliminary aircraft design. Proceedings. 2008 ;[citado 2024 nov. 02 ]
Vancouver
Oliveira RF de, Cortellazzi Filho AEJ, Nakamura PH lengo, Oioli Neto R, Belo EM, Abdalla AM. Genetic optimization applied in conceptual and preliminary aircraft design. Proceedings. 2008 ;[citado 2024 nov. 02 ]
Trabalho de evento
Application of the method EERA for identification in real time of the modal parameters of an aluminnum plate (2007)
Rebolho, Daniela Cristina; Belo, Eduardo Morgado
Source: Proceedings. Conference titles: International Symposium on Dynamic Problems of Mechanics - DINAME. Unidade: EESC
Subjects: TEMPO-REAL, DINÂMICA DE VOO, ENGENHARIA AERONÁUTICA
A citação é gerada automaticamente e pode não estar totalmente de acordo com as normas
ABNT
REBOLHO, Daniela Cristina e BELO, Eduardo Morgado. Application of the method EERA for identification in real time of the modal parameters of an aluminnum plate. 2007, Anais.. Rio de Janeiro, RJ: ABCM, 2007. Disponível em: https://repositorio.usp.br/directbitstream/f388ab4e-7b2b-43fe-8fdf-5110196c6c48/trabalho%2028%20-%20Application%20of%20the%20method%20EERA%20for%20identification%20in%20real%20time%20of%20the%20modal%20parameters%20of%20an%20aluminum%20plate%20%28XII%20DINAME%29.pdf. Acesso em: 02 nov. 2024.
APA
Rebolho, D. C., & Belo, E. M. (2007). Application of the method EERA for identification in real time of the modal parameters of an aluminnum plate. In Proceedings. Rio de Janeiro, RJ: ABCM. Recuperado de https://repositorio.usp.br/directbitstream/f388ab4e-7b2b-43fe-8fdf-5110196c6c48/trabalho%2028%20-%20Application%20of%20the%20method%20EERA%20for%20identification%20in%20real%20time%20of%20the%20modal%20parameters%20of%20an%20aluminum%20plate%20%28XII%20DINAME%29.pdf
NLM
Rebolho DC, Belo EM. Application of the method EERA for identification in real time of the modal parameters of an aluminnum plate [Internet]. Proceedings. 2007 ;[citado 2024 nov. 02 ] Available from: https://repositorio.usp.br/directbitstream/f388ab4e-7b2b-43fe-8fdf-5110196c6c48/trabalho%2028%20-%20Application%20of%20the%20method%20EERA%20for%20identification%20in%20real%20time%20of%20the%20modal%20parameters%20of%20an%20aluminum%20plate%20%28XII%20DINAME%29.pdf
Vancouver
Rebolho DC, Belo EM. Application of the method EERA for identification in real time of the modal parameters of an aluminnum plate [Internet]. Proceedings. 2007 ;[citado 2024 nov. 02 ] Available from: https://repositorio.usp.br/directbitstream/f388ab4e-7b2b-43fe-8fdf-5110196c6c48/trabalho%2028%20-%20Application%20of%20the%20method%20EERA%20for%20identification%20in%20real%20time%20of%20the%20modal%20parameters%20of%20an%20aluminum%20plate%20%28XII%20DINAME%29.pdf
Trabalho de evento
A neural network model to estimate the aerodinamic derivatives of fixed wing aircraft (2007)
Souza, Luciane de Fátima Rodrigues de; Belo, Eduardo Morgado
Source: Proceedings. Conference titles: International Symposium on Dynamic Problems of Mechanics - DINAME. Unidade: EESC
Subjects: SIMULADORES DE VOO, REDES NEURAIS, AERONAVES, ENGENHARIA AERONÁUTICA
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ABNT
SOUZA, Luciane de Fátima Rodrigues de e BELO, Eduardo Morgado. A neural network model to estimate the aerodinamic derivatives of fixed wing aircraft. 2007, Anais.. Rio de Janeiro, RJ: ABCM, 2007. Disponível em: https://repositorio.usp.br/directbitstream/3a80073d-c6c1-4878-ba2e-417bc9b7dd56/trabalho%2029%20-%20A%20neural%20network%20model%20to%20estimate%20the%20aerodynamic%20derivatives%20of%20fixed%20wing%20aircraft%20%28XII%20DINAME%29.pdf. Acesso em: 02 nov. 2024.
APA
Souza, L. de F. R. de, & Belo, E. M. (2007). A neural network model to estimate the aerodinamic derivatives of fixed wing aircraft. In Proceedings. Rio de Janeiro, RJ: ABCM. Recuperado de https://repositorio.usp.br/directbitstream/3a80073d-c6c1-4878-ba2e-417bc9b7dd56/trabalho%2029%20-%20A%20neural%20network%20model%20to%20estimate%20the%20aerodynamic%20derivatives%20of%20fixed%20wing%20aircraft%20%28XII%20DINAME%29.pdf
NLM
Souza L de FR de, Belo EM. A neural network model to estimate the aerodinamic derivatives of fixed wing aircraft [Internet]. Proceedings. 2007 ;[citado 2024 nov. 02 ] Available from: https://repositorio.usp.br/directbitstream/3a80073d-c6c1-4878-ba2e-417bc9b7dd56/trabalho%2029%20-%20A%20neural%20network%20model%20to%20estimate%20the%20aerodynamic%20derivatives%20of%20fixed%20wing%20aircraft%20%28XII%20DINAME%29.pdf
Vancouver
Souza L de FR de, Belo EM. A neural network model to estimate the aerodinamic derivatives of fixed wing aircraft [Internet]. Proceedings. 2007 ;[citado 2024 nov. 02 ] Available from: https://repositorio.usp.br/directbitstream/3a80073d-c6c1-4878-ba2e-417bc9b7dd56/trabalho%2029%20-%20A%20neural%20network%20model%20to%20estimate%20the%20aerodynamic%20derivatives%20of%20fixed%20wing%20aircraft%20%28XII%20DINAME%29.pdf
Trabalho de evento
Variação do número de saídas no processo de identificação em tempo real (2006)
Rebolho, Daniela Cristina; Belo, Eduardo Morgado; De Marqui Junior, Carlos; Marques, Flávio Donizeti; Tsunaki, Roberto Hideaki
Source: Proceedings. Conference titles: Iberian Latin American Congress on Computational Methods in Engineering. Unidade: EESC
Subjects: TEMPO-REAL (IDENTIFICAÇÃO), ALGORITMOS
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ABNT
REBOLHO, Daniela Cristina et al. Variação do número de saídas no processo de identificação em tempo real. 2006, Anais.. Belém: Escola de Engenharia de São Carlos, Universidade de São Paulo, 2006. . Acesso em: 02 nov. 2024.
APA
Rebolho, D. C., Belo, E. M., De Marqui Junior, C., Marques, F. D., & Tsunaki, R. H. (2006). Variação do número de saídas no processo de identificação em tempo real. In Proceedings. Belém: Escola de Engenharia de São Carlos, Universidade de São Paulo.
NLM
Rebolho DC, Belo EM, De Marqui Junior C, Marques FD, Tsunaki RH. Variação do número de saídas no processo de identificação em tempo real. Proceedings. 2006 ;[citado 2024 nov. 02 ]
Vancouver
Rebolho DC, Belo EM, De Marqui Junior C, Marques FD, Tsunaki RH. Variação do número de saídas no processo de identificação em tempo real. Proceedings. 2006 ;[citado 2024 nov. 02 ]
Trabalho de evento
On the investigation of state space reconstruction of non-linear aeroelastic response time series (2005)
Marques, Flavio Donizeti ; Belo, Eduardo Morgado; Oliveira, Vilma Alves de ; Rosolen, José Ricardo; Simoni, Andréia Raquel
Source: Proceedings. Conference titles: International Symposium on Dynamic Problems of Mechanics - DINAME. Unidade: EESC
Subjects: AEROELASTICIDADE DE AERONAVES, VIBRAÇÕES DE AERONAVES, ENGENHARIA AERONÁUTICA
A citação é gerada automaticamente e pode não estar totalmente de acordo com as normas
ABNT
MARQUES, Flavio Donizeti et al. On the investigation of state space reconstruction of non-linear aeroelastic response time series. 2005, Anais.. Rio de Janeiro, RJ: ABCM, 2005. Disponível em: https://repositorio.usp.br/directbitstream/32d28424-a334-4750-a581-2b794dd84893/trabalho%2032%20-%20On%20the%20Investigation%20of%20State%20Space%20Reconstruction%20of%20Non-Linear%20Aeroelastic%20Response%20Time%20Series%20%28XI%20DINAME%29.pdf. Acesso em: 02 nov. 2024.
APA
Marques, F. D., Belo, E. M., Oliveira, V. A. de, Rosolen, J. R., & Simoni, A. R. (2005). On the investigation of state space reconstruction of non-linear aeroelastic response time series. In Proceedings. Rio de Janeiro, RJ: ABCM. Recuperado de https://repositorio.usp.br/directbitstream/32d28424-a334-4750-a581-2b794dd84893/trabalho%2032%20-%20On%20the%20Investigation%20of%20State%20Space%20Reconstruction%20of%20Non-Linear%20Aeroelastic%20Response%20Time%20Series%20%28XI%20DINAME%29.pdf
NLM
Marques FD, Belo EM, Oliveira VA de, Rosolen JR, Simoni AR. On the investigation of state space reconstruction of non-linear aeroelastic response time series [Internet]. Proceedings. 2005 ;[citado 2024 nov. 02 ] Available from: https://repositorio.usp.br/directbitstream/32d28424-a334-4750-a581-2b794dd84893/trabalho%2032%20-%20On%20the%20Investigation%20of%20State%20Space%20Reconstruction%20of%20Non-Linear%20Aeroelastic%20Response%20Time%20Series%20%28XI%20DINAME%29.pdf
Vancouver
Marques FD, Belo EM, Oliveira VA de, Rosolen JR, Simoni AR. On the investigation of state space reconstruction of non-linear aeroelastic response time series [Internet]. Proceedings. 2005 ;[citado 2024 nov. 02 ] Available from: https://repositorio.usp.br/directbitstream/32d28424-a334-4750-a581-2b794dd84893/trabalho%2032%20-%20On%20the%20Investigation%20of%20State%20Space%20Reconstruction%20of%20Non-Linear%20Aeroelastic%20Response%20Time%20Series%20%28XI%20DINAME%29.pdf
Trabalho de evento
Identification of flutter parameters for a wing model (2005)
De Marqui Júnior, Carlos ; Rebolho, Daniela Cristina; Belo, Eduardo Morgado; Marques, Flavio Donizeti
Source: Proceedings. Conference titles: International Symposium on Dynamic Problems of Mechanics - DINAME. Unidade: EESC
Subjects: IDENTIFICAÇÃO DE SISTEMAS, TÚNEIS DE VENTO, AEROELASTICIDADE DE AERONAVES, ENGENHARIA MECÂNICA
A citação é gerada automaticamente e pode não estar totalmente de acordo com as normas
ABNT
DE MARQUI JÚNIOR, Carlos et al. Identification of flutter parameters for a wing model. 2005, Anais.. Rio de Janeiro, RJ: ABCM, 2005. Disponível em: https://repositorio.usp.br/directbitstream/06e14a03-e7b9-43cd-a14f-eebe4cac44e1/PROD_25648_SYSNO_3123819.pdf. Acesso em: 02 nov. 2024.
APA
De Marqui Júnior, C., Rebolho, D. C., Belo, E. M., & Marques, F. D. (2005). Identification of flutter parameters for a wing model. In Proceedings. Rio de Janeiro, RJ: ABCM. Recuperado de https://repositorio.usp.br/directbitstream/06e14a03-e7b9-43cd-a14f-eebe4cac44e1/PROD_25648_SYSNO_3123819.pdf
NLM
De Marqui Júnior C, Rebolho DC, Belo EM, Marques FD. Identification of flutter parameters for a wing model [Internet]. Proceedings. 2005 ;[citado 2024 nov. 02 ] Available from: https://repositorio.usp.br/directbitstream/06e14a03-e7b9-43cd-a14f-eebe4cac44e1/PROD_25648_SYSNO_3123819.pdf
Vancouver
De Marqui Júnior C, Rebolho DC, Belo EM, Marques FD. Identification of flutter parameters for a wing model [Internet]. Proceedings. 2005 ;[citado 2024 nov. 02 ] Available from: https://repositorio.usp.br/directbitstream/06e14a03-e7b9-43cd-a14f-eebe4cac44e1/PROD_25648_SYSNO_3123819.pdf
Trabalho de evento
Wind-tunnel model and a controller for flutter suppression (2004)
De Marqui Júnior, Carlos ; Belo, Eduardo Morgado; Marques, Flavio Donizeti
Source: Proceedings. Conference titles: AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference. Unidade: EESC
Subjects: AEROELASTICIDADE DE AERONAVES, TÚNEIS DE VENTO, ENGENHARIA MECÂNICA
A citação é gerada automaticamente e pode não estar totalmente de acordo com as normas
ABNT
DE MARQUI JÚNIOR, Carlos e BELO, Eduardo Morgado e MARQUES, Flavio Donizeti. Wind-tunnel model and a controller for flutter suppression. 2004, Anais.. Reston, VA: AIAA, 2004. Disponível em: https://doi.org/10.2514/6.2004-1854. Acesso em: 02 nov. 2024.
APA
De Marqui Júnior, C., Belo, E. M., & Marques, F. D. (2004). Wind-tunnel model and a controller for flutter suppression. In Proceedings. Reston, VA: AIAA. doi:10.2514/6.2004-1854
NLM
De Marqui Júnior C, Belo EM, Marques FD. Wind-tunnel model and a controller for flutter suppression [Internet]. Proceedings. 2004 ;[citado 2024 nov. 02 ] Available from: https://doi.org/10.2514/6.2004-1854
Vancouver
De Marqui Júnior C, Belo EM, Marques FD. Wind-tunnel model and a controller for flutter suppression [Internet]. Proceedings. 2004 ;[citado 2024 nov. 02 ] Available from: https://doi.org/10.2514/6.2004-1854
Trabalho de evento
Non-linear phenomena analysis of stall-induced aeroelastic oscillations (2004)
Marques, Flavio Donizeti ; Belo, Eduardo Morgado; Oliveira, Vilma Alves de ; Rosolen, José Ricardo; Simoni, Andréia Raquel
Source: Proceedings. Conference titles: AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference. Unidade: EESC
Subjects: AEROELASTICIDADE DE AERONAVES, ENGENHARIA MECÂNICA
A citação é gerada automaticamente e pode não estar totalmente de acordo com as normas
ABNT
MARQUES, Flavio Donizeti et al. Non-linear phenomena analysis of stall-induced aeroelastic oscillations. 2004, Anais.. Reston, VA: AIAA, 2004. Disponível em: https://doi.org/10.2514/6.2004-1940. Acesso em: 02 nov. 2024.
APA
Marques, F. D., Belo, E. M., Oliveira, V. A. de, Rosolen, J. R., & Simoni, A. R. (2004). Non-linear phenomena analysis of stall-induced aeroelastic oscillations. In Proceedings. Reston, VA: AIAA. doi:10.2514/6.2004-1940
NLM
Marques FD, Belo EM, Oliveira VA de, Rosolen JR, Simoni AR. Non-linear phenomena analysis of stall-induced aeroelastic oscillations [Internet]. Proceedings. 2004 ;[citado 2024 nov. 02 ] Available from: https://doi.org/10.2514/6.2004-1940
Vancouver
Marques FD, Belo EM, Oliveira VA de, Rosolen JR, Simoni AR. Non-linear phenomena analysis of stall-induced aeroelastic oscillations [Internet]. Proceedings. 2004 ;[citado 2024 nov. 02 ] Available from: https://doi.org/10.2514/6.2004-1940
Trabalho de evento
Design and tests of an experimental flutter mount system (2004)
De Marqui Júnior, Carlos; Belo, Eduardo Morgado; Tsunaki, Roberto Hideaki; Rebolho, Daniela Cristina; Marques, Flávio Donizeti
Source: Proceedings. Conference titles: International Modal Analysis Conference - IMAC : a conference and exposition on structural dynamics. Unidade: EESC
Subjects: AERODINÂMICA, AEROELASTICIDADE DE AERONAVES
A citação é gerada automaticamente e pode não estar totalmente de acordo com as normas
ABNT
DE MARQUI JÚNIOR, Carlos et al. Design and tests of an experimental flutter mount system. 2004, Anais.. Bethel, CT: SEM, 2004. . Acesso em: 02 nov. 2024.
APA
De Marqui Júnior, C., Belo, E. M., Tsunaki, R. H., Rebolho, D. C., & Marques, F. D. (2004). Design and tests of an experimental flutter mount system. In Proceedings. Bethel, CT: SEM.
NLM
De Marqui Júnior C, Belo EM, Tsunaki RH, Rebolho DC, Marques FD. Design and tests of an experimental flutter mount system. Proceedings. 2004 ;[citado 2024 nov. 02 ]
Vancouver
De Marqui Júnior C, Belo EM, Tsunaki RH, Rebolho DC, Marques FD. Design and tests of an experimental flutter mount system. Proceedings. 2004 ;[citado 2024 nov. 02 ]
Trabalho de evento
State space reconstruction of non-linear stall-induced oscillatory aeroelastic motion (2004)
Marques, Flávio Donizeti; Belo, Eduardo Morgado; Oliveira, Vilma Alves de
Source: Proceedings. Conference titles: International Congress of the Aeronautical Sciences. Unidade: EESC
Subjects: SISTEMAS NÃO LINEARES, CAOS (SISTEMAS DINÂMICOS), AEROELASTICIDADE DE AERONAVES
A citação é gerada automaticamente e pode não estar totalmente de acordo com as normas
ABNT
MARQUES, Flávio Donizeti e BELO, Eduardo Morgado e OLIVEIRA, Vilma Alves de. State space reconstruction of non-linear stall-induced oscillatory aeroelastic motion. 2004, Anais.. Edinburgh, UK: Optimage Ltd/International Council of Aeronautical Sciences - ICAS, 2004. . Acesso em: 02 nov. 2024.
APA
Marques, F. D., Belo, E. M., & Oliveira, V. A. de. (2004). State space reconstruction of non-linear stall-induced oscillatory aeroelastic motion. In Proceedings. Edinburgh, UK: Optimage Ltd/International Council of Aeronautical Sciences - ICAS.
NLM
Marques FD, Belo EM, Oliveira VA de. State space reconstruction of non-linear stall-induced oscillatory aeroelastic motion. Proceedings. 2004 ;[citado 2024 nov. 02 ]
Vancouver
Marques FD, Belo EM, Oliveira VA de. State space reconstruction of non-linear stall-induced oscillatory aeroelastic motion. Proceedings. 2004 ;[citado 2024 nov. 02 ]
Trabalho de evento
A fuzzy controller for active flutter suppression (2001)
Belo, Eduardo Morgado; Rocha, José Celso; De Marqui Júnior, Carlos
Source: Proceedings. Conference titles: International Symposium on Dynamic Problems of Mechanics. Unidade: EESC
Subjects: AEROELASTICIDADE DE AERONAVES, CONTROLE (TEORIA DE SISTEMAS E CONTROLE), LÓGICA FUZZY
A citação é gerada automaticamente e pode não estar totalmente de acordo com as normas
ABNT
BELO, Eduardo Morgado e ROCHA, José Celso e DE MARQUI JÚNIOR, Carlos. A fuzzy controller for active flutter suppression. 2001, Anais.. Rio de Janeiro: ABCM, 2001. . Acesso em: 02 nov. 2024.
APA
Belo, E. M., Rocha, J. C., & De Marqui Júnior, C. (2001). A fuzzy controller for active flutter suppression. In Proceedings. Rio de Janeiro: ABCM.
NLM
Belo EM, Rocha JC, De Marqui Júnior C. A fuzzy controller for active flutter suppression. Proceedings. 2001 ;[citado 2024 nov. 02 ]
Vancouver
Belo EM, Rocha JC, De Marqui Júnior C. A fuzzy controller for active flutter suppression. Proceedings. 2001 ;[citado 2024 nov. 02 ]
Trabalho de evento
Bilinear system representation of an aircraft dynamics (1999)
Marques, Flávio D; Belo, Eduardo Morgado
Source: Proceedings. Conference titles: Joint Conference Pan American Congress of Applied Mechanics. Unidade: EESC
Assunto: ENGENHARIA DE AERONAVES
A citação é gerada automaticamente e pode não estar totalmente de acordo com as normas
ABNT
MARQUES, Flávio D e BELO, Eduardo Morgado. Bilinear system representation of an aircraft dynamics. 1999, Anais.. Philadelphia: AAM, 1999. . Acesso em: 02 nov. 2024.
APA
Marques, F. D., & Belo, E. M. (1999). Bilinear system representation of an aircraft dynamics. In Proceedings. Philadelphia: AAM.
NLM
Marques FD, Belo EM. Bilinear system representation of an aircraft dynamics. Proceedings. 1999 ;[citado 2024 nov. 02 ]
Vancouver
Marques FD, Belo EM. Bilinear system representation of an aircraft dynamics. Proceedings. 1999 ;[citado 2024 nov. 02 ]
Trabalho de evento
Identification of aircraft non-linear dynamics using Volterra series. [CD-ROM] (1998)
Marques, F D; Belo, Eduardo Morgado
Source: Proceedings. Conference titles: Congress of the International Council of the Aeronautical Sciences. Unidade: EESC
Subjects: TRANSPORTE AÉREO, INTELIGÊNCIA ARTIFICIAL, SISTEMAS NÃO LINEARES
A citação é gerada automaticamente e pode não estar totalmente de acordo com as normas
ABNT
MARQUES, F D e BELO, Eduardo Morgado. Identification of aircraft non-linear dynamics using Volterra series. [CD-ROM]. 1998, Anais.. Melbourne: ICAS/AIAA, 1998. . Acesso em: 02 nov. 2024.
APA
Marques, F. D., & Belo, E. M. (1998). Identification of aircraft non-linear dynamics using Volterra series. [CD-ROM]. In Proceedings. Melbourne: ICAS/AIAA.
NLM
Marques FD, Belo EM. Identification of aircraft non-linear dynamics using Volterra series. [CD-ROM]. Proceedings. 1998 ;[citado 2024 nov. 02 ]
Vancouver
Marques FD, Belo EM. Identification of aircraft non-linear dynamics using Volterra series. [CD-ROM]. Proceedings. 1998 ;[citado 2024 nov. 02 ]
Trabalho de evento
Vibration alleviation of a hingeless helicopter rotor blade by state feedback (1996)
Belo, E M; Maia, A; Marques, F D
Source: Proceedings. Conference titles: Congress of the International Council of the Aeronautical Sciences. Unidade: EESC
Subjects: VIBRAÇÕES, ROTOR, HELICÓPTEROS
A citação é gerada automaticamente e pode não estar totalmente de acordo com as normas
ABNT
BELO, E M e MAIA, A e MARQUES, F D. Vibration alleviation of a hingeless helicopter rotor blade by state feedback. 1996, Anais.. Sorrento: Aiaa, 1996. Disponível em: https://repositorio.usp.br/directbitstream/d69ff488-f584-44b9-bb3a-7e546f3a498c/PROD_000767_SYSNO_912732.pdf. Acesso em: 02 nov. 2024.
APA
Belo, E. M., Maia, A., & Marques, F. D. (1996). Vibration alleviation of a hingeless helicopter rotor blade by state feedback. In Proceedings. Sorrento: Aiaa. Recuperado de https://repositorio.usp.br/directbitstream/d69ff488-f584-44b9-bb3a-7e546f3a498c/PROD_000767_SYSNO_912732.pdf
NLM
Belo EM, Maia A, Marques FD. Vibration alleviation of a hingeless helicopter rotor blade by state feedback [Internet]. Proceedings. 1996 ;[citado 2024 nov. 02 ] Available from: https://repositorio.usp.br/directbitstream/d69ff488-f584-44b9-bb3a-7e546f3a498c/PROD_000767_SYSNO_912732.pdf
Vancouver
Belo EM, Maia A, Marques FD. Vibration alleviation of a hingeless helicopter rotor blade by state feedback [Internet]. Proceedings. 1996 ;[citado 2024 nov. 02 ] Available from: https://repositorio.usp.br/directbitstream/d69ff488-f584-44b9-bb3a-7e546f3a498c/PROD_000767_SYSNO_912732.pdf
Trabalho de evento
Eigenstructure assignment for laser tracking systems (1995)
Belo, E M; Abackerli, A J; Santoro, F G
Source: Proceedings. Conference titles: Symposium on Dynamic Problems of Mechanics. Unidade: EESC
Subjects: ENGENHARIA MECÂNICA, TEORIA DE SISTEMAS E CONTROLE
A citação é gerada automaticamente e pode não estar totalmente de acordo com as normas
ABNT
BELO, E M e ABACKERLI, A J e SANTORO, F G. Eigenstructure assignment for laser tracking systems. 1995, Anais.. Uberlandia: Abcm, 1995. . Acesso em: 02 nov. 2024.
APA
Belo, E. M., Abackerli, A. J., & Santoro, F. G. (1995). Eigenstructure assignment for laser tracking systems. In Proceedings. Uberlandia: Abcm.
NLM
Belo EM, Abackerli AJ, Santoro FG. Eigenstructure assignment for laser tracking systems. Proceedings. 1995 ;[citado 2024 nov. 02 ]
Vancouver
Belo EM, Abackerli AJ, Santoro FG. Eigenstructure assignment for laser tracking systems. Proceedings. 1995 ;[citado 2024 nov. 02 ]

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