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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: 30 nov. 2025.
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 2025 nov. 30 ]
Vancouver
Degrande MP, Moreira EET, Belo EM. An application of digital imaging processing for UAV's automatic landing system AID. Proceedings. 2014 ;[citado 2025 nov. 30 ]
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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: 30 nov. 2025.
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 2025 nov. 30 ] 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 2025 nov. 30 ] 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
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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: 30 nov. 2025.
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 2025 nov. 30 ]
Vancouver
Becerra-Vargas M, Belo EM. Fuzzy sliding mode control of a flight simulator motion base. Proceedings. 2010 ;[citado 2025 nov. 30 ]
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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: 30 nov. 2025.
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 2025 nov. 30 ]
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 2025 nov. 30 ]
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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: 30 nov. 2025.
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 2025 nov. 30 ] 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 2025 nov. 30 ] 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
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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: 30 nov. 2025.
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 2025 nov. 30 ] 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 2025 nov. 30 ] 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
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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: 30 nov. 2025.
APA
Rebolho, D. C., Belo, E. M., De Marqui Júnior, 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 Júnior C, Marques FD, Tsunaki RH. Variação do número de saídas no processo de identificação em tempo real. Proceedings. 2006 ;[citado 2025 nov. 30 ]
Vancouver
Rebolho DC, Belo EM, De Marqui Júnior C, Marques FD, Tsunaki RH. Variação do número de saídas no processo de identificação em tempo real. Proceedings. 2006 ;[citado 2025 nov. 30 ]
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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: 30 nov. 2025.
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 2025 nov. 30 ] 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 2025 nov. 30 ] 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
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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: 30 nov. 2025.
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 2025 nov. 30 ] 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 2025 nov. 30 ] Available from: https://repositorio.usp.br/directbitstream/06e14a03-e7b9-43cd-a14f-eebe4cac44e1/PROD_25648_SYSNO_3123819.pdf
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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: 30 nov. 2025.
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 2025 nov. 30 ] 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 2025 nov. 30 ] Available from: https://doi.org/10.2514/6.2004-1854
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 2025 nov. 30 ] 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 2025 nov. 30 ] Available from: https://doi.org/10.2514/6.2004-1940
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DE MARQUI JÚNIOR, Carlos et al. Design and tests of an experimental flutter mount system. 2004, Anais.. Bethel, CT: SEM, 2004. . Acesso em: 30 nov. 2025.
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 2025 nov. 30 ]
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 2025 nov. 30 ]
A citação é gerada automaticamente e pode não estar totalmente de acordo com as normas
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MARQUES, Flavio 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: 30 nov. 2025.
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 2025 nov. 30 ]
Vancouver
Marques FD, Belo EM, Oliveira VA de. State space reconstruction of non-linear stall-induced oscillatory aeroelastic motion. Proceedings. 2004 ;[citado 2025 nov. 30 ]
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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: 30 nov. 2025.
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 2025 nov. 30 ]
Vancouver
Belo EM, Rocha JC, De Marqui Júnior C. A fuzzy controller for active flutter suppression. Proceedings. 2001 ;[citado 2025 nov. 30 ]
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MARQUES, Flavio Donizeti e BELO, Eduardo Morgado. Identification of aircraft non-linear dynamics using Volterra series. [CD-ROM]. 1998, Anais.. Melbourne: ICAS/AIAA, 1998. . Acesso em: 30 nov. 2025.
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 2025 nov. 30 ]
Vancouver
Marques FD, Belo EM. Identification of aircraft non-linear dynamics using Volterra series. [CD-ROM]. Proceedings. 1998 ;[citado 2025 nov. 30 ]
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ABNT
BELO, Eduardo Morgado e MAIA, A e MARQUES, Flavio Donizeti. 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: 30 nov. 2025.
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 2025 nov. 30 ] 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 2025 nov. 30 ] Available from: https://repositorio.usp.br/directbitstream/d69ff488-f584-44b9-bb3a-7e546f3a498c/PROD_000767_SYSNO_912732.pdf
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BELO, Eduardo Morgado e ABACKERLI, A J e SANTORO, F G. Eigenstructure assignment for laser tracking systems. 1995, Anais.. Uberlandia: Abcm, 1995. . Acesso em: 30 nov. 2025.
APA
Belo, E. M., Abackerli, A. J., & Santoro, F. G. (1995). Eigenstructure assignment for laser tracking systems. In Proceedings. Uberlandia: Abcm.
Belo, E. M., & Marques, F. D. (1995). Eigenstructure assignment for helicopter rotor blade vibration control. In Proceedings. Uberlandia: Abcm. Recuperado de https://repositorio.usp.br/directbitstream/26b87ab4-97c2-457e-922e-a9f546ba17f7/PROD_000763_SYSNO_887514.pdf
NLM
Belo EM, Marques FD. Eigenstructure assignment for helicopter rotor blade vibration control [Internet]. Proceedings. 1995 ;[citado 2025 nov. 30 ] Available from: https://repositorio.usp.br/directbitstream/26b87ab4-97c2-457e-922e-a9f546ba17f7/PROD_000763_SYSNO_887514.pdf
Vancouver
Belo EM, Marques FD. Eigenstructure assignment for helicopter rotor blade vibration control [Internet]. Proceedings. 1995 ;[citado 2025 nov. 30 ] Available from: https://repositorio.usp.br/directbitstream/26b87ab4-97c2-457e-922e-a9f546ba17f7/PROD_000763_SYSNO_887514.pdf
A citação é gerada automaticamente e pode não estar totalmente de acordo com as normas
ABNT
BELO, Eduardo Morgado e MARQUES, Flavio Donizeti. Analysis and vibration control of a helicopter rotor blade. 1994, Anais.. Stevenage: Iee, 1994. Disponível em: https://repositorio.usp.br/directbitstream/c3948c55-7cba-493b-a135-dcf3b5e2eee7/PROD_000760_SYSNO_885594.pdf. Acesso em: 30 nov. 2025.
APA
Belo, E. M., & Marques, F. D. (1994). Analysis and vibration control of a helicopter rotor blade. In Proceedings. Stevenage: Iee. Recuperado de https://repositorio.usp.br/directbitstream/c3948c55-7cba-493b-a135-dcf3b5e2eee7/PROD_000760_SYSNO_885594.pdf
NLM
Belo EM, Marques FD. Analysis and vibration control of a helicopter rotor blade [Internet]. Proceedings. 1994 ;[citado 2025 nov. 30 ] Available from: https://repositorio.usp.br/directbitstream/c3948c55-7cba-493b-a135-dcf3b5e2eee7/PROD_000760_SYSNO_885594.pdf
Vancouver
Belo EM, Marques FD. Analysis and vibration control of a helicopter rotor blade [Internet]. Proceedings. 1994 ;[citado 2025 nov. 30 ] Available from: https://repositorio.usp.br/directbitstream/c3948c55-7cba-493b-a135-dcf3b5e2eee7/PROD_000760_SYSNO_885594.pdf