Aerodynamic Modeling of an Unmanned Aerial Vehicle using Vortex Lattice Method

Autores

  • David F. Castillo-Zúñiga
  • Raphaela. C. Machado
  • Luiz. C. S. Góes

Resumo

The determination of a aircraft aerodynamic characteristics is an important stage in aircraft flight simulation. In order to compose the flight aircraft equations of motions the computation of the aerodynamics stability and control derivatives is needed. In this work will presented a methodology to modeling the aerodynamic and flight dynamics characteristics of an Unmanned Aerial Vehicle (UAV). The steady aerodynamic coefficients are calculated based on the vortex-laticce method. The research platform is the Vector-P UAV [1, 2] shown in the Fig. 1. [...]

Downloads

Não há dados estatísticos.

Biografia do Autor

David F. Castillo-Zúñiga

DEA/UNESP, São João da Boa Vista, SP

Raphaela. C. Machado

DEE/UNESP, Guaratinguetá, SP

Luiz. C. S. Góes

ITA, São José dos Campos, SP

Referências

G. D. Franco. Instrumentação e operacionalização de um sistema de ensaios em voo para VANTs (VECTOR-P). 2009.

D. F. Castillo-Zuñiga. Análise Aeroelástica e Comparação com Ensaio em Voo de uma Aeronave Não Tripulada. 2013.

Brian L Stevens, Frank L Lewis, and Eric N Johnson. Aircraft control and simulation: dynamics, controls design, and autonomous systems. 2nd. Hoboken, New Jersey: John Wiley and Sons, 2015.

Ravindra V. Jategaonkar. Flight Vehicle System Identification: A Time-Domain Methodology, Second Edition. Reston, VA: American Institute of Aeronautics and Astronautics, Inc., Jan. 2015. isbn: 978-1-62410-278-3. doi: 10.2514/4.102790. url: http://arc.aiaa.org/doi/book/10.2514/4.102790.

Downloads

Publicado

2023-12-18

Edição

Seção

Resumos