Modelo Matemático para un Vehículo Aéreo no Tripulado de Ala Fija, Usando un Estimador de Parámetros “Filtro de Kalman”

  • Paula A. Ortiz-Valencia Instituto Tecnológico Metropolitano, Medellín
  • Luis B. Gutiérrez-Zea Universidad Pontificia Bolivariana, Medellín
Keywords: UAV, Kalman Filter Aerodynamical Coefficients.

Abstract

On this work a mathematical model is presented for an UAV that is being developed in UPB (Pontifical Bolivarian University)for the Automatics and Design investigation group (A+D), in the project “Design of a fixed wing unmanned flying vehicle for inspection and vigilance (AURA)”. In order to develop the UAV model, two steps were followed: On the first one, the mathematical equations describing aircraft behavior were gotten, in terms of aerodynamical coefficients, depending on particular aircraft characteristics. On the second step, the values of these coefficients were found using an extended Kalman filter.

Author Biographies

Paula A. Ortiz-Valencia, Instituto Tecnológico Metropolitano, Medellín
Ingeniera en Instrumentación y Control. Magíster en Ingeniería Área Automática. Docente de tiempo completo Instituto Tecnológico Metropolitano, Medellín
Luis B. Gutiérrez-Zea, Universidad Pontificia Bolivariana, Medellín
Ingeniero electrónico. PhD. Docente Investigador Universidad Pontificia Bolivariana, Medellín
How to Cite
Ortiz-Valencia, P. A., & Gutiérrez-Zea, L. B. (2009). Modelo Matemático para un Vehículo Aéreo no Tripulado de Ala Fija, Usando un Estimador de Parámetros “Filtro de Kalman”. TecnoLógicas, (22), 75-98. https://doi.org/10.22430/22565337.229

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Published
2009-06-27
Section
Articles

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