Modelo Matemático para un Vehículo Aéreo no Tripulado de Ala Fija, Usando un Estimador de Parámetros “Filtro de Kalman”
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.
How to Cite
[1]
P. A. Ortiz-Valencia and L. B. Gutiérrez-Zea, “Modelo Matemático para un Vehículo Aéreo no Tripulado de Ala Fija, Usando un Estimador de Parámetros ‘Filtro de Kalman’”, TecnoL., no. 22, pp. 75–98, Jun. 2009.
Downloads
Download data is not yet available.
