Instrument Landing System Lateral Beam Guidance System Based on Sliding Mode Control Technique
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Resumen
En este artículo se muestra un entorno basado en Matlab-Simulink para el análisis de un sistema de aterrizaje de un avión que puede ser utilizado para el aterrizaje automatizado o asistido. Se describe la construcción de un modelo matemático que posteriormente es simulado para validar su funcionamiento. Finalmente, el controlador por modos deslizantes es implementado y se analiza el comportamiento del sistema controlado incluso tomando en cuenta perturbaciones.
Abstract:This paper shows an environment based on Matlab-Simulink to analyze a landing system of an aircraft which can be used for automated or assisted landing. Firstly, it is described the development of a mathematical model which is simulated to validate its performance. Finally, the sliding mode controller is implemented, and the behavior of the controlled system is analyzed even taking into account disturbances.
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E.McGookin,"Instrument Landing System Lateral Beam Guidance System,"University of Glasgow, Oct. 2012
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