Estudio del desarrollo de las aeronaves tilt-rotor
DOI:
https://doi.org/10.46842/ipn.cien.v28n2a07Palabras clave:
Tilt-rotor, VANT, Control, Vuelo híbridoResumen
La aeronave de rotor basculante es un diseño híbrido que combina los modos de vuelo de ala fija y ala rotatoria, de esta forma, combina las ventajas de vuelo de los aviones y los helicópteros. En este artículo se presenta la descripción de las aeronaves hibridas en modo de vuelo y el estado del arte del desarrollo de modelos de aeronaves híbridas, y esquemas de control. Se exponen diferentes modelos mecánicos de aeronaves que incluyen mecanismos para la transición de modo de vuelo de ala rotatoria a ala fija y viceversa. También, se formula el modelo matemático empleado comúnmente en los trabajos reportados, así como el planteamiento de algoritmos de control propuestos enfocados en la estabilidad de las aeronaves en su transición de modo de vuelo.
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Derechos de autor 2024 Víctor Gabriel Sánchez Meza, Alberto Luviano Juárez, Yair Lozano Hernández, Jaime González Sierra (Autor/a)
Esta obra está bajo una licencia internacional Creative Commons Atribución-NoComercial-CompartirIgual 4.0.
