2 research outputs found
Análisis y control de la dinámica lateral de aviones.
Objetivos y método de estudio: ´ El objetivo general de esta tesis es analizar, mediante el marco de trabajo de Individual Channnel Analysis and Design, ICAD, los acoplamientos dinámicos que se tienen en el movimiento lateral de aviones en configuración estándar. El método de estudio fue totalmente analítico. Se escogió el modelo estándar para aviones en configuración convencional. Se analizaron cada uno de los 12 casos posibles de emparejamientos mediante el análisis de la Multivariable Structure Function. Se muestra un caso de estudio numérico para una aeronave militar. Contribuciones y conclusiones: La contribución, y conclusión, principal es que el emparejamiento entre alerones con ´ángulo de alabeo y timón direccional co
Fundamental Analysis of the Perturbation Rejection Characteristics of Single-Input-Multiple-Output Systems Subject to Multiple Perturbations
Single-Input-Multiple-Output (SIMO) systems are found in several applications. Some of the main concerns are (1) the possibility
of stabilizing all the outputs and (2) the possibility of attaining independent tracking control of all the outputs. Whereas the first
issue can be easily be elucidated, the second has proven to be impossible in all but a few systems. In many cases one practical option
is to use the input to drive a main output, taking care that the behavior of the remaining secondary outputs is acceptable. In this
configuration, in addition to the features of the main control loop, the perturbation rejection properties of the secondary outputs
become important. This article analyzes the structural properties, stability, and perturbation rejection characteristics of SIMO
systems. The article presents fundamental conclusions regarding the relationship of the main control loop and the perturbation
rejection characteristics of the secondary outputs. A simple and intuitive example is used to show how the theoretical findings can
be used to improve the design of the main control loop through its frequency domain characteristics. The results are developed
using simple frequency domain theoretical elements, making the findings relevant for both engineering applications and deriving
further theoretical developments