
Daniel AgudeloCENTRO3D CORP SAS
Daniel Agudelo
MSc Aerospace Engineering
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11
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Introduction
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January 2013 - May 2017
Publications
Publications (11)
Aircraft aerodynamic forces and moments can be expressed as a function of the dynamic pressure, aircraft dimensions and flight conditions. They are very important do predict the aircraft behavior and performance. Moreover, they play an important role predicting the model response to control inputs. For these reasons it is important to accurate dete...
This paper presents an analysis of a Total Energy Control System (TECS) introduced by Lambregts to control unmanned aerial vehicle (UAV) velocity and altitude by using the total energy distribution. Furthermore, an extended Kalman filter (EKF) approach was used to predict aircraft response in terms of angular rates and linear acceleration during a...
Este capítulo presenta el desarrollo y validación de la herramienta computacional Aplicación para la Resolución de Casos de Deformación en el Uso de Materiales Compuestos (ARCUM), la cual fue diseñada a partir de un proyecto de investigación desarrollado en la Universidad de San Buenaventura, sede Bogotá, con el propósito de determinar el comportam...
Actualmente existe una gran variedad de materiales y procesos de manufactura que suplen las necesidades de los diferentes sectores industriales a nivel mundial. Los procesos de investigación, innovación y desarrollo generan constantemente nuevos materiales y tecnologías aplicables a los procesos de diseño y manufactura. Como resultado, los sistemas...
El modelo productivo actual y el desarrollo de nuevos productos de forma rápida y óptima han impulsado cada vez más el uso de técnicas de prototipado rápido. Dentro de las técnicas de prototipado rápido, la impresión 3D mediante el modelamiento por deposición de hilo fundido se ha posicionado debido a su versatilidad, facilidad y economía [1]. Por...
In this paper, two sets of multisine signals are designed for system identification purposes. The first one is obtained without any information about system dynamics. In the second case, the a priori information is given in terms of dimensional stability and control derivatives. Magnitude Bode plots are obtained to design the multisine power spectr...
The objective of the project was to determine if the accuracy of the estimated data for lateral motion could be increased by the use a priori model information during the system identification multisine maneuver design process. For this purpose, a linear aircraft model was used which contains a-priori information in terms of aerodynamic derivatives...
The aim of the project was to determine if including a-priori information in the system identification multisine maneuver design process will improve the quality of the estimated data in the lateral motion. During this study we used a linear aircraft model which was containing a-priori information in terms of aerodynamic derivatives. A-priori knowl...
The objective of the project was to determine if the accuracy of the estimated data for lateral motion could be increased by the use a priori model information during the system identification multisine maneuver design process. For this purpose, a linear aircraft model was used which contains a-priori information in terms of aerodynamic derivatives...