Sergio Esteban

Prof. Sergio Esteban

orcid

Research Focus & Metrics

Academic Career Length

26Years (2001-Present)

(Calculated once Scilit publication data is synced: current year − year of first publication + 1)

Representative Publications

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10 May 2012 in International Journal of Robust and Nonlinear Control
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Journal Article
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Sergio EstebanSergio Esteban
Sergio Esteban
Francisco GordilloFrancisco Gordillo
Francisco Gordillo
JAJ. Aracil
J. Aracil

1 January 2015 in IFAC-PapersOnLine
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Journal Article
Closed access
FGFrancisco Gavilan
Francisco Gavilan
RVRafael Vazquez
Rafael Vazquez
Sergio EstebanSergio Esteban
Sergio Esteban

12 February 2024 in Journal of the Franklin Institute
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Journal Article
Closed access
JCJonatan M. Campos
Jonatan M. Campos
Daniel Neri CardosoDaniel Neri Cardoso
Daniel Neri Cardoso
Sergio EstebanSergio Esteban
Sergio Esteban
Guilherme Vianna RaffoGuilherme Vianna Raffo
Guilherme Vianna Raffo

28 February 2010 in Aerospace Science and Technology
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Journal Article
Closed access
DRDamián Rivas
Damián Rivas
OLOscar Lopez-Garcia
Oscar Lopez-Garcia
Sergio EstebanSergio Esteban
Sergio Esteban
Eduardo GalloEduardo Gallo
Eduardo Gallo

6 August 2001
Verified
Conference Paper
Open access
Sergio EstebanSergio Esteban
Sergio Esteban
The need to investigate the static and dynamic stability for unconventional planes requires development of a code that automates the analysis for the airplane's stability performance. Flying wings are unconventional and challenging to analyze because they lack a tail to control the plane in the longitudinal and the lateral directions. With this motivation, an automated code was designed that was able to accurately predict the stability performance of flying wings. In general most of the stability derivatives that govern the dynamic behavior of an airplane are simplified so they would only include the terms that represent the greatest contribution to its final value. When the greatest contribution to any of the derivatives comes from the tail, and the airplane being analyzed lacks a tail, this represents a problem. This study tries to solve this problem by focusing on decoupling the longitudinal and lateral stability derivatives into its wing and vertical fin contributions.University of Missouri-Roll