PG-EAM - Programa de Pós-Graduação em Engenharia Aeronáutica e Mecânica
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Artigo 2022

IDENTIFICATION OF THE COMPLETE AERODYNAMIC MODEL OF A SUBSCALE FLIGHT TESTING

Autores

Fischer, Clécio
Nepomuceno, Leonardo Murilo
de Moura, Éder Alves

33rd Congress of the International Council of the Aeronautical Sciences Icas 2022 , vol. 7 , pp. 5441-5450

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Resumo

© (2022) by International Council of Aeronautical Sciences (ICAS) All rights reserved.Subscale aircraft have been used for decades to design new aircraft and evaluate new design techniques. The acquisition of in-flight data from subscale aircraft is already possible today, such as a manned or fullscale aircraft. Thus, more reliable flight simulators are built for flight quality analysis and control design. This work aims to implement a data acquisition and processing system, with the objective of identifying the complete dynamics of a subscale aircraft, model Cessna 182.

Palavras-chave

acquisition and processing system flight testing subscale system identification

Aerospace Engineering (ENGI) Control and Systems Engineering (ENGI) Electrical and Electronic Engineering (ENGI) Materials Science (all) (MATE)
: Scopus
Última atualização: 2026-06-25
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