Design and Flight Test of a Stability Augmentation System for a Flexible Aircraft
Author:
Affiliation:
1. Aeronautics Institute of Technology, 12228-900 São José dos Campos, Brazil
2. Technical University of Berlin, 10587 Berlin, Germany
Funder
Embraer
Coordenação de Aperfeiçoamento de Pessoal de Nível Superior
Financiadora de Estudos e Projetos
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Applied Mathematics,Electrical and Electronic Engineering,Space and Planetary Science,Aerospace Engineering,Control and Systems Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.G006271
Reference23 articles.
1. High-Altitude Platforms - Present Situation and Technology Trends
2. X-HALE: A Very Flexible Unmanned Aerial Vehicle for Nonlinear Aeroelastic Tests
3. Preliminary flight test correlations of the X-HALE aeroelastic experiment
4. Aircraft Control Based on Flexible Aircraft Dynamics
5. Loop-Separation Control for Very Flexible Aircraft
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1. Wind Tunnel Investigations of a Pitch-Free Flexible High Aspect Ratio Aircraft Model;AIAA SCITECH 2024 Forum;2024-01-04
2. An improved linear parameter-varying modeling, model order reduction, and control design process for flexible aircraft;Aerospace Science and Technology;2024-01
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