Flexible Aircraft Simulation Validation with Flight Test Data
Author:
Affiliation:
1. Aeronautics Institute of Technology, 12228-900 São José dos Campos, Brazil
2. Technical University of Berlin, 10587 Berlin, Germany
3. Embraer S.A., 12247-004 São José dos Campos, Brazil
4. University of Michigan, Ann Arbor, Michigan 48109-2140
Funder
Financiadora de Estudos e Projetos
Conselho Nacional de Desenvolvimento Científico e Tecnológico
Embraer
Coordenação de Aperfeiçoamento de Pessoal de Nível Superior
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.J060960
Reference36 articles.
1. Nonlinear Aeroelastic Analysis of Complete Aircraft in Subsonic Flow
2. Nonlinear Aeroelasticity and Flight Dynamics of High-Altitude Long-Endurance Aircraft
3. Nonlinear Flight Dynamics of Very Flexible Aircraft
4. Trajectory Control for Very Flexible Aircraft
5. Flight dynamics of aeroelastic vehicles
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