Nonlinear Aeroelastic Control of Very Flexible Aircraft Using Model Updating
Author:
Affiliation:
1. Imperial College, London, England SW7 2AZ, United Kingdom
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.C034684
Reference29 articles.
1. Reexamined Structural Design Procedures for Very Flexible Aircraft
2. Flight Dynamics of Highly Flexible Aircraft
3. Dynamic Response of Highly Flexible Flying Wings
4. Nonlinear-Aerodynamics/Nonlinear-Structure Interaction Methodology for a High-Altitude Long-Endurance Wing
5. Applications of the unsteady vortex-lattice method in aircraft aeroelasticity and flight dynamics
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