Robust Gust Load Alleviation at Different Flight Points and Mass configurations
Author:
Affiliation:
1. Airbus SAS
2. Laboratoire Ampere
Publisher
American Institute of Aeronautics and Astronautics
Link
https://arc.aiaa.org/doi/pdf/10.2514/6.2022-0285
Reference40 articles.
1. Gust Loads Alleviation Using Special Control Surfaces
2. Gust Load Alleviation for a Regional Aircraft Through a Static Output Feedback
3. Integrated Flight/Structural Mode Control for Very Flexible Aircraft Using L1 Adaptive Output Feedback Controller
4. Gradient-Based Aeroservoelastic Optimization with Static Output Feedback
5. Multiple-Input Multiple-Output Experimental Aeroelastic Control Using a Receptance-Based Method
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