Novel Concepts for Active Load Alleviation
Author:
Affiliation:
1. Technische Universitat Braunschweig
2. Deutsches Zentrum fur Luft- und Raumfahrt DLR Standort Braunschweig
Publisher
American Institute of Aeronautics and Astronautics
Link
https://arc.aiaa.org/doi/pdf/10.2514/6.2022-0009
Reference51 articles.
1. Maneuver Load Control for Flexible Delta Wing Using Multidisciplinary Design Optimization
2. Aircraft Design with Maneuver and Gust Load Alleviation
3. Gust Load Alleviation for a Regional Aircraft Through a Static Output Feedback
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3. Aeroservoelastic Wind Tunnel Evaluation of Preview H2 and H∞ Gust Load Alleviation;Journal of Guidance, Control, and Dynamics;2023-11
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