Model Predictive Control Architectures for Maneuver Load Alleviation in Very Flexible Aircraft
Author:
Affiliation:
1. University of Michigan, Ann Arbor
2. Airbus
Publisher
American Institute of Aeronautics and Astronautics
Link
https://arc.aiaa.org/doi/pdf/10.2514/6.2019-1591
Reference28 articles.
1. Nonlinear Aeroelastic Simulation of X-HALE: a Very Flexible UAV
2. Improving the Airplane Efficiency by Use of Wing Maneuver Load Alleviation
3. X-HALE: A Very Flexible Unmanned Aerial Vehicle for Nonlinear Aeroelastic Tests
4. Reexamined Structural Design Procedures for Very Flexible Aircraft
5. Predictive Control for Alleviation of Gust Loads on Very Flexible Aircraft
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