Gust Load Alleviation and Ride Quality Improvement with Incremental Nonlinear Dynamic Inversion
Author:
Affiliation:
1. Delft University of Technology
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2017-1400
Reference21 articles.
1. Flight dynamics of aeroelastic vehicles
2. A Multi-Objective Flight Control Approach for Performance Adaptive Aeroelastic Wing
3. Adaptive Linear Quadratic Gaussian Optimal Control Modification for Flutter Suppression of Adaptive Wing
4. Gust Loads Alleviation Using Special Control Surfaces
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