Real-Time Shape Estimation for a Small Flexible Flying-Wing Aircraft
Author:
Affiliation:
1. Systems Technology, Inc.
2. D.K. Schmidt and Associates
3. University of Minnesota, Twin Cities
Publisher
American Institute of Aeronautics and Astronautics
Link
https://arc.aiaa.org/doi/pdf/10.2514/6.2019-1818
Reference22 articles.
1. Modal Isolation and Damping for Adaptive Aeroservoelastic Suppression
2. Flight Testing Flutter Suppression on a Small Flexible Flying-Wing Aircraft
3. NDOF Simulation Model for Flight Control Development with Flight Test Correlation
4. Robust Control Design for Active Flutter Suppression
5. Estimation of dynamic structural displacements using fiber Bragg grating strain sensors
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