Real-Time Estimation of Time-Varying Bending Modes Using Fiber Bragg Grating Sensor Arrays
Author:
Affiliation:
1. Department of Mechanical and Aerospace Engineering, Florida Institute of Technology, Melbourne, Florida 32901
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.J051702
Reference20 articles.
1. Stability result for dynamic inversion devised to control large flexible aircraft
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