Optimized neural network based controller for a nonlinear aeroelastic system
Author:
Affiliation:
1. Rensselaer Polytechnic Inst., Troy, NY
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1997-1182
Reference24 articles.
1. Molusis, J. A., Mookergee, P. and Bar-Shalom, Y. "Evaluation of the Effect of Vibration Nonlinearity on ConvergenceBehavior of Adaptive Higher HarmonicControl,"NASA CR-166424,Jan. 1983.
2. Neural networks approach to AIAA aircraft control design challenge
3. Variable structure systems with sliding modes
4. Refined H-infinity-optimal approach to rotorcraft flight control
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1. Integrated wing design with adaptive control surfaces;19th AIAA Applied Aerodynamics Conference;2001-06-11
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