Application of a Kalman Filter for Reduction of Sensor/Turbulence-Induced Noise Within a Model Reference Adaptive Controller
Author:
Affiliation:
1. Wichita State University
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2016-1625
Reference13 articles.
1. Linear and neural network feedback for flight control decoupling
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4. Adaptive Control of an Elastic General Aviation Aircraft
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