Parametric Model Identification of Nonlinear Aircraft System With Actuator Saturation
Author:
Affiliation:
1. Babol Noshirvani University of Technology,Faculty of Electrical and Computer Engineering,Babol,Iran
Publisher
IEEE
Link
http://xplorestaging.ieee.org/ielx7/9945699/9945700/09945765.pdf?arnumber=9945765
Reference16 articles.
1. Stability Analysis of Model Reference Adaptive Control with the New Theorem of Stability
2. Design and Implementation of a Real-Time Nonlinear Model Predictive Controller for a Lower Limb Exoskeleton with Input Saturation;zarandi;Iranian Journal of Science and Technology Transactions of Electrical Engineering,2020
3. Introspective Control Systems: Fast Model Predictive Control with Explicit Optimization Search, Nonlinear Models, and On-line Learning
4. Pilot-Induced-Oscillations Alleviation Through Anti-windup Based Approach
5. Flight testing of a rate saturation compensation scheme on the ATTAS aircraft
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