Real-Time Parameter Estimation and Prediction-Based Control for Aircraft Pitch Dynamics
Graduate Course Project, National Cheng Kung University, ME 8601 Adaptive Control (Instructor: Ming-Shaung Ju), 2021
This project utilizes the recursive integral-operator-based least-squares (RLS) algorithm to estimate the system parameters for a aircraft pitch dynamics (textbook example). The simulation results show that the proposed RLS estimator enable to estimate the system parameters. By introduced the predicted states as the feedback states, the control performance is further improved.
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