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Proportional-Derivative (PD) control is a widely used control method in various engineering systems to enhance stability and performance. In a system with only proportional control, common issues include high maximum overshoot and oscillation, observed in both the error signal and its rate of change. This behavior can be divided into three distinct phases: initial overshoot, subsequent undershoot, and gradual stabilization.
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Related Experiment Video

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Event-Triggering-Learning-Based ADP Control for Post-Stall Pitching Maneuver of Aircraft.

Yaohua Shen, Mou Chen

    IEEE Transactions on Cybernetics
    |October 20, 2022
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    Summary

    This study introduces an improved event-triggering-learning (ETL)-based adaptive dynamic programming (ADP) method for robust aircraft control during post-stall pitching maneuvers, significantly reducing computational costs.

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    Area of Science:

    • Aerospace Engineering
    • Control Systems Theory
    • Computational Intelligence

    Background:

    • Post-stall pitching maneuvers in aircraft present significant control challenges due to unsteady aerodynamic disturbances.
    • Existing control methods may struggle with robustness and computational efficiency in these complex flight regimes.

    Purpose of the Study:

    • To propose an improved event-triggering-learning (ETL)-based adaptive dynamic programming (ADP) method for robust optimal control of aircraft post-stall pitching maneuvers.
    • To reduce the computational cost associated with traditional adaptive dynamic programming techniques.
    • To enhance control system performance by attenuating aerodynamic disturbances.

    Main Methods:

    • Design of a feedforward control incorporating a nonlinear disturbance observer (NDO) to mitigate aerodynamic disturbances.
    • Application of an adaptive dynamic programming (ADP) approach utilizing a critic neural network to approximate the Hamilton-Jacobi-Bellman value function.
    • Integration of an improved event-triggering (ET) mechanism to decrease learning computational cost.

    Main Results:

    • The proposed ETL-based ADP method achieves robust optimal control for aircraft post-stall pitching maneuvers.
    • Significant reduction in computational cost compared to conventional ADP methods.
    • Lyapunov stability theory confirms uniform ultimate boundedness of all closed-loop system signals.

    Conclusions:

    • The developed ETL-based ADP method effectively addresses the challenges of post-stall pitching maneuver control.
    • The integration of NDO and ET mechanisms enhances control robustness and computational efficiency.
    • Simulation results validate the superior performance of the proposed control strategy.