In this paper, the authors address the critical issue of quantifying maximum actuator degradation in linear dynamical systems. Actuator degradation is crucial in engineering control systems due to wear, environmental influences, or aging components leading to diminished performance and potential system failure. The study focuses on developing methodologies for assessing and quantifying maximum actuator degradation to ensure robustness in various engineering applications.
The content explores two main approaches in addressing faults or degradation in systems: enhancing controller robustness by integrating degradation estimates and developing models for actuator degradation. Various papers are referenced, showcasing methods related to fault-tolerant control design utilizing actuator health information, modeling actuator degradation using different algorithms, and introducing controllers for electric vehicles that enhance speed tracking and reliability.
The authors introduce a novel unified framework involving convex optimization formulations to determine the controller gain while maximizing actuator degradation and maintaining desired closed-loop performance. The results are demonstrated through the design of a full-state feedback controller for an F-16 aircraft model representing longitudinal motion.
Key contributions include presenting new convex optimization formulations that concurrently determine the controller gain, maximize actuator degradation, and ensure desired closed-loop performance in both H2 and H∞ system norms. The study is limited to open-loop stable systems but provides valuable insights into quantifying worst-case or maximum actuator degradation for acceptable closed-loop performance.
The technical results section delves into detailed mathematical notations, theorems, proofs, and examples applying the findings to flight control applications like F-16 aircraft models. Simulation results highlight minimum actuator cutoff frequencies, DC gains, maximum actuator noise scaling values across different actuators like thrust (T), elevator (δe), and leading-edge flap (δlef).
Overall, this content provides a comprehensive analysis of quantifying maximum actuator degradation for achieving optimal closed-loop performance in engineering control systems.
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by Hrishav Das,... о arxiv.org 03-05-2024
https://arxiv.org/pdf/2403.01333.pdfГлибші Запити