Recent Advances in Adaptive Control Theory and Applications for Nonlinear Systems

A special issue of Mathematics (ISSN 2227-7390). This special issue belongs to the section "E2: Control Theory and Mechanics".

Deadline for manuscript submissions: 31 August 2026 | Viewed by 692

Special Issue Editors


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Guest Editor
School of Information and Control Engineering, Qingdao University of Technology, Qingdao 266520, China
Interests: neural networks; adaptive control; sliding mode control

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Guest Editor
School of Automation and Electrical Engineering, University of Science and Technology Beijing, Beijing 100083, China
Interests: adaptive control; self-tuning control; multiple model adaptive control; multiple model adaptive estimation; stability analysis
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Guest Editor
Faculty of Mechanical & Electrical Engineering, Kunming University of Science & Technology, Kunming 650500, China
Interests: adaptive control; intelligent control; parameter estimation; nonlinear control and application
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Guest Editor
Zhejiang Key Laboratory of Intelligent Perception and Control for Complex Systems, College of Information Engineering, Zhejiang University of Technology, Hangzhou 310023, China
Interests: adaptive and learning control; data-driven control of magnetically controlled capsules; intelligent adaptive control of electromechanical systems
Special Issues, Collections and Topics in MDPI journals

Special Issue Information

Dear Colleagues,

Adaptive control serves as a foundational element of modern control engineering, enabling systems to autonomously maintain performance, stability, and robustness in the face of dynamic uncertainties and changing operating conditions. Its importance extends beyond theoretical innovation to mission-critical applications, effectively bridging the gap between idealized models and practical implementation.

However, the adaptive control of nonlinear systems involves significant challenges. These include establishing mathematically rigorous stability guarantees, ensuring robustness against unmodeled dynamics and external disturbances, and achieving computational efficiency sufficient for real-time operation.

This Special Issue, titled “Recent Advances in Adaptive Control Theory and Applications for Nonlinear Systems”, aims to highlight recent advances in the adaptive control theory and practical implementations. In response to feedback from the Editorial Board, we explicitly welcome contributions that also cover advanced topics in robust adaptive control with fixed/predefined-time convergence, data-driven adaptive dynamic programming and learning, adaptive control for multi-agent systems, adaptive model predictive control, adaptive control under multi-constraints, and hybrid learning-adaptive control fusion.

We encourage works that combine theoretical developments with real-world applications of control techniques, including, but not limited to, sliding mode control, intelligent observers, fractional-order controllers, high-gain estimation, machine learning-based adaptive schemes, adaptive graph neural networks, semi-supervised multi-modal fusion, permanent magnet motors, nonlinear modeling, optimal control, aircraft control, synchronization, system identification, and defect detection. Contributions exploring the convergence between robust linear theory and nonlinear dynamics are especially welcome.

Of particular interest are studies that demonstrate the interplay between mathematics and engineering, showcasing innovative uses of nonlinear models, optimal feedback strategies, and data-driven approaches applied to electrical, biological, or mechanical systems. Cross-disciplinary research combining control theory with robotics, biotechnology, computer vision, artificial intelligence, and process industries is highly encouraged.

We invite researchers from academia and industry to submit original papers that contribute to this vibrant and evolving field, strengthening the connection between mathematical theory and technological innovation.

Dr. Jianhua Zhang
Dr. Weicun Zhang
Prof. Dr. Jing Na
Prof. Dr. Qiang Chen
Guest Editors

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Keywords

  • adaptive control
  • neural networks
  • sliding mode control
  • multi-agent systems
  • observer
  • synchronization
  • optimization
  • predictive control

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Published Papers (2 papers)

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Research

31 pages, 1414 KB  
Article
Optimal Control of a Small Flexible Aircraft Using an Active Gust Alleviation Device
by Yanxuan Wu, Yifan Fu, Hao Li, Xudong Luo and Haonan Sun
Mathematics 2025, 13(24), 3986; https://doi.org/10.3390/math13243986 - 14 Dec 2025
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Abstract
Small flexible-wing aircraft are vulnerable to gusts due to their low inertia and operating regime at low-Reynolds-number regimes, compromising flight stability and mission reliability. This paper introduces a novel active gust alleviation device (AGAD) installed at the wingtip, which works in concert with [...] Read more.
Small flexible-wing aircraft are vulnerable to gusts due to their low inertia and operating regime at low-Reynolds-number regimes, compromising flight stability and mission reliability. This paper introduces a novel active gust alleviation device (AGAD) installed at the wingtip, which works in concert with the conventional tail-plane to form a multi-surface control system. To coordinate these surfaces optimally, a quasi-static aeroelastic aircraft model is established, and a linear–quadratic regulator (LQR) controller is designed. A key innovation is the integration of an extended state observer (ESO) to estimate the unmeasurable, gust-induced angle of attack in real time, allowing the LQR to effectively counteract unsteady disturbances. Comparative simulations against a baseline (tail-plane-only control) demonstrate the superiority of the combined AGAD-tail strategy: the peak gust responses in pitch angle and normal acceleration are reduced by over 57% and 20%, respectively, while structural loads at the wing root are also significantly attenuated. Furthermore, the AGAD enhances maneuverability, reducing climb time by 20% during a specified maneuver. This study confirms that the integrated AGAD and LQR-ESO framework provides a practical and effective solution for enhancing both the stability and agility of small flexible aircraft in gusty environments, with direct benefits for applications like precision inspection and monitoring. Full article
23 pages, 8067 KB  
Article
Closed-Loop Inner–Outer Dual-Loop Attitude Adjustment Control for Dual-Super Spacecraft with Pointing Constraints
by Jiaxiang Xie, Jie Qin, Chensheng Cai, Fanwei Meng and Aiping Pang
Mathematics 2025, 13(23), 3748; https://doi.org/10.3390/math13233748 - 21 Nov 2025
Viewed by 240
Abstract
As a high-precision and high-stability engineering platform for aerospace missions, the dual-super spacecraft is subject to numerous environmental constraints and disturbances in increasingly complex space environments, posing significant challenges to its attitude maneuvering process. Unlike traditional spacecraft, the dual-super spacecraft consists of two [...] Read more.
As a high-precision and high-stability engineering platform for aerospace missions, the dual-super spacecraft is subject to numerous environmental constraints and disturbances in increasingly complex space environments, posing significant challenges to its attitude maneuvering process. Unlike traditional spacecraft, the dual-super spacecraft consists of two cabins: a payload cabin and a platform cabin, with a magnetic levitation mechanism installed between them to prevent vibration transmission. This paper establishes a multi-coupled attitude model for the payload cabin, the platform cabin, and the magnetic levitation mechanism between them. Additionally, a collision avoidance control strategy is designed for the magnetic levitation mechanism to ensure the operational safety of the entire system. To address the external environmental constraints, a closed-loop dual-loop control framework is proposed for the payload cabin. The outer-loop performs stability control on the payload cabin, while the inner-loop employs explicit reference governor (ERG) to handle pointing constraints. The platform cabin follows the attitude control of the payload cabin, forming a master–slave coordinated control scheme. Simulation results demonstrate that the proposed multi-coupled control system framework performs effectively, ensuring both the satisfaction of pointing constraints and the operational safety of the dual-super spacecraft system. Full article
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