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A new 4-D hyperchaotic four-wing system, its bifurcation analysis, complete synchronization and circuit simulation 一种新型四维超混沌四翼系统及其分岔分析、完全同步和电路仿真
4区 计算机科学 Q4 AUTOMATION & CONTROL SYSTEMS Pub Date : 2023-11-06 DOI: 10.24425/acs.2022.142847
In this work, we modify the dynamics of 3-D four-wing Li chaotic system (Li et al. 2015) by introducing a feedback controller and obtain a new 4-D hyperchaotic four-wing system with complex properties. We show that the new hyperchaotic four-wing system have three saddle-foci balance points, which are unstable. We carry out a detailed bifurcation analysis for the new hyperchaotic four-wing system and show that the hyperchaotic four-wing system has multistability and coexisting attractors. Using integral sliding mode control, we derive new results for the master-slave synchronization of hyperchaotic four-wing systems. Finally, we design an electronic circuit using MultiSim for real implementation of the new hyperchaotic four-wing system.
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引用次数: 0
146963 146963
4区 计算机科学 Q4 AUTOMATION & CONTROL SYSTEMS Pub Date : 2023-09-13 DOI: 10.24425/acs.2023.146963
We build a mathematical game model of pandemic transmission, including vaccinations of population and budget costs of different acting to eliminate pandemic. We assume the interactions among different groups: vaccinated, susceptible, exposed, infectious, super-spreaders, hospitalized and fatality, defining a system of ordinary differential equations, which describes compartment model of disease and costs of the treatment. The goal of the game is to describe the development disease under different types of treatment, but including costs of them and social restrictions, during the shortest time period. To this effect we construct a dual dynamic programming method to describe open-loop Nash equilibrium for treatment, a group of people having antibodies and budget costs. Next, we calculate numerically an approximate open-loop Nash equilibrium.
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引用次数: 0
146962 146962
4区 计算机科学 Q4 AUTOMATION & CONTROL SYSTEMS Pub Date : 2023-09-13 DOI: 10.24425/acs.2023.146962
We investigate a scalar characteristic exponential polynomial with complex coefficients associated with a first order scalar differential-difference equation. Our analysis provides necessary and sufficient conditions for allocation of the roots in the complex open left half-plane what guarantees asymptotic stability of the differential-difference equation. The conditions are expressed explicitly in terms of complex coefficients of the characteristic exponential polynomial, what makes them easy to use in applications. We show examples including those for retarded PDEs in an abstract formulation.
{"title":"146962","authors":"","doi":"10.24425/acs.2023.146962","DOIUrl":"https://doi.org/10.24425/acs.2023.146962","url":null,"abstract":"We investigate a scalar characteristic exponential polynomial with complex coefficients associated with a first order scalar differential-difference equation. Our analysis provides necessary and sufficient conditions for allocation of the roots in the complex open left half-plane what guarantees asymptotic stability of the differential-difference equation. The conditions are expressed explicitly in terms of complex coefficients of the characteristic exponential polynomial, what makes them easy to use in applications. We show examples including those for retarded PDEs in an abstract formulation.","PeriodicalId":48654,"journal":{"name":"Archives of Control Sciences","volume":"32 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2023-09-13","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"134990167","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":4,"RegionCategory":"计算机科学","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}
引用次数: 1
146956 146956
4区 计算机科学 Q4 AUTOMATION & CONTROL SYSTEMS Pub Date : 2023-09-13 DOI: 10.24425/acs.2023.146956
In this article, we extended the concept of controllability, traditionally used to control the final state of a system, to the exact control of its final speed. Inspired by Kalman’s theory, we have established some conditions to characterize the control that allows the system to reach a desired final speed exactly. When the assumptions ensuring speed-controllability are not met, we adopt a regulation strategy that involves determining the control law to make the system’s final speed approach as closely as possible to the predefined final speed, and this at a lower cost. The theoretical results obtained are illustrated through three examples.
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引用次数: 0
Review, design, stabilization and synchronization of fractional-order energy resources demand-supply hyperchaotic systems using Fractional-order PD-based Feedback Control scheme 基于分数阶pd反馈控制方案的分数阶能源供需超混沌系统的评审、设计、稳定与同步
4区 计算机科学 Q4 AUTOMATION & CONTROL SYSTEMS Pub Date : 2023-09-13 DOI: 10.24425/acs.2023.146957
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引用次数: 0
ARL-Wavelet-BPF optimization using PSO algorithm for bearing fault diagnosis 基于粒子群算法的arl -小波- bpf优化轴承故障诊断
4区 计算机科学 Q4 AUTOMATION & CONTROL SYSTEMS Pub Date : 2023-09-13 DOI: 10.24425/acs.2023.146961
Rotating element bearings are the backbone of every rotating machine. Vibration signals measured from these bearings are used to diagnose the health of the machine, but when the signal-to-noise ratio is low, it is challenging to diagnose the fault frequency. In this paper, a new method is proposed to enhance the signal-to-noise ratio by applying the Asymmetric Real Laplace wavelet Bandpass Filter (ARL-wavelet-BPF). The Gaussian function of the ARL-wavelet represents an excellent BPF with smooth edges which helps to minimize the ripple effects. The bandwidth and center frequency of the ARL-wavelet-BPF are optimized using the Particle Swarm Optimization (PSO) algorithm. Spectral kurtosis (SK) of the envelope spectrum is employed as a fitness function for the PSO algorithm which helps to track the periodic spikes generated by the fault frequency in the vibration signal. To validate the performance of the ARL-wavelet-BPF, different vibration signals with low signal-to-noise ratio are used and faults are diagnosed.
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引用次数: 0
146959 146959
4区 计算机科学 Q4 AUTOMATION & CONTROL SYSTEMS Pub Date : 2023-09-13 DOI: 10.24425/acs.2023.146959
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引用次数: 0
146955 146955
IF 1.2 4区 计算机科学 Q4 AUTOMATION & CONTROL SYSTEMS Pub Date : 2023-08-01 DOI: 10.24425/acs.2023.146955
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引用次数: 0
A 4-D chaotic hyperjerk system with a hidden attractor, adaptive backstepping control and circuit design 一种具有隐藏吸引子、自适应反步控制和电路设计的四维混沌超跳系统
IF 1.2 4区 计算机科学 Q4 AUTOMATION & CONTROL SYSTEMS Pub Date : 2023-07-20 DOI: 10.24425/123458
S. Vaidyanathan, Sajad Jafar, V. Pham, A. Azar, F. Alsaadi
A novel 4-D chaotic hyperjerk system with four quadratic nonlinearities is presented in this work. It is interesting that the hyperjerk system has no equilibrium. A chaotic attractor is said to be a hidden attractor when its basin of attraction has no intersection with small neighborhoods of equilibrium points of the system. Thus, our new non-equilibrium hyperjerk system possesses a hidden attractor. Chaos in the system has been observed in phase portraits and verified by positive Lyapunov exponents. Adaptive backstepping controller is designed for the global chaos control of the non-equilibrium hyperjerk system with a hidden attractor. An electronic circuit for realizing the non-equilibrium hyperjerk system is also introduced, which validates the theoretical chaotic model of the hyperjerk system with a hidden chaotic attractor.
提出了一种具有四个二次非线性的新型四维混沌超跳系统。有趣的是,超跳系统不存在平衡。当混沌吸引子的吸引盆与系统平衡点的小邻域不相交时,我们称混沌吸引子为隐吸引子。因此,我们的新非平衡超跳系统具有一个隐藏的吸引子。系统中的混沌已在相图中被观察到,并用正李亚普诺夫指数进行了验证。针对具有隐藏吸引子的非平衡超跳系统的全局混沌控制问题,设计了自适应反步控制器。介绍了一种实现非平衡超跳系统的电子电路,验证了具有隐藏混沌吸引子的超跳系统的理论混沌模型。
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引用次数: 39
Dynamic Contraction Method approach to digital longitudinal aircraft flight controller design 动态收缩法在数字纵向飞机飞行控制器设计中的应用
IF 1.2 4区 计算机科学 Q4 AUTOMATION & CONTROL SYSTEMS Pub Date : 2023-07-20 DOI: 10.24425/acs.2019.127525
R. Czyba, Lukasz Stajer
This paper presents the design of digital controller for longitudinal aircraft model based on the Dynamic Contraction Method. The control task is formulated as a tracking problem of velocity and flight path angle, where decoupled output transients are accomplished in spite of incomplete information about varying parameters of the system and external disturbances. The design of digital controller based on the pseudo-continuous approach is presented, where the digital controller is the result of continuous-time controller discretization. A resulting output feedback controller has a simple form of a combination of low-order linear dynamical systems and a matrix whose entries depend nonlinearly on certain known process variables. Simulation results for an aircraft model confirm theoretical expectations.
提出了一种基于动态收缩法的飞机纵向模型数字控制器的设计方法。该控制任务被表述为速度和航迹角的跟踪问题,在系统参数变化和外部干扰信息不完全的情况下实现了输出瞬态解耦。提出了基于伪连续方法的数字控制器设计,其中数字控制器是连续时间控制器离散化的结果。所得到的输出反馈控制器具有低阶线性动力系统和矩阵的简单组合形式,其条目非线性地依赖于某些已知过程变量。飞机模型的仿真结果证实了理论预期。
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引用次数: 3
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Archives of Control Sciences
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