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航空发动机多变量模糊滑模变结构模型跟踪控制 被引量:14
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作者 蔡开龙 谢寿生 《推进技术》 EI CAS CSCD 北大核心 2008年第6期737-742,共6页
针对现代航空发动机是一个具有不确定性的强非线性系统,结合滑模变结构控制和模糊逻辑系统的优点,提出了一种模糊滑模变结构模型跟踪控制方法。采用比例积分型切换超平面设计滑模变结构控制系统,使用模糊逻辑系统自适应调节切换增益,得... 针对现代航空发动机是一个具有不确定性的强非线性系统,结合滑模变结构控制和模糊逻辑系统的优点,提出了一种模糊滑模变结构模型跟踪控制方法。采用比例积分型切换超平面设计滑模变结构控制系统,使用模糊逻辑系统自适应调节切换增益,得到某涡扇发动机的模糊滑模变结构模型跟踪控制器。数字仿真结果表明,所设计的控制器不但能使被控对象较好地跟踪参考模型,消除抖振现象,而且对系统的不确定性具有不变性,保证了被控系统在整个控制阶段都具有较强的鲁棒性。 展开更多
关键词 航空发动机 ^控制系统^+ ^模糊控制^+ ^滑模结构控制^+ 模型
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Optimal variable structure control with sliding modes for unstable processes 被引量:4
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作者 KUMAR Satyendra AJMERI Moina 《Journal of Central South University》 SCIE EI CAS CSCD 2021年第10期3147-3158,共12页
In this work,a variable structure control(VSC)technique is proposed to achieve satisfactory robustness for unstable processes.Optimal values of unknown parameters of VSC are obtained using Whale optimization algorithm... In this work,a variable structure control(VSC)technique is proposed to achieve satisfactory robustness for unstable processes.Optimal values of unknown parameters of VSC are obtained using Whale optimization algorithm which was recently reported in literature.Stability analysis has been done to verify the suitability of the proposed structure for industrial processes.The proposed control strategy is applied to three different types of unstable processes including non-minimum phase and nonlinear systems.A comparative study ensures that the proposed scheme gives superior performance over the recently reported VSC system.Furthermore,the proposed method gives satisfactory results for a cart inverted pendulum system in the presence of external disturbance and noise. 展开更多
关键词 variable structure control sliding mode control Whale optimization algorithm ROBUSTNESS non-linear system
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Sliding mode identifier for parameter uncertain nonlinear dynamic systems with nonlinear input 被引量:2
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作者 张克勤 庄开宇 +2 位作者 苏宏业 褚健 高红 《Journal of Zhejiang University Science》 CSCD 2002年第4期426-430,共5页
This paper presents a sliding mode (SM) based identifier to deal with the parameter identification problem for a class of parameter uncertain nonlinear dynamic systems with input nonlinearity. A sliding mode controlle... This paper presents a sliding mode (SM) based identifier to deal with the parameter identification problem for a class of parameter uncertain nonlinear dynamic systems with input nonlinearity. A sliding mode controller (SMC) is used to ensure the global reaching condition of the sliding mode for the nonlinear system; an identifier is designed to identify the uncertain parameter of the nonlinear system. A numerical example is studied to show the feasibility of the SM controller and the asymptotical convergence of the identifier. 展开更多
关键词 Nonlinear system Sliding mode IDENTIFIER Input nonlinearity
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A new PMSM speed modulation system with sliding mode based on active-disturbance-rejection control 被引量:11
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作者 荣智林 黄庆 《Journal of Central South University》 SCIE EI CAS CSCD 2016年第6期1406-1415,共10页
A sliding mode and active disturbance rejection control(SM-ADRC)was employed to regulate the speed of a permanent magnet synchronous motor(PMSM).The major advantages of the proposed control scheme are that it can main... A sliding mode and active disturbance rejection control(SM-ADRC)was employed to regulate the speed of a permanent magnet synchronous motor(PMSM).The major advantages of the proposed control scheme are that it can maintain the original features of ADRC and make the parameters of ADRC transition smoothly.The proposed control scheme also ensures speed control accuracy and improves the robustness and anti-load disturbance ability of the system.Moreover,through the analysis of a d-axis current output equation,a novel current-loop SM-ADRC is presented to improve the system’s dynamic performance and inner ability of anti-load disturbance.Results of a simulation and experiments show that the improved sliding-mode ADRC system has the advantages of fast response,small overshoot,small steady-state error,wide speed range and high control accuracy.It shows that the system has strong anti-interference ability to reduce the influence of variations in rotational inertia,load and internal parameters. 展开更多
关键词 disturbance rejection auto tuning permanent magnet synchronous motor speed modulation system
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Fuzzy Sliding Mode Control for a Discrete Servo System
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作者 王传江 孙秀娟 《Journal of Measurement Science and Instrumentation》 CAS 2011年第1期81-83,共3页
A discrete fuzzy sliding mode variable structure controller was studied and designed for a class of electro-hydraulic servo system by means of the combination of sliding mode control theory and fuzzy control theory. D... A discrete fuzzy sliding mode variable structure controller was studied and designed for a class of electro-hydraulic servo system by means of the combination of sliding mode control theory and fuzzy control theory. Designed based on the exponential reaching law, paratmter e of conventional sliding mode controller is the key factor of system chattering, and is ~onal to it as well. In view of this, fuzzy control theory was introduced into the design to ensure the real- time adjusting of parameter e. Sinmlation results show that the sys tem chattering is eliminated perfectly, and the dynamic performance of the control system is improved effectively. 展开更多
关键词 sliding mate control fuzzy control reaching law servo system
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Research on hovering control scheme to non-circular orbit 被引量:2
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作者 WANG GongBo ZHENG Wei +1 位作者 MENG YunHe TANG GuoJian 《Science China(Technological Sciences)》 SCIE EI CAS 2011年第11期2974-2980,共7页
An open-loop control system for hovering at any selected position on spacecraft orbit is first presented given that the satellite's engine provides continuous finite thrust. Actually, the hovering states are unstable... An open-loop control system for hovering at any selected position on spacecraft orbit is first presented given that the satellite's engine provides continuous finite thrust. Actually, the hovering states are unstable considering perturbations and thrust errors, so a feedback sliding mode variable structure control, which is adaptive and chattering-free, is designed. Under this feedback control scheme, the high-frequency chattering phenomenon is avoided, while the system stays highly robust at the same time. Simulation results show that the feedback control thrusts are continuous and the steady-states error can be confmed to 10-4 m at the presence of uncertain perturbations. Finally, the feasibility of realizing hovering orbits is analyzed taking the "Moliya" and geosynchronous Earth orbit (GEO) satellites as examples. 展开更多
关键词 continuous finite thrust hovering orbit chattering-free variable structure control
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