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控制系统鲁棒性的计算机辅助分析方法
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作者 慕春棣 陈德刚 高龙 《控制理论与应用》 EI CAS 1986年第4期109-114,共6页
本文以强抗扰恒值系统为例,说明对控制系统鲁棒性的计算机辅助分析方法。该方法比较容易找出参数摄动对系统稳定性及其性能指标的影响,并且可以找出参数的稳定域来。计算机辅助分析方法可以克服理论分析上的困难,并且可以避免线性化所... 本文以强抗扰恒值系统为例,说明对控制系统鲁棒性的计算机辅助分析方法。该方法比较容易找出参数摄动对系统稳定性及其性能指标的影响,并且可以找出参数的稳定域来。计算机辅助分析方法可以克服理论分析上的困难,并且可以避免线性化所带来的误差,与辅助设计结合在一起,对工业控制系统的设计和实际调整具有一定的指导意义。 展开更多
关键词 计算机辅助分析 恒值系统 抗扰 计算机辅助技术 控制系统鲁棒性 伺服补偿器 性能指标 参数摄动 系统参数 反馈控制
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基于改进DDPG的变速抽蓄机组参与系统调频研究 被引量:1
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作者 劳文洁 史林军 +3 位作者 王伟 杨冬梅 吴峰 林克曼 《太阳能学报》 EI CAS CSCD 北大核心 2024年第3期240-250,共11页
在挖掘双馈型抽水蓄能(DFIM-PSH)机组调频能力的基础上,提出一种基于改进深度确定性策略梯度(DDPG)算法的系统频率控制方法。首先,基于所确定的DFIM-PSH机组在发电与抽水工况下的频率控制环节,构建考虑风电接入的含DFIMPSH单区域系统频... 在挖掘双馈型抽水蓄能(DFIM-PSH)机组调频能力的基础上,提出一种基于改进深度确定性策略梯度(DDPG)算法的系统频率控制方法。首先,基于所确定的DFIM-PSH机组在发电与抽水工况下的频率控制环节,构建考虑风电接入的含DFIMPSH单区域系统频率控制模型。其次,在考虑机组运行约束的基础上以最小化系统频率偏差及调频出力为目标,引入DDPG算法对各机组的AGC控制指令进行优化。通过在预学习中同时引入随机外部扰动与模型参数变化,提高AGC控制器在具有强不确定性环境中的适应性。最后,在仿真验证DFIM-PSH调频优势的基础上,在不同风电接入及扰动等多场景进行仿真分析,结果表明,所提频率控制方法能有效改善新型电力系统的频率特性且具有强鲁棒性。 展开更多
关键词 抽水蓄能机组 鲁棒性(控制系统) 频率控制 深度确定性策略梯度算法 新型电力系统
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高超声速飞行器鲁棒舵回路控制器设计 被引量:1
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作者 王鑫 冯冬竹 《西北工业大学学报》 EI CAS CSCD 北大核心 2009年第5期641-644,共4页
文章针对高超声速飞行器在缺少实际试飞数据的情况下,需要设计鲁棒自动驾驶仪的舵回路控制器来保证飞行器的姿态角控制精度满足超燃冲压发动机的工作条件。根据高超声速飞行器横滚通道的动态特性,针对舵回路的死区间隙等非线性不确定性... 文章针对高超声速飞行器在缺少实际试飞数据的情况下,需要设计鲁棒自动驾驶仪的舵回路控制器来保证飞行器的姿态角控制精度满足超燃冲压发动机的工作条件。根据高超声速飞行器横滚通道的动态特性,针对舵回路的死区间隙等非线性不确定性因素,结合滚动通道数学模型,采用Lyapunov方法设计了横滚通道差动舵的鲁棒控制器。其鲁棒控制律对系统参数不确定性和外界干扰不确定性的补偿控制采用差动舵偏补偿算法,自动补偿不确定因素及舵回路死区、饱和的非线性影响,并完成了其鲁棒指数镇定的证明。最后通过数字仿真验证了文中控制算法的有效性。 展开更多
关键词 控制系统鲁棒性 高超声速飞行器 鲁棒舵回路控制
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一种有效的高速攻击型无人机二自由度PID控制 被引量:2
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作者 耿峰 祝小平 +1 位作者 周洲 孟俊生 《西北工业大学学报》 EI CAS CSCD 北大核心 2013年第1期1-7,共7页
高速攻击型无人机的飞行控制系统需要具有最佳的指令跟踪性能、干扰抑制性能和鲁棒性,而传统单自由度PID控制技术只有1组PID参数,无法同时满足上述设计要求,针对这一问题,采用给定值滤波器型二自由度微分先行PID控制技术。通过利用基于... 高速攻击型无人机的飞行控制系统需要具有最佳的指令跟踪性能、干扰抑制性能和鲁棒性,而传统单自由度PID控制技术只有1组PID参数,无法同时满足上述设计要求,针对这一问题,采用给定值滤波器型二自由度微分先行PID控制技术。通过利用基于改进的粒子群优化算法的H∞参数整定方法进行微分先行PID控制器设计,保证系统"干扰抑制性能及鲁棒性最佳",通过调节二自由度化系数(给定值滤波器设计),确保系统"指令跟踪性能最佳"。以俯仰控制回路设计为例,经仿真与对比研究,结果表明,该控制技术克服了单自由度PID控制技术的不足,控制回路的控制品质满足设计要求。 展开更多
关键词 约束最优化 自由度(力学) 扰动抑制 飞行控制系统 纵向控制 多目标优化 粒子群 优化 鲁棒性(控制系统) 示意图 无人机 微分先行 PID控制
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欠驱动四旋翼飞行器反演模糊自适应控制 被引量:6
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作者 杨立本 章卫国 +1 位作者 黄得刚 车军 《西北工业大学学报》 EI CAS CSCD 北大核心 2015年第3期495-499,共5页
针对欠驱动四旋翼飞行器的结构特性,提出一种自适应模糊反演欠驱动控制算法,该算法可以克服传统反演控制中存在的问题,如欠驱动控制律过于复杂,抗干扰能力弱及系统建模误差对跟踪性能影响较大等弱点,该算法利用自适应模糊系统逼近系统... 针对欠驱动四旋翼飞行器的结构特性,提出一种自适应模糊反演欠驱动控制算法,该算法可以克服传统反演控制中存在的问题,如欠驱动控制律过于复杂,抗干扰能力弱及系统建模误差对跟踪性能影响较大等弱点,该算法利用自适应模糊系统逼近系统中的非线性函数及扰动项,并利用模糊系统来构造系统的虚拟控制量,从而实现对欠驱动四旋翼飞行器的高精度控制,并以欠驱动四旋翼飞行器的自由度x为例,详细论述了自适应模糊系统的设计过程,并对算法的收敛性做了分析,仿真结果表明,该算法具有很强的抗干扰性,并且达到了理想的控制精度。 展开更多
关键词 执行器 自适应控制系统 算法 飞行器 角速度 反步 计算机仿真 控制器设计 误差 模糊控制 干扰抑制 李雅普诺夫方程 数学模型 鲁棒性(控制系统) 示意图 稳定性 无人机 自适应模糊系统 抗干扰 建模误差 欠驱动飞行器
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A practical robust nonlinear controller for maglev levitation system 被引量:5
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作者 李金辉 李杰 张耿 《Journal of Central South University》 SCIE EI CAS 2013年第11期2991-3001,共11页
In order to explore the precise dynamic response of the maglev train and verify the validity of proposed controller,a maglev guideway-electromagnet-air spring-cabin coupled model is developed in the first step.Based o... In order to explore the precise dynamic response of the maglev train and verify the validity of proposed controller,a maglev guideway-electromagnet-air spring-cabin coupled model is developed in the first step.Based on the coupled model,the stresses of the modules are analyzed,and it is pointed out that the inherent nonlinearity,the inner coupling,misalignments between the sensors and actuators,and external disturbances are the main issues that should be considered for the maglev engineering.Furthermore,a feedback linearization controller based on the mathematical model of a maglev module is derived,in which the nonlinearity,coupling and misalignments are taken into account.Then,to attenuate the effect of external disturbances,a disturbance observer is proposed and the dynamics of the estimation error is analyzed using the input-to-state stability theory.It shows that the error is negligible under a low-frequency disturbance.However,at the high-frequency range,the error is unacceptable and the disturbances can not be compensated in time,which lead to over designed fluctuations of levitation gap,even a clash between the upper surface of electromagnet and lower surface of guideway.To solve this problem,a novel nonlinear acceleration feedback is put forward to enhancing the attenuation ability of fast varying disturbances.Finally,numerical comparisons show that the proposed controller outperforms the traditional feedback linearization controller and maintains good robustness under disturbances. 展开更多
关键词 dynamic robust nonlinear DECOUPLING separation levitation system MAGLEV
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A new semi-active suspension control strategy through mixed H_2/H_∞ robust technique 被引量:2
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作者 郑玲 李以农 陈兵奎 《Journal of Central South University》 SCIE EI CAS 2010年第2期332-339,共8页
A new semi-active suspension control strategy through mixed H2/H∞ robust technique was developed due to its flexibility and robustness to model uncertainties.A full car model with seven degrees of freedom was establi... A new semi-active suspension control strategy through mixed H2/H∞ robust technique was developed due to its flexibility and robustness to model uncertainties.A full car model with seven degrees of freedom was established to demonstrate the effectiveness of the new control approach.Magneto-rheological(MR) dampers were designed,manufactured and characterized as available semi-active actuators in the developed semi-active suspension system.The four independent mixed H2/H∞ controllers were devised in order to perform a distributed semi-active control system in the vehicle by which the response velocity and reliability can be improved significantly.The performance of the proposed new approach was investigated in time and frequency domains.A good balance between vehicle's comfort and road holding was achieved.An effective and practical control strategy for semi-active suspension system was thus obtained.This new approach exhibits some advantages in implementation,performance flexibility and robustness compared to existing methods. 展开更多
关键词 mixed H2/H∞ control semi-active suspension magneto-rheological (MR) damper linear matrix inequality (LMI)
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Fuzzy robust sliding mode control of a class of uncertain systems 被引量:7
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作者 REN Li-tong 《Journal of Central South University》 SCIE EI CAS CSCD 2016年第9期2296-2304,共9页
Aiming at a class of systems under parameter perturbations and unknown external disturbances, a method of fuzzy robust sliding mode control was proposed. Firstly, an integral sliding mode surface containing state feed... Aiming at a class of systems under parameter perturbations and unknown external disturbances, a method of fuzzy robust sliding mode control was proposed. Firstly, an integral sliding mode surface containing state feedback item was designed based on robust H∞ control theory. The robust state feedback control was utilized to substitute for the equivalent control of the traditional sliding mode control. Thus the robustness of systems sliding mode motion was improved even the initial states were unknown. Furthermore, when the upper bound of disturbance was unknown, the switching control logic was difficult to design, and the drawbacks of chattering in sliding mode control should also be considered simultaneously. To solve the above-mentioned problems, the fuzzy nonlinear method was applied to approximate the switching control term. Based on the Lyapunov stability theory, the parameter adaptive law which could guarantee the system stability was devised. The proposed control strategy could reduce the system chattering effectively. And the control input would not switch sharply, which improved the practicality of the sliding mode controller. Finally, simulation was conducted on system with parameter perturbations and unknown external disturbances. The result shows that the proposed method could enhance the approaching motion performance effectively. The chattering phenomenon is weakened, and the system possesses stronger robustness against parameter perturbations and external disturbances. 展开更多
关键词 uncertain systems robust control fuzzy sliding mode control CHATTERING
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Linearization of T-S fuzzy systems and robust H_∞ control 被引量:4
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作者 YOON Tae-Sung 王法广 +2 位作者 PARK Seung-Kyu KWAK Gun-Pyong AHN Ho-Kyun 《Journal of Central South University》 SCIE EI CAS 2011年第1期140-145,共6页
Takagi-Sugeno(T-S) fuzzy model is difficult to be linearized because of membership functions included.So,novel T-S fuzzy state transformation and T-S fuzzy feedback are proposed for the linearization of T-S fuzzy syst... Takagi-Sugeno(T-S) fuzzy model is difficult to be linearized because of membership functions included.So,novel T-S fuzzy state transformation and T-S fuzzy feedback are proposed for the linearization of T-S fuzzy system.The novel T-S fuzzy state transformation is the fuzzy combination of local linear transformation which transforms local linear models in the T-S fuzzy model into the local linear controllable canonical models.The fuzzy combination of local linear controllable canonical model gives controllable canonical T-S fuzzy model and then nonlinear feedback is obtained easily.After the linearization of T-S fuzzy model,a robust H∞ controller with the robustness of sliding model control(SMC) is designed.As a result,controlled T-S fuzzy system shows the performance of H∞ control and the robustness of SMC. 展开更多
关键词 T-S fuzzy control LINEARIZATION H∞ control sliding mode control
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H∞ control of novel active steering integrated with electric power steering function 被引量:8
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作者 ZHAO Wan-zhong LI Yi-jun +2 位作者 WANG Chun-yan ZHAO Ting GU Xiao-yue 《Journal of Central South University》 SCIE EI CAS 2013年第8期2151-2157,共7页
Based on the traditional active steering system, a novel active steering system integrated with electric power steering function was introduced, which can achieve the functions of both active steering and electric pow... Based on the traditional active steering system, a novel active steering system integrated with electric power steering function was introduced, which can achieve the functions of both active steering and electric power steering. In view of the interference from road random signal and sensor noise in the novel active steering system, the H∞ control model of the novel active steering system was built. With satisfying steering feel, good robust performance and steering stability being the control objectives, the H∞ controller for the novel active front steering (AFS) system was designed. The simulation results show that the novel AFS system with H∞ control strategy can attenuate the road interference quickly, and there is no resonance peak in the bode diagram. It can make the driver obtain more useful information in the low frequency range, and attenuate the road interference better in the high frequency range, thus the driver can get more satisfying road feeling. Therefore, the designed H∞ controller can synthesize the advantages of both robust performance and robust stability, and has certain contribution to the design of novel AFS system. 展开更多
关键词 vehicle engineering active steering electric power steering H∞ control
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Robust H_∞ directional control for a sampled-data autonomous airship 被引量:2
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作者 王曰英 王全保 +1 位作者 周平方 段登平 《Journal of Central South University》 SCIE EI CAS 2014年第4期1339-1346,共8页
A robust H∞ directional controller for a sampled-data autonomous airship with polytopic parameter uncertainties was proposed. By input delay approach, the linearized airship model was transformed into a continuous-ti... A robust H∞ directional controller for a sampled-data autonomous airship with polytopic parameter uncertainties was proposed. By input delay approach, the linearized airship model was transformed into a continuous-time system with time-varying delay. Sufficient conditions were then established based on the constructed Lyapunov-Krasovskii functional, which guarantee that the system is mean-square exponentially stable with H∞ performance. The desired controller can be obtained by solving the obtained conditions. Simulation results show that guaranteed minimum H∞ performance γ=1.4037 and fast response of attitude for sampled-data autonomous airship are achieved in spite of the existence of parameter uncertainties. 展开更多
关键词 autonomous airship H∞ directional control sampled-data system polytopic parameter uncertainty Lyapunov-Krasovskii functional
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