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Simple PID Parameter Tuning Method Based on Outputs of the Closed Loop System 被引量:12
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作者 HAN Jianda ZHU Zhiqiang +1 位作者 jiang ziya HE Yuqing 《Chinese Journal of Mechanical Engineering》 SCIE EI CAS CSCD 2016年第3期465-474,共10页
Most of the existing PID parameters tuning methods are only effective with pre-known accurate system models, which often require some strict identification experiments and thus infeasible for many complicated systems.... Most of the existing PID parameters tuning methods are only effective with pre-known accurate system models, which often require some strict identification experiments and thus infeasible for many complicated systems. Actually, in most practical engineering applications, it is desirable for the PID tuning scheme to be directly based on the input-output response of the closed-loop system. Thus, a new parameter tuning scheme for PID controllers without explicit mathematical model is developed in this paper. The paper begins with a new frequency domain properties analysis of the PID controller. After that, the definition of characteristic frequency for the PID controller is given in order to study the mathematical relationship between the PID parameters and the open-loop frequency properties of the controlled system. Then, the concepts of M-field and θ-field are introduced, which are then used to explain how the PID control parameters influence the closed-loop frequency-magnitude property and its time responses. Subsequently, the new PID parameter tuning scheme, i.e., a group of tuning rules, is proposed based on the preceding analysis. Finally, both simulations and experiments are conducted, and the results verify the feasibility and validity of the proposed methods. This research proposes a PID parameter tuning method based on outputs of the closed loop system. 展开更多
关键词 PID control characteristic frequency step response frequency property
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四旋翼飞行器自适应控制及真实参数估计 被引量:7
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作者 江紫亚 何玉庆 韩建达 《信息与控制》 CSCD 北大核心 2018年第4期455-460,共6页
针对四旋翼飞行器的参数不确定性问题,提出了一种基于线性滤波降阶的自适应跟踪控制策略.通过将四旋翼系统的动力学方程进行姿态和高度解耦,同时进行改写使其满足参数线性化形式,继而设计控制策略和参数自适应更新律.利用李亚普诺夫理... 针对四旋翼飞行器的参数不确定性问题,提出了一种基于线性滤波降阶的自适应跟踪控制策略.通过将四旋翼系统的动力学方程进行姿态和高度解耦,同时进行改写使其满足参数线性化形式,继而设计控制策略和参数自适应更新律.利用李亚普诺夫理论对闭环系统进行稳定性分析,保证了轨迹跟踪误差及其导数渐近收敛.同时,从系统辨识的角度对参数估计的收敛性问题进行分析.通过与基于标称模型设计的反馈线性化控制器进行对比,验证了所提控制方法的有效性.仿真结果表明,在满足持续激励条件的情况下,参数能够收敛到真实值. 展开更多
关键词 四旋翼 自适应 跟踪控制 参数辨识
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