存在时滞的柔性梁的振动主动控制

本文对控制存在时滞的柔性梁的振动主动控制进行研究.主动控制策略采用独立模态空间控制,模态控制律采用离散变结构控制进行设计.给出了从实际测量中提取模态坐标和将模态控制力转换成实际控制力的方法,以及离散切换面和离散变结构模态控制律的确定方法.由于模态控制律直接通过时滞微分方程而得出,因此所给控制方法易于保证控制系统的稳定性.算例结果显示,文中所述控制方法能够有效地对梁的振动进行控制;若按无时滞时的控制设计对时滞系统进行控制,系统响应有可能出现发散.     

柔性机械臂的时滞最优跟踪控制

采用最优跟踪控制方法对柔性机械臂线性化主动控制中的时滞问题进行研究。首先采用一种积分变换,将包含时滞项的动力学方程转换成形式上不包含时滞项的标准形式,然后根据最优跟踪控制理论设计控制律。在每一步控制律的计算中,不但包含有当前步的状态反馈,而且包含有前若干步控制的线性组合。文中还给出了一个模态坐标的提取方法。仿真结果显示,若对时滞不处理,控制系统会在很小时滞量时出现发散;当控制系统中的时滞量不大时,本文的线性化时滞控制设计能够取得较好的控制效果;当系统存在较大时滞量时,线性化时滞控制设计的有效范围是有限的。     

带有末端集中质量的双连杆柔性机械臂主动控制

对带有末端集中质量的双连杆柔性机械臂的主动控制进行了研究,给出系统的动力学方程,采用非线性解耦反馈控制方法分别得出系统大范围运动方程和柔性臂的动力学方程,采用机械臂逆动力学方法和LQR方法分别设计大范围运动控制律和压电作动器控制律.仿真结果显示,本文控制方法能够有效地进行机械臂的轨迹跟踪,柔性臂的弹性振动可以得到有效抑制.     

不确定线性时滞系统模型参考自适应控制研究

以具有不确定参数和时滞的线性时滞系统为对象,开展时滞系统的模型参考自适应控制研究。首先利用时滞控制力项的差分方程对系统的状态变量进行增广,将时滞系统动力学方程变为形式上不含有时滞项的增广状态方程。然后根据时滞系统动力学方程和已确定的参数建立相应参考模型,并采用线性二次调节器(LQR)设计参考模型控制律,以保证闭环参考模型系统稳定。最后基于参考模型的LQR控制律,采用基于类观测器的模型参考自适应控制方法设计相应的自适应控制律。因此,针对原时滞系统动力学方程,本文所设计的时滞控制律由LQR控制律和自适应控制律两部分组成。数值仿真结果表明:本文所使用的基于LQR的自适应控制方法在系统参数和时滞不确定的情况下,能够有效地跟踪稳定的参考模型的动力学行为,从而对系统进行控制。该方法可以作为LQR控制方法的有益补充,进一步改善控制系统的动力学行为。     

控制存在延时的建筑结构地震作用下的最优控制方法

直接从时滞微分方程进行控制律设计,对控制存在延时的建筑结构在地震作用下的最优控制方法进行了研究。在控制时滞量为采样周期的整数倍和非整数倍的两种情况下,通过采用零阶保持器,将包含时滞的连续系统转化为形式上不包含时滞的标准离散线性系统,然后进行控制律的设计。所得出的控制律表达式中,除了含有当前的状态反馈外,还包含有前若干步控制项的线形组合。最后对某三自由度结构模型进行了仿真计算,结果表明,延时对控制效果有较大的影响,延时并非愈短愈好。     

控制存在时滞的线性系统主动控制的滑移模态方法

本文研究控制存在时滞的线性系统的滑模控制方法。在控制时滞量为采样周期的整数倍和非整数倍的两种情况下，通过采用零阶保持器，将包含时滞的连续系统转化为形式上不包含时滞的标准离散线性系统，然后分别进行切换函数和控制律的设计。所得出的切换面和控制律表达式中，除了含有当前的状态反馈外，还包含有前若干步控制项的线形组合。最后对某三自由度结构模型进行仿真计算，验证了所给控制方法的有效性。     

线性时滞系统的离散最优控制

介绍了对线性时滞系统进行最优控制的设计,将具有时滞控制的线性系统离散后引入增广状态向量。获得不显含时滞的差分方程,根据时滞量的两种分类情况采用连续和离散形式的性能指标函数导出了最优控制律。控制律包含当前状态和此前若干步状态向量的叠加,最优控制律直接从时滞方程中得到,可保证系统的稳定性,此方法亦适用于大时滞的情况。数值算例验证了控制策略的有效性。     

考虑时滞的主动悬架系统控制策略对比研究全文替换

本文以二自由度四分之一汽车悬架系统为研究对象,采用不同控制策略对考虑时滞的悬架系统控制特性进行研究,并对控制效果进行对比分析．首先,采用第二类拉氏方程建立考虑时滞的二自由度悬架控制系统的动力学模型;然后分别基于状态变换法和H_∞控制理论,设计系统的时滞反馈控制律．其中状态变换法主要通过系统状态变量的转换,将系统时滞控制方程转换成不显含时滞的动力学方程,然后采用传统的二次型最优控制方法对系统进行控制．H_∞控制主要通过使用Lyapunov-Krasovskii泛函和自由权矩阵法,设计考虑时滞的H_∞控制律;最后在Matlab/Simulink平台上对控制系统进行仿真分析,并在相同时滞下对两种控制结果进行对比．研究表明,两种控制策略在考虑时滞的情况下均可保证系统的稳定性,且H_∞控制相比于状态变换法有更好的控制效果．     

时滞对结构振动半主动控制效果的影响

应用磁流变阻尼器对结构振动进行控制，采用最优控制原理设计了控制器，给出在地震激励下结构半主动控制的仿真计算。研究了时滞对结构振动半主动控制效果的影响。数值结果表明：本文设计的半主动控制策略可有效地减小结构的振动响应，时滞对磁流变半主动控制效果随着时滞的增大而变差，但时滞不会导致该反馈控制系统的失稳。     

旋转运动柔性梁的时滞主动控制实验研究

对旋转运动柔性梁的时滞主动控制进行实验研究,验证时滞反馈控制的有效性. 实验中采用交流伺服电机带动柔性梁旋转运动,柔性梁上粘贴有压电作动器,用于控制梁的弹性振动. 实验研究考虑如下3种情况:(1)仅使用电机扭矩进行控制,电机扭矩存在时滞;(2)使用电机扭矩和压电作动器同时控制,仅压电作动器存在时滞;(3)使用电机扭矩和压电作动器同时控制,电机和压电作动器存在不同的时滞量. 重点通过实验验证时滞反馈控制的可行性和有效性.      

A criterion of robustness intelligent nonlinear control for multiple time-delay systems based on fuzzy Lyapunov methods

A control system with state feedback controllers, in which the fuzzy Lyapunov approach is developed for the stability criterion, is studied. The proposed intelligent design provides a systematic and effective framework for the control systems. The global nonlinear controller is constructed based on T–S (Takagi–Sugeno) fuzzy controller design techniques, blending all such local state feedback controllers. Based on this design, the stability conditions of a multiple time-delay system are derived in terms of the fuzzy Lyapunov theory. The effectiveness and the feasibility of the proposed controller design method are demonstrated through numerical simulations.     

Delayed full-state feedback control of airfoil flutter using sliding mode control method

This paper studies the delayed feedback control of flutter of a two-dimensional airfoil using a sliding mode control (SMC) method. The dynamic equation of airfoil flutter is firstly established using the Lagrange method, in which the cubic hardening spring nonlinearity of pitch stiffness is considered. Then, the state equation with time delay is transformed into a standard state equation with implicit time delay by a special integral transformation. Next a nonlinear time-delay controller is designed using the SMC method. Finally the effectiveness of the proposed controller is verified through numerical simulations. Simulation results indicate that time delay in the control system has significant influence on the control performance. Control failure may happen if time delay is not considered in control design. The time-delay controller proposed is effective in suppressing the airfoil flutter with either small or large control time delay.     

Design method of multiple time-delay controller for active structural vibration control

An optimal control method for seismic-excited building structures with multiple time delays is investigated in this paper. The system state equation with multiple time delays is discretized and transformed into a standard discrete form without any explicit time delay by a particular augmenting for state variables. A time-delay controller is then designed based on this standard equation using the discrete optimal control method. Effectiveness of the proposed controller is demonstrated by numerical simulations. Simulation results indicate that a very small time delay may result in the instability of the control system if it is not compensated in the control design. Time delay may be compensated effectively by the proposed controller, in the mean time, an effective control may be obtained. The proposed controller is valid for both small and large time delays.     

Stabilization control for offshore steel jacket platforms with actuator time-delays

This paper is concerned with the stabilization control for the offshore steel jacket platforms subject to wave-induced force. Two state feedback stabilization control schemes are proposed to reduce the vibration amplitudes of the systems. One scheme is that for the systems without actuator time-delay, a state feedback controller is designed. Compared with the nonlinear controller, both the control force and the vibration amplitudes of the systems under the state feedback controller are much reduced; and compared with the dynamic output feedback controller and the integral sliding mode controller, the required control force under the state feedback controller are significantly reduced. The other scheme is that based on the integral inequality approach, a delay-dependent state feedback controller, which can be solved by using the cone complementarity algorithm, is developed to control the systems with actuator time-delays. Compared with the state feedback controller, the delay-dependent state feedback controller is less conservative with actuator time-delays. In addition, it is capable of improving the control performance of the offshore platforms significantly, which are illustrated by simulation results.     

Design and experimental verification of multiple delay feedback control for time-delay nonlinear oscillators

This study aims to show that a multiple delay feedback control method can stabilize unstable fixed points of time-delay nonlinear oscillators. The boundary curves of stability in a control parameter space are derived using linear stability analysis. A simple procedure for designing a feedback gain is provided. The main advantage of this procedure is that the designed controller can stabilize a system even if the controller delay times are long. These analytical results are experimentally verified using electronic circuits.     

Pure delayed non-fragile control for offshore steel jacket platforms subject to non-linear self-excited wave force

This paper is concerned with pure delayed non-fragile control for an offshore steel jacket platform subject to non-linear self-excited wave force. By purposefully introducing a proper time-delay into control channel, a pure delayed non-fragile controller (DNFC) is proposed to improve performance of the offshore steel jacket platform. The positive effects of time-delays on non-fragile stabilization control for the system are investigated. It is shown through simulation results that (i) the DNFC and the delay-free non-fragile controller are capable of attenuating the vibration of the offshore platform to almost the same level, while the required control force under the DNFC is less than that under the delay-free one; and (ii) both the oscillation amplitudes of the offshore platform and the ranges of the control force under the pure delayed state feedback controller (DSFC) are smaller than the ones under the non-linear controller and the dynamic output feedback controller; and (iii) the oscillation amplitudes of the offshore platform under the DSFC are almost the same as the ones under integral sliding mode controller and the delayed dynamic output feedback controller, while the control force required by the former is less than the one by the latter.     

Active control of time-delay in cutting vibration

The system dynamics of turning processes can be described by a delay differential equation. How to improve the stability and suppress the vibration of cutting is of an interesting topic. In this paper, a multiple time-delay controller is developed based on discrete optimal control method for the turning vibrations control. Numerical simulations are carried out to verify the efficiency of the controller. Results indicate the designed controller can suppress the cutting vibration efficiently and improve the stability of the cutting processes. The influence of designed time-delay and sampling time on the control performance is also discussed.