不确定时滞系统多目标约束下的满意容错控制

针对一类具有不确定参数、干扰输入和时滞特性的非线性系统,研究了当执行器发生故障时的满意容错控制问题。在更实际、更一般的执行器连续增益故障模型下,采用一种含有时滞记忆的状态反馈控制律,分析了鲁棒稳定性能与H∞指标的相容性,并在相容指标约束下,给出了鲁棒H∞满意容错控制器存在的充分条件和设计方法。仿真算例验证了该方法的有效性。     

一类不确定线性系统容错保成本控制器设计

考虑了具有参数不确定性的线性定常系统,研究了带有执行器故障和不确定性扰动的保成本容错控制问题。在考虑更一般、更实际的执行器故障模型的基础上,给出了系统鲁棒稳定及容错保成本控制器存在的充分条件。通过求解代数Ricatti方程完成动态反馈控制器的设计。仿真实例验证了所得结果的可行性。比较不考虑故障的控制器与考虑故障的容错控制器的控制效果,进一步说明了对系统进行容错控制的必要性。     

基于状态多时延模型的NCS鲁棒H_∞容错控制

针对一类具有时变时延和丢包的网络化控制系统,同时考虑模型参数不确定性和外界扰动的影响,基于一种状态多时延模型,以时滞依赖的方法,推证出了确保闭环系统在执行器或传感器发生失效故障时具有鲁棒H∞完整性的判据,并以求解线性或非线性矩阵不等式的方式,给出了鲁棒H∞容错控制器的设计方法。由于模型中考虑了时延下界,且证明过程未进行模型转换和交叉项放大处理,其结果具有较少保守性。最后以一仿真示例验证了所述方法的有效性。     

基于RMMAC的集成主动容错飞行控制

针对主动容错飞行控制系统设计问题,提出一种基于改进鲁棒多模型自适应控制(robust multiplemodel adaptive control,RMMAC)的故障检测与控制重构集成设计方法。建立了飞行器传感器和执行器故障的数学模型,介绍了改进鲁棒多模型自适应控制算法的结构和实现步骤。某无尾飞机重构飞行控制的仿真结果表明,在执行器故障情况下,基于改进RMMAC的集成主动容错飞行控制系统能够快速准确地辨识故障,并依据故障信息更新局部控制器权值,实现控制重构,提高了飞机可靠性、安全性和生存能力。     

基于T-S模型的不确定NNCS鲁棒容错保性能设计

针对一类具有时变时延和丢包的不确定非线性网络化控制系统,基于T-S(Takagi-Sugeno)模糊模型,通过构造适当的Lyapunov-Krasovskii泛函,得出在执行器发生失效故障的情形下,系统基于线性矩阵不等式的渐近稳定且具有良好动态性能的时滞依赖充分条件,并给出了最优鲁棒容错保性能控制器的设计方法。由于证明中没有进行任何模型变换,并考虑了时延下界,使结果具有较少保守性。最后,仿真示例验证了本文所述方法的有效性和可行性。     

基于模糊模型的非线性时滞系统的H∞鲁棒容错控制

研究了一类具有时滞的非线性连续系统的H∞鲁棒容错控制。采用具有时滞的T-S模糊模型,在系统存在执行器失效情况下,设计了状态反馈控制器。基于Lyapunov稳定性理论和LMI方法,给出了在执行器失效的情况下系统稳定的充分条件,保证系统的鲁棒渐近稳定。仿真实例验证了方法的有效性。     

无人机姿控系统鲁棒动态面容错控制设计

针对含有不确定和执行器故障的无人机姿态控制系统,提出了一种鲁棒自适应动态面容错控制方法。在设计中,首先提出由非线性阻尼技术抵消不确定性及外界干扰,然后设计一种基于自适应动态面控制方法的容错控制策略,保证无人机在出现未知执行器故障情况下,其闭环姿态控制系统是全局渐近稳定的,实现姿态输出对制导指令的容错跟踪。最后对所提出的容错控制方法进行了某无人机非线性姿态控制系统的仿真验证, 结果表明了所提方法的有效性。     

一种新型鲁棒容错控制器在飞控系统中的应用

讨论了一种新型的鲁棒容错控制器在飞控系统中的应用。该鲁棒容错控制器由两部分组成,主控制器和补偿控制器。首先,建立了飞机的正常标称模型,通过比较标称模型和实际系统的输出生成残差。在飞机无故障情况下,残差近似为零,仅主控制器作用,保证系统在无故障时具有良好的性能;考虑执行机构故障,飞机发生故障后,故障残差不再为零,补偿控制器以残差为输入,输出补偿控制信号,保证系统稳定,补偿故障对系统的影响。仿真结果表明了该新型鲁棒容错控制器的正确性和可行性。     

Delta算子系统的鲁棒D稳定可靠控制

研究具有执行器故障的Delta算子线性不确定系统鲁棒D-稳定可靠控制问题,即设计控制器,消除系统不确定性和执行器故障的影响,确保闭环系统极点落在复平面指定圆盘区域内。考虑执行器故障为连续故障模型的情形,利用线性矩阵不等式(linear matrix inequality,LMI)方法,给出Delta算子系统状态反馈鲁棒D-稳定可靠控制器存在的充分条件,并由此提出相应控制器设计方法。利用所得结论,给出Delta算子系统状态反馈鲁棒稳定可靠控制器存在的充分条件。数值算例表明设计方法的可行性和有效性。     

具有状态和控制时滞系统的鲁棒容错控制研究

研究一类不确定时滞系统的鲁棒容错控制问题。针对既有状态滞后,又有控制输入滞后,且假定状态和控制输入的不确定项均是范数有界的线性系统,通过引入无记忆状态反馈控制器,基于Lyapunov稳定性理论和LMI方法,给出了一个在传感器完全失效或执行器完全失效故障情况下具有鲁棒容错性能的充分条件,并用求解线性矩阵不等式组方便地得到容错控制器设计结果。最后用算例验证了该设计方法的有效性和可行性。     

基于H∞鲁棒动态逆的飞行器轨迹跟踪方法

利用非线性动态逆方法的精确线性化功能,结合H_∞控制理论,提出了一种阻力加速度能量标准轨迹的跟踪方法。通过动态逆将非线性的高超声速飞行器系统等效为线性对象,继而考虑非结构不确定性及参数不确定性,采用H_∞控制理论设计外回路鲁棒控制器,实现了标准轨迹的精确跟踪,同时给出了闭环系统的鲁棒稳定性证明。仿真结果验证了该方法的有效性。     

离散模糊时滞系统的鲁棒LQ/H∞非脆弱控制

针对一类由T-S模糊模型描述的不确定离散非线性时滞系统,讨论其在控制器存在可加性摄动情形下的鲁棒LQ/H_∞非脆弱控制问题。通过构造适当的Lyapunov函数,给出以线性矩阵不等式形式表示的系统时滞依赖稳定的充分条件以及相应的鲁棒LQ/H_∞非脆弱控制器设计方法。数值仿真表明,所构造的控制器不仅能够保证闭环模糊时滞系统的鲁棒渐近稳定性,还能使系统达到一定的H_∞干扰抑制水平。     

Fault-tolerant control of linear uncertain systems using H∞ robust predictive control

The robust fault-tolerant control problem of linear uncertain systems is studied. It is shown that a solution for this problem can be obtained from a H∞ robust predictive controller （RMPC） by the method of linear matrix inequality （LMI）. This approach has the advantages of both H∞ control and MPC： the robustness and ability to handle constraints explicitly. The robust closed-loop stability of the linear uncertain system with input and output constraints is proven under an actuator and sensor faults condition. Finally, satisfactory results of simulation experiments verify the validity of this algorithm.     

Robust H∞ control for networked control systems

The robust H∞ control for networked control systems with both stochastic network-induced delay and data packet dropout is studied. When data are transmitted over network, the stochastic data packet dropout process can be described by a two-state Markov chain. The networked control systems with stochastic network-induced delay and data packet dropout are modeled as a discrete time Markov jump linear system with two operation modes. The sufficient condition of robust H∞ control for networked control systems stabilized by state feedback controller is presented in terms of linear matrix inequality. The state feedback controller can be constructed via the solution of a set of linear matrix inequalities. An example is given to verify the effectiveness of the method proposed.     

Delay-dependent robust H∞ control for uncertain discrete time-delay fuzzy systems

The robust H∞ control problem of norm bounded uncertain discrete Takagi-Sugeno (T-S) fuzzy systems with state delay is addressed. First, by constructing an appropriate basis-dependent Lyapunov-Krasovskii function, a new delay-dependent sufficient condition on robust H∞-disturbance attenuation is presented, in which both robust stability and prescribed H∞ performance are guaranteed to be achieved. Then based on the condition, a delay-dependent robust H∞ controller design scheme is developed in term of a convex algorithm. Finally, examples are given to illustrate the effectiveness of the proposed method.     

基于LPV的超空泡航行体H∞抗饱和控制

针对超空泡航行体在运动过程中面临的执行器饱和问题,提出一种基于线性变参数(linear parameter varing ,LPV)的抗饱和控制方法。首先在航行体动力学模型基础上考虑执行器饱和非线性因素,将滑行力和执行器分别建模为时变参数的仿射函数,最终得到系统矩阵仿射依赖于时变参数的LPV模型,同时,该模型也考虑了噪声干扰条件下控制器的鲁棒性。基于该LPV模型,运用多面体理论和Lyapunov方法设计了不依赖于时变参数的静态状态反馈控制器。仿真结果表明,所设计的控制器可以保证航行体在执行器发生饱和时仍能渐近跟踪给定深度指令,且在零初始条件下具有对噪声的H∞抑制性能。     

具有时变时延和丢包的网络控制系统H∞优化控制

研究了一类存在时变时延和丢包的网络控制系统(networked control systems, NCS )的H∞优化控制问题。当网络时延和连续丢包有界时,NCS被建模为等效的具有时变时滞的系统,利用Lvapunov Krasovskii泛函和线性矩阵不等式方法,在NCS渐近稳定的基础上给出NCS状态反馈次优和最优H∞控制律的设计方法,求解时不需要使用重复迭代,设计控制器时也无须知道调节参数。仿真表明了此方法的可行性和有效性。     

Robust reliable H∞ control for discrete-time Markov jump linear systems with actuator failures

The robust reliable H∞ control problem for discrete-time Markovian jump systems with actuator failures is studied. A more practical model of actuator failures than outage is considered. Based on the state feedback method, the resulting closed-loop systems are reliable in that they remain robust stochastically stable and satisfy a certain level of H∞ disturbance attenuation not only when all actuators are operational, but also in case of some actuator failures, The solvability condition of controllers can be equivalent to a feasibility problem of coupled linear matrix inequalities （LMIs）. A numerical example is also given to illustrate the design procedures and their effectiveness.     

Sliding mode H∞ control for a class of uncertain nonlinear state-delayed systems

A new proportional-integral (PI) sliding surface is designed for a class of uncertain nonlinear state-delayed systems. Based on this, an adaptive sliding mode controller (ASMC) is synthesized, which guarantees the occurrence of sliding mode even when the system is undergoing parameter uncertainties and external disturbance. The resulting sliding mode has the same order as the original system, so that it becomes easy to solve the H_∞ control problem by designing a memoryless H_∞ state feedback controller. A delay-dependent sufficient condition is proposed in terms of linear matrix inequalities (LMIs), which guarantees the sliding mode robust asymptotically stable and has a noise attenuation level γ in an H_∞ sense. The admissible state feedback controller can be found by solving a sequential minimization problem subject to LMI constraints by applying the cone complementary linearization method. This design scheme combines the strong robustness of the sliding mode control with the H_∞ norm performance. A numerical example is given to illustrate the effectiveness of the proposed scheme.     

Robust H∞ controller design for sampled-data systems with parametric uncertainties

This article investigates the problem of robust H∞ controller design for sampled-data systems with time-varying norm-bounded parameter uncertainties in the state matrices. Attention is focused on the design of a causal sampled-data controller, which guarantees the asymptotical stability of the closed-loop system and reduces the effect of the disturbance input on the controlled output to a prescribed H∞ performance bound for all admissible uncertainties. Sufficient condition for the solvability of the problem is established in terms of linear matrix inequalities (LMIs). It is shown that the desired H∞ controller can be constructed by solving certain LMIs. An illustrative example is given to demonstrate the effectiveness of the proposed method.