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非线性时滞系统鲁棒L2控制器设计 总被引:1,自引:0,他引:1
本文针对带有不确定性的非线性时滞系统,基于系统耗散的定义,讨论了其鲁棒L2控制器设计问题,通过设计一个新的李雅普诺夫泛函,得到了系统稳定且满足耗散的充分必要条件,在此基础上设计满足L2性能指标的控制器,所得结果通过线性矩阵不等式给出. 相似文献
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四旋翼无人机鲁棒自适应姿态控制 总被引:1,自引:0,他引:1
四旋翼无人机的姿态控制是自主飞行控制的核心,针对四旋翼姿态易受外界环境干扰和内部参数摄动等不确定性影响的问题,设计了一种鲁棒自适应反步控制器,以提高四旋翼的鲁棒性。建立了四旋翼完整的姿态运动模型,并将其转化为含有广义不确定性的多输入多输出非线性系统。根据该系统满足严格反馈的结构特点,设计了反步控制器; 针对系统中存在的外部干扰和内部参数摄动等不确定性,引入了一类鲁棒自适应函数来抵消该不确定性对系统的影响; 采用非线性跟踪微分器估计虚拟控制量的微分信号,减小了反步控制器设计中普遍存在的“计算膨胀”问题; 通过构造Lyapunov 函数证明闭环系统是稳定且指数收敛的。仿真结果表明,所设计控制器具有良好的控制效果和鲁棒性。 相似文献
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电液负载模拟器的自适应滑模控制方法 总被引:1,自引:0,他引:1
针对电液负载模拟器存在的系统非线性、不确定性和强干扰的控制难点,设计了自适应滑模控制方法.设计积分滑模以降低控制器对期望跟踪轨迹高阶导数的要求;设计动态滑模算法抑制抖振;采用小脑模型关节控制器(CMAC)在线学习系统不确定性以降低控制器参数设计的保守性.设计了自适应滑模控制律,给出了CMAC神经网络权值调整算法,证明了控制器的稳定性,以确保系统稳定且输出跟踪误差渐近收敛于零.仿真结果证明了控制策略的有效性. 相似文献
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基于观测器的时滞系统鲁棒控制器的设计 总被引:1,自引:0,他引:1
研究了一类不确定时滞系统基于观测器的鲁棒镇定问题,系统的不确定性时变未知且范数有界,目的是设计状态观测器和线性无记忆观测状态反馈控制器,使其能够镇定一类状态和控制输入不确定性时滞系统。基于Lyapunov稳定性理论,采用线形矩阵不等式这一有效工具,给出了系统基于观测状态反馈鲁棒镇定的充分条件,并且利用线形矩阵不等式的解构造了使得系统鲁棒稳定的基于观测状态反馈控制器,所得结果与时滞相关,从而相对减弱了控制器设计的保守性。数值算例表明了所提出的设计方法的有效性。 相似文献
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基于Backstepping设计的不确定非线性系统的预测控制 总被引:1,自引:0,他引:1
本文的目的是针对一类带有不确定性的单输入单输出的仿射非线性系统,设计一种非线性预测控制器.用反步设计思想获得具有待定参数的控制器表达式,然后用预测控制在线优化获得控制器的参数.用这种方法设计的控制器更易使闭环系统稳定,且闭环系统具有良好的动态特性.连续发酵过程的仿真结果也验证了控制器是有效的. 相似文献
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针对一类含不确定参数且存在未知扰动的非线性系统,设计了一种新型的自适应鲁棒控制器。用反演设计思想获得具有待定系数的控制器表达式,用BP神经网络自适应调节控制器的参数。仿真结果表明该控制器对系统参数的不确定性和未知扰动具有一定的鲁棒性,并能保证闭环系统全局稳定。 相似文献
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A systematic approach to parameter-dependent control synthesis of a high-speed supercavitation vehicle (HSSV) is presented. The aim of the control design is to provide robust reference tracking across a large flight envelope, while directly accounting for the interaction of liquid and gas phases with the vehicle. A nonlinear dynamic HSSV model is presented and discussed relative to the actual vehicle. A linear, parameter-varying (LPV) controller is synthesized for angle rate tracking in the presence of model uncertainty. The control design takes advantage of coupling in the governing equations to achieve improved performance. Multiple LPV controllers synthesized for smaller overlapping regions of the parameter space are blended together, providing a single controller for the full flight envelope. Time-domain simulations implemented on high-fidelity simulations, provide insight into the performance and robustness of the proposed scheme. 相似文献
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In this paper, we develop a theoretical framework for linear quadratic regulator design for linear systems with probabilistic uncertainty in the parameters. The framework is built on the generalized polynomial chaos theory. In this framework, the stochastic dynamics is transformed into deterministic dynamics in higher dimensional state space, and the controller is designed in the expanded state space. The proposed design framework results in a family of controllers, parameterized by the associated random variables. The theoretical results are applied to a controller design problem based on stochastic linear, longitudinal F16 model. The performance of the stochastic design shows excellent consistency, in a statistical sense, with the results obtained from Monte-Carlo based designs. 相似文献
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This paper studies the resilient (non‐fragile) H∞ output‐feedback control design for discrete‐time uncertain linear systems with controller uncertainty. The design considers parametric norm‐bounded uncertainty in all state‐space matrices of the system, output and controller equations. The paper shows that the resilient H∞ output‐feedback control problem is equivalent to a scaled H∞ output‐feedback control problem of an auxiliary system without any system or controller uncertainty. Using the existing optimal H∞ design to solve the auxiliary system, the design guarantees that the resultant closed‐loop systems are quadratically stable with disturbance attenuation γ for all admissible system and controller uncertainties. A numerical example is given to illustrate the design method and its benefits. 相似文献
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Probabilistic Robust Linear Parameter-varying Control of a Small Helicopter Using Iterative Scenario Approach 下载免费PDF全文
In this paper, we present an iterative scenario approach (ISA) to design robust controllers for complex linear parameter-varying (LPV) systems with uncertainties. The robust controller synthesis problem is transformed to a scenario design problem, with the scenarios generated by identically extracting random samples on both uncertainty parameters and scheduling parameters. An iterative scheme based on the maximum volume ellipsoid cutting-plane method is used to solve the problem. Heuristic logic based on relevance ratio ranking is used to prune the redundant constraints, and thus, to improve the numerical stability of the algorithm. And further, a batching technique is presented to remarkably enhance the computational efficiency. The proposed method is applied to design an output-feedback controller for a small helicopter. Multiple uncertain physical parameters are considered, and simulation studies show that the closed-loop performance is quite good in both aspects of model tracking and dynamic decoupling. For robust LPV control problems, the proposed method is more computationally efficient than the popular stochastic ellipsoid methods. 相似文献
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根据控制和观测间的对偶性,论证了“通过对偶系统控制器的设计来获得线性时滞系统的状态观测器”这一方法的可行性,并就一工业实例作了计算机仿真。另外,对含状态观测器、并具线性状态估计值反馈结构的闭环系统的分离性作了探讨。 相似文献
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This paper considers the problem of decentralized H controller design via measurement feedback for linear composite systems. Two decentralized controller design procedures are presented in terms of positive definite solutions to modified algebraic Riccati inequalities. The resulting controllers guarantee closed-loop stability and an H -norm bound on disturbance attenuation. A numerical example is given to illustrate the design procedures. 相似文献
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