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2018 15th International Workshop on Variable Structure Systems (VSS)最新文献

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Robust Control for Perturbed Linear Systems with Time-Varying Delay via Sliding Mode Control 时变时滞摄动线性系统的滑模鲁棒控制
Pub Date : 2018-07-09 DOI: 10.1109/VSS.2018.8460263
H. Caballero-Barragán, L. Osuna-Ibarra, A. Loukianov, F. Plestan
In the present paper, a robust predictor-based sliding mode control for perturbed time-varying delay systems is proposed. A predictor is designed to compensate the time-varying delay effect in control input, and then an integral sliding mode control technique along with super-twisting algorithm is applied to compensate partially the effect of the perturbation term. Finally, a nominal delay-free part of the control input is designed to stabilize the sliding mode dynamics. Conditions for the stability of the closed-loop perturbed system are derived. Simulation result is presented.
提出了一种基于鲁棒预测器的摄动时变时滞系统滑模控制方法。设计了一个预测器来补偿控制输入中的时变时滞效应,然后采用积分滑模控制技术和超扭转算法来部分补偿扰动项的影响。最后,设计了控制输入的标称无延迟部分来稳定滑模动力学。导出了闭环摄动系统稳定的条件。给出了仿真结果。
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引用次数: 4
Discrete-Time Equivalent Homogeneous Differentiators 离散时间等价齐次微分器
Pub Date : 2018-07-09 DOI: 10.1109/VSS.2018.8460284
Stefan Koch, M. Reichhartinger
This paper proposes an entirely new discrete-time realization of an arbitrary order robust exact differentiator. Its construction relies on the redesign of the differentiator in the discrete-time domain by means of a non-linear eigenvalue placement. The resulting algorithm is consistent with the continuous-time algorithm and preserves the best possible asymptotic accuracies known from the continuous-time differentiator. In contrast to the existing discretization schemes, the proposed schemes are exact in the sense that in the unperturbed case the differentiators ensure vanishing estimation errors. Limit cycles typically present in the error state variables enforced by the forward Euler discretized algorithm are avoided and the precision is insensitive to an overestimation of the gains.
本文提出了一种全新的任意阶鲁棒精确微分器的离散时间实现方法。它的构造依赖于通过非线性特征值的放置在离散域重新设计微分器。所得算法与连续时间算法一致,并保持了从连续时间微分器中已知的最佳渐近精度。与现有的离散化方案相比,所提出的方案是精确的,因为在无摄动情况下,微分器确保估计误差消失。避免了前向欧拉离散算法强制的误差状态变量中通常存在的极限环,并且精度对增益的高估不敏感。
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引用次数: 23
Application of Higher-Order Sliding-Modes to a Ball and Plate System 高阶滑动模态在球盘系统中的应用
Pub Date : 2018-07-01 DOI: 10.1109/VSS.2018.8460469
Alexander Barth, C. Weise, J. Reger
This paper presents a control strategy that combines feedback-linearization with higher-order sliding-mode control for the tracking control of a cam-plate driven ball and plate system. The concept of the practical relative degree legitimates to reconsider the system representation as a simpler feedback-linearizable system. For the remaining linear dynamics, a higher-order sliding-mode algorithm serves to estimate the states required for a super-twisting controller. The effectiveness of the proposed approach is demonstrated on a laboratory test-bench imposing a circular trajectory for tracking.
提出了一种将反馈线性化与高阶滑模控制相结合的控制策略,用于凸轮-板驱动球板系统的跟踪控制。实际相对度的概念使得将系统表示重新考虑为更简单的反馈线性化系统是合理的。对于剩余的线性动力学,一个高阶滑模算法用于估计超扭转控制器所需的状态。该方法的有效性在实验室试验台上得到了验证,试验台施加了圆形轨迹进行跟踪。
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引用次数: 1
Filtering Differentiators and Observers 滤波微分器和观察器
Pub Date : 2018-07-01 DOI: 10.1109/VSS.2018.8460259
A. Levant
New finite-time-exact robust (FTER) differentiators, filters and observers based on sliding modes are produced which are capable of filtering out unbounded sampling noises and of the complete FTER output-dynamics observation in the case of known relative degrees and high-frequency gains.
新的有限时间精确鲁棒(FTER)微分器、滤波器和基于滑模的观测器能够在已知相对度和高频增益的情况下滤除无界采样噪声和完整的FTER输出动态观测。
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引用次数: 25
Selection of Switching Surface Parameters in the Presence of Control Constraints in Aerospace Applications 航空航天中存在控制约束的开关面参数选择
Pub Date : 2018-07-01 DOI: 10.1109/VSS.2018.8460260
Sachit Rao
The closed-loop properties as well as the simple design procedure for the control of linear time-invariant (LTI) systems, offered by the sliding mode control (SMC) algorithm, are well known. The focus of this paper is in designing an SMC for a fixed-wing aircraft in the presence of control constraints and illustrating that the switching surface parameters decide the initial conditions of the aircraft states from which sliding mode can even be expected to occur. The need to perform a trade-off between the magnitudes of these initial states and the speed of the sliding mode dynamics is highlighted; a procedure to calculate these magnitudes is also proposed. A dynamic model of the longitudinal dynamics of a fixed-wing aircraft, linearised about some trim conditions, is chosen for the study.
滑模控制(SMC)算法所提供的线性时不变(LTI)系统的闭环特性和简单的控制设计过程是众所周知的。本文的重点是设计一个存在控制约束的固定翼飞机的SMC,并说明切换面参数决定飞机状态的初始条件,甚至可以预期滑模的发生。强调需要在这些初始状态的大小和滑模动力学的速度之间进行权衡;还提出了一种计算这些震级的方法。选择了一个固定翼飞机纵向动力学模型,该模型对一些配平条件进行了线性化。
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引用次数: 3
Saturated Continuous Twisting Algorithm 饱和连续扭曲算法
Pub Date : 2018-07-01 DOI: 10.1109/VSS.2018.8460449
M. Golkani, L. Fridman, Stefan Koch, M. Reichhartinger, M. Horn
In this paper, a second-order system affected by perturbations is considered. A feedback control law adopting the continuous twisting algorithm is designed such that a saturated and continuous control signal is introduced to the system. In the case that a state variable is not measurable, estimate information obtained through a super-twisting observer is incorporated into the design. For the closed-loops (with and without observer), global finite-time stability properties are established. The feasibility and effectiveness of the strategy is shown employing numerical simulations.
本文研究了一类二阶扰动系统。设计了一种采用连续扭转算法的反馈控制律,将饱和连续控制信号引入系统。在状态变量不可测量的情况下,通过超扭转观测器获得的估计信息被纳入设计。对于有观测器和无观测器的闭环,建立了全局有限时稳定性。通过数值仿真验证了该策略的可行性和有效性。
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引用次数: 6
On Stability of Event-Triggered Systems With Sliding Mode Control 论采用滑模控制的事件触发系统的稳定性
Pub Date : 2018-07-01 DOI: 10.1109/VSS.2018.8460428
Abhisek K. Behera, B. Bandyopadhyay
In this paper, we investigate the stability of a controlled system in the event-triggering framework. By designing the triggering scheme, the control signals are updated when it is demanded subject to some satisfactory system performance. However, the stability of the system is not yet fully investigated with respect to the triggering conditions. So, the main purpose of the paper is to analyse the stability of the system with respect to the proposed triggering scheme. In this paper, sliding mode control (SMC) is used to design the event-triggered control. Our analysis proposes a new notion called bounded event property for the event which guarantees the triggering instants are generated in finite-time for all possible values of the triggering parameter. It is shown that the event-triggered SMC ensures possess the bounded event property and moreover the proposed triggering mechanism also guarantees the stability of the closed loop system stability.
本文研究了事件触发框架下受控系统的稳定性。通过设计触发方案,在系统性能令人满意的前提下,控制信号会在需要时更新。然而,对于触发条件,系统的稳定性尚未得到充分研究。因此,本文的主要目的是分析与拟议触发方案相关的系统稳定性。本文采用滑模控制(SMC)来设计事件触发控制。我们的分析提出了一个新的概念,即事件的有界事件属性,它保证了在所有可能的触发参数值下,触发时刻都是在有限时间内产生的。结果表明,事件触发式 SMC 可确保具备有界事件特性,而且所提出的触发机制还能保证闭环系统的稳定性。
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引用次数: 2
Robust State Estimation for Linear Time Varying Lateral Vehicle Dynamics with Unknown Road Curvature 未知道路曲率下线性时变车辆横向动力学的鲁棒状态估计
Pub Date : 2018-07-01 DOI: 10.1109/VSS.2018.8460385
Markus Tranninger, Martin Steinberger, L. Fridman, M. Horn, S. Zhuk
This paper presents a cascaded observer scheme for state estimation of the lateral vehicle dynamics. A velocity dependent linear time varying model where the road curvature acts as an unknown input is considered. The proposed observer structure is based on an $mathcal{H}_{alpha}$, filter in combination with a higher order sliding mode compensator and yields finite time exact state reconstruction. The observer design is carried out step by step and simulation results show the applicability of the proposed approach.
提出了一种用于车辆横向动力学状态估计的级联观测器方案。考虑了以道路曲率作为未知输入的速度依赖线性时变模型。所提出的观测器结构是基于$mathcal{H}_{alpha}$,滤波器与高阶滑模补偿器相结合,并产生有限时间精确的状态重建。逐步进行了观测器设计,仿真结果表明了该方法的适用性。
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引用次数: 0
Adaptive Exponent Parameter: a Robust Control Solution Balancing Between Linear and Twisting Controllers 自适应指数参数:一种平衡线性控制器和扭转控制器的鲁棒控制方法
Pub Date : 2018-07-01 DOI: 10.1109/VSS.2018.8460266
E. Tahoumi, F. Plestan, M. Ghanes, J. Barbot
In this paper, a new controller is proposed, based on a well known homogeneous controller. The suggested controller gives rise to an efficient trade-off between the standard linear state feedback and twisting algorithm. As a consequence, the obtained controller has the advantages of both controllers with their drawbacks reduced. To achieve this objective, a parameter on the exponent terms of the homogeneous controller is adapted. The convergence of the closed loop system to a vicinity of the origin is given. Finally, some simulations validate the effectiveness of the proposed controller.
本文在齐次控制器的基础上提出了一种新的控制器。所提出的控制器在标准线性状态反馈和扭曲算法之间进行了有效的权衡。因此,所得到的控制器既具有两种控制器的优点,又减少了它们的缺点。为了实现这一目标,采用了齐次控制器指数项上的参数。给出了闭环系统在原点附近的收敛性。最后,通过仿真验证了所提控制器的有效性。
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引用次数: 5
A Single-Loop High-Order Sliding Mode Controller for a Missile Interceptor 导弹拦截器单回路高阶滑模控制器
Pub Date : 2018-07-01 DOI: 10.1109/VSS.2018.8460335
M. Cross, Y. Shtessel
The guidance and control (G&C) on a missile interceptor orchestrate the vehicle's functional subsystems to minimize miss distance. In contrast to the traditional cascaded G&C loop structure that handles the guidance and control separately, a single-loop and single control law govern the fin actuation. The high relative degree of a missile engagement scenario makes controller design more difficult. The use of higher order sliding mode differentiators mitigates the problem. The objective of this work is to develop a robust, high-order sliding mode controller that intercepts maneuvering targets using minimal information. Nonlinear pitch plane engagement kinematics and linear pitch plane missile dynamics are defined for controller development and simulation purposes. Through simulation the control law is shown to be simple and intuitive, only requiring relative normal velocity for state feedback, meaning it can work in a GPS-denied environment.
导弹拦截器上的制导和控制(G&C)协调车辆的功能子系统以最小化脱靶距离。与传统的分离制导和控制的级联G&C回路结构不同,鳍形驱动采用单回路和单控制律。高相对程度的导弹交战场景使得控制器设计更加困难。使用高阶滑模微分器减轻了这个问题。这项工作的目的是开发一种鲁棒的高阶滑模控制器,该控制器可以使用最少的信息拦截机动目标。为了控制器的开发和仿真目的,定义了非线性俯仰平面啮合运动学和线性俯仰平面导弹动力学。仿真结果表明,该控制律简单直观,只需要相对法向速度进行状态反馈,可以在无gps环境下工作。
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引用次数: 2
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2018 15th International Workshop on Variable Structure Systems (VSS)
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