基于模糊控制的高超声速飞行器二阶滑模姿态控制

考虑高超声速飞行器飞行过程中气动参数变动导致的不确定,将模糊控制与二阶滑模控制相结合,形成自适应模糊二阶滑模控制器,用于控制高超声速飞行器姿态的飞行系统中.依据奇异摄动理论,设计快速和慢速双闭环系统控制角速率和姿态角.设计二阶滑模控制器用于有效地衰减抖振,同时对姿态角指令实现准确和快速跟踪.采用自适应模糊逻辑逼近高超声速飞行器动力学和运动学模型中的不确定部分,以对控制器进行有效补偿,基于Lyapunov稳定性理论,推导模糊规则参数的自适应律,确保整个闭环控制系统的稳定.仿真结果表明,所提出的高超声速飞行器的自适应模糊滑模控制系统能够有效抑制气动参数摄动的影响,对姿态角指令有较好的跟踪性能.     

基于新型固定时间稳定方法的一类二阶非线性系统镇定控制

本文研究了受未知外部扰动侵袭的一类二阶非线性系统的固定时间镇定控制问题.首先,提出了一种新的固定时间稳定方法,并给出了收敛时间及其上界估计值的计算公式.理论分析表明,收敛时间的上界与系统初始状态无关,可由系统参数完全确定.然后,基于所提出的固定时间稳定方法设计了新型滑模趋近律和终端滑模面,使得系统状态能够在有界的有限时间内,从任意初始状态收敛至滑模面并沿着滑模面收敛至原点,同时引入了基于系统状态的自适应切换方法,有效避免了终端滑模面导致的奇异问题.最后,通过仿真验证了算法的有效性.     

不确定欠驱动系统的高阶自适应Super-Twisting滑模控制

为实现一类不确定欠驱动系统在未知干扰情况下的鲁棒控制,针对传统滑模控制中存在的抖振问题,提出一种基于二次型Lyapunov函数的二阶Super-Twisting自适应滑模控制策略.首先,控制器的不连续项采用二阶Super-Twisting算法,将不连续控制作用在滑模量的二阶导数.然后,针对滑模面受不确定干扰影响的情况,为调节参数设计一种自适应律方法,该方法不受传统二阶滑模控制中干扰项的一阶导数边界已知的条件限制,保证滑模面在有干扰情况下的收敛,削弱控制器输入的抖振现象.最后,以两轮自平衡车为实验对象验证该方法,并与传统滑模及普通二阶滑模方法做仿真对比.仿真结果表明文中所提的二阶自适应滑模控制方法在控制效果和降低抖振方面表现更优.     

四旋翼无人侦察器轨迹跟踪控制研究

针对在系统动力参数不确定、干扰随机性的情况下,对四旋翼无人侦察器非线性模型进行有效控制的问题,建立了侦察器的动力学模型,并提出了一种基于双层回路的非线性控制器设计方法.其外层回路中设计了基于模糊PID(proportional-integral-derivation)控制的控制器来实现高度和位置跟踪;内层回路中利用滑模控制器来实现姿态稳定控制.仿真结果表明,设计的控制器能够使无人侦察器的运动轨迹和姿态角快速收敛到期望值且稳定在较小的误差范围内,具有较好的适应性和鲁棒性.     

四旋翼飞行器的自适应二阶滑模控制

针对四旋翼飞行器参数变化的姿态控制问题,将自适应光滑二阶滑模控制方法应用于四旋翼飞行器控制系统.对于参数变化引起的模型不确定性部分采用滑模干扰观测器进行补偿,对姿态系统设计自适应光滑二阶滑模控制器,有效地减弱传统滑模控制的抖振,控制器参数的在线调整提高了系统的控制精度.基于Lyapunov理论证明了系统的有限时间稳定.数字仿真和实验结果都验证了所提控制方法的有效性.     

基于高阶滑模速度控制器的异步电机模型预测转矩控制

针对三相异步电机驱动系统,提出一种基于高阶滑模速度控制器的模型预测转矩控制策略.为了降低负载扰动对系统运行性能的影响,设计一种基于二阶Super-Twisting滑模技术的速度环控制器,以代替传统PI速度控制器,并应用Lyapunov稳定性理论对其稳定性和鲁棒性进行分析,得到使速度控制系统收敛的参数范围.为了提升转矩控...     

基于学习观测器的航天器指定时间跟踪控制

针对一类含有外部扰动和执行器故障的刚体航天器姿态控制系统,提出一种基于自适应学习观测器的指定时间容错控制器的设计方案.首先,系统性地给出一种改进型自适应学习观测器设计方案,基于自适应学习观测器框架,设计航天器姿态系统的学习观测器实现对系统的综合扰动值估计;然后,利用综合扰动的估计信息和滑模控制理论设计指定时间容错跟踪控制器,使得系统的姿态角能够在指定时间跟踪指令信号,系统的收敛时间可通过容错控制器的参数预先设置,且与系统的初始状态值无关;接着,基于Lyapunov稳定性理论验证含有故障的姿态控制系统能够在指定时间内稳定;最后,通过数值仿真,与已有的观测器和有限时间控制方案进行对比,表明所提出方案的有效性和可行性.     

基于非奇异快速终端滑模的轧机液压伺服位置系统反步控制

针对具有非线性、参数不确定性和未知负载扰动的非对称缸轧机液压伺服位置系统,提出一种基于模糊自适应观测器和非奇异快速终端滑模面的反步控制方法.首先,基于非奇异快速终端滑模面和双幂次趋近律完成非对称缸轧机液压伺服位置系统反步控制器的设计,并通过构造二阶滑模滤波器对虚拟控制量的微分信号进行估计,有效地避免了反步控制中的微分爆炸现象;然后,选用模糊自适应观测器对系统的不确定项进行逼近估计,并将输出的估计值引入到设计的控制器中进行补偿,有效地提高了系统的跟踪控制精度,且分析表明,所提出的控制方法能够保证闭环系统全局渐近稳定;最后,基于某650mm可逆冷带轧机液压伺服位置系统的实际参数进行仿真研究,并与常规线性滑模控制方法相比较,结果验证了所提出方法能够有效提高系统在整个全局过程的收敛速度和鲁棒稳定性.     

快速二阶终端滑模控制及其在下肢外骨骼的应用

为了提高传统二阶终端滑模控制的全局收敛性,提出一种快速二阶终端滑模控制算法.设计一种二阶趋近律,将绝对值函数隐藏在积分项里,并增加线性项以提高全局收敛性.当系统状态未到达滑模面时,采用二阶趋近律,并通过调整参数避免奇异问题;当系统状态到达滑模面时,采用不含不连续符号项的指数趋近律,以保证控制误差有限时间收敛.采用Lyapunov直接法证明快速二阶终端滑模控制算法的稳定性,及其比super twisting算法具有更优良的收敛特性.以下肢外骨骼为研究对象,建立动力学模型.在考虑建模误差和外部干扰的情况下,将该算法应用于下肢外骨骼的姿态控制.仿真结果表明,所提出的控制算法能够有效抑制抖振,并且比super twisting算法具有更良好的跟踪性能,验证了该算法的有效性.     

轮式移动机器人轨迹跟踪控制研究

针对轮式移动机器人参数摄动和内外部扰动等问题,提出一种新型的基于自适应扩张状态观测器的滑模控制算法。采用自适应虚拟速度控制器估计系统未知参数,滑模控制器抑制参数摄动和内外部扰动,非线性扩张状态观测器观测系统扰动并减小控制输入的抖振,实现了轨迹跟踪误差的快速收敛。利用Lyapunov稳定性理论证明了控制算法的稳定收敛性。将所提算法与传统自适应反演滑模算法进行对比,对比结果表明了所提算法的有效性和鲁棒性。     

作业型飞行机器人抓取后重心偏移的轨迹跟踪控制

作业型飞行机器人是指能够对环境施加主动影响的飞行机器人, 它通常由旋翼飞行器与机械臂组合而成. 本文针对作业型飞行机器人在动态飞行抓取后, 重心位置变化产生的系统控制难题, 设计了有效的跟踪控制策略. 首先, 在系统建模时引入重心偏移系统参数和重心偏移控制参数, 并考虑惯性张量不为常数, 提高了系统建模的精度. 然后, 在姿态解算时, 考虑重心偏移对系统性能的影响, 构建包含重心偏移系统参数的解算方法, 得到更高精度的期望翻滚角和期望俯仰角. 接着, 设计了基于滑模控制的重心偏移补偿位置控制器, 实现了有效的位置跟踪控制. 同时, 在姿态反演控制器的基础上, 加入自适应律估计重心偏移控制参数和变化的惯性张量, 再通过小脑神经网络逼近惯性张量的真实值, 提高姿态控制器的精度. 最后, 给出了所设计控制器的稳定性证明, 并在仿真环境下验证了所提出的方法的有效性和优越性.     

Static and dynamic sliding mode control of variable reluctance motors

In this paper, static and a dynamic sliding mode control schemes are proposed for the speed control of a variable reluctance motor (VRM). The proposed controllers guarantee the asymptotic regulation of the speed of the motor to its desired value. Simulation results of the proposed controllers are given to illustrate the developed theory. In addition, the robustness of the proposed sliding mode controllers to changes in the parameters of the motor and to load disturbances is validated through simulation studies.     

Second-order Sliding Mode Approaches for the Control of a Class of Underactuated Systems

In this paper, first-order and second-order sliding mode controllers for underactuated manipulators are proposed. Sliding mode control(SMC) is considered as an effective tool in different studies for control systems. However, the associated chattering phenomenon degrades the system performance. To overcome this phenomenon and track a desired trajectory, a twisting, a supertwisting and a modified super-twisting algorithms are presented respectively. The stability analysis is performed using a Lyapunov function for the proposed controllers. Further, the four different controllers are compared with each other. As an illustration, an example of an inverted pendulum is considered. Simulation results are given to demonstrate the effectiveness of the proposed approaches.     

任意初态下的工业机器人迭代学习控制

对迭代初值为任意值的工业机器人轨迹跟踪控制系统,提出了一种基于滑模面的非线性迭代学习控制算法,使机器人轨迹能快速、精确跟踪上期望轨迹.基于有限时间收敛原理,构建了关于机器人轨迹跟踪误差的迭代滑模面,在滑模面内,机器人轨迹跟踪误差在预定时间内收敛到零.设计了基于滑模面的迭代学习控制算法,理论证明了随着迭代次数的增加,处于...     

Robust Stabilization of Nonlinear PVTOL Aircraft with Parameter Uncertainties

In this work, the stabilization control problem is investigated for the planar vertical take‐off and landing (PVTOL) aircraft with unknown model parameters. To cope with the challenges caused by non‐minimum phase and parametric uncertainties, a new appropriate output, different from the general centroid position output, is carefully constructed to ensure the zero dynamics asymptotically stable, then the sliding‐mode technique is applied to design a state feedback control law. The proposed robust control law is proved able to asymptotically stabilize the PVTOL aircraft to the desired fixed position with null velocities and roll angle despite the unknown model parameters. Simulation examples illustrate the effectiveness of the proposed control algorithm.     

A novel adaptive high-order sliding mode control based on integral sliding mode

This paper presents an adaptive high-order sliding mode control scheme targeting for uncertain minimum phase nonlinear single-input-single-output (SISO) systems, which can be equivalently formulated as the finite-time stabilization of high-order input-output dynamics subject to the uncertainties of parameters such as a chain of integrators. The proposed controller is derived from the concept of integral sliding mode and consists of two parts, one part of which achieves the finite-time stabilization of the high-order input-output dynamics without uncertainties by solving a finite-horizon optimal control problem with a free-final-state. The other part adopts the adaptive sliding mode control technique considering the practical bounded uncertainties, by which a modified switching gain adaptation algorithm is developed so that the on-line switching gain selection can be executed and the upper bounds of the uncertainties are not requisite in advance. As a result, a high-order sliding mode is established, ensuring the sliding variables and its high-order derivatives converge to an arbitrarily small vicinity of the origin in finite time. Therefore, the proposed controller achieves fixed convergence time and further improves strong robustness against bounded uncertainties with lower chattering and the easy implementation. Simulation results are presented in detail to verify the effectiveness and feasibility of the proposed algorithm.     

多变量模型不确定系统的二阶滑模分解控制方法

提出一种多变量模型不确定系统的二阶终端滑模分解控制方法。通过状态变换和去耦合处理将系统转换为块能控标准型，它由输入输出子系统和穗定的零动态子系统组成。提出了特殊的二阶终端滑模超曲面和相应的控制策峪，使输入输出子系统状态渐近收敛到平衡点，零动态子系统随后也渐近收敛到平衡点。所提出方法对于控制维教较高的系统具有较大的意义，可简化设计，实现鲁棒分解控制。由于采用了二阶滑模的思想，可有效地消除系统的高频抖振。仿真实例表明了该方法的有效性。     

Terminal angle constrained time-varying sliding mode guidance law with autopilot dynamics and input saturation

To intercept the maneuvering target at a desired terminal angle, this paper presents a time-varying sliding mode guidance law with consideration of the second-order autopilot dynamics and input saturation. To achieve the finite-time interception and satisfactory overload characteristics, a time-varying sliding mode guidance law is developed, which enables the line-of-sight (LOS) angle error to converge into a small neighborhood of the origin at the interception time. An auxiliary system is constructed to reduce the adverse effect generated from the input saturation. Moreover, with the aid of extended state observers, the proposed guidance law requires no information on the target acceleration and the acceleration derivative of the interceptor. The performance of this guidance law is verified via the numerical simulations.     

Finite time distributed distance‐constrained shape stabilization and flocking control for d‐dimensional undirected rigid formations

Most of the existing results on distributed distance‐constrained rigid formation control establish asymptotic or exponential convergence. To further improve the convergence rate, we explain in this paper how to modify existing gradient controllers to obtain finite time stability. For point agents modeled by single integrators, the controllers proposed in this paper drive the whole formation to locally converge to a desired shape with finite settling time. We also show for undirected triangular formation shape control, if all the agents start with non‐collinear positions, then the formation will converge to the desired shape in finite time. For agents modeled by double integrators, the proposed controllers allow all agents to both achieve the same velocity and reach a desired shape in finite time. All controllers are totally distributed. Simulations are also provided to validate the proposed control strategies. Copyright © 2015 John Wiley & Sons, Ltd.