具有预设性能的近距离星间相对姿轨耦合控制

针对存在系统不确定性和外界干扰的接近绕飞阶段跟踪航天器相对目标航天器的姿态与轨道一体化控制任务,设计了一种具有预设性能的鲁棒反演控制器。该控制器能预先设计系统的稳态与暂态性能,保证相对姿轨跟踪误差满足预先设计的性能指标要求;为避免传统反演控制方法中存在的“微分膨胀”问题,引入滑模微分器对虚拟控制量的导数进行估计;同时利用自适应控制技术估计不确定模型参数及包含滑模微分器估计误差和外界干扰的集总干扰上界,并引入鲁棒补偿项处理这些不确定性带来的影响。理论分析证明所设计的控制方法能保证相对姿轨跟踪误差满足预设性能指标要求,仿真结果验证了所设计控制方法的有效性。     

航天器非线性鲁棒自适应姿态机动控制律

针对存在未知转动惯量和外部干扰力矩的敏捷航天器快速大角度姿态机动问题,结合非线性反步法和Lyapunovo稳定性分析方法设计控制力矩和转动惯量估计值的非线性鲁棒自适应控制律。在控制力矩控制律中,加入非线性阻尼项对外部干扰力矩进行补偿,证明了系统的全局一致最终有界稳定性。引入非线性动系数增加系统的动态性能,提高了姿态快速机动后的快速稳定能力。在Maltlab/Simulink环境下进行航天器姿态机动控制仿真研究,仿真结果验证了所设计控制器的有效性和可行性。     

超机动飞行的非线性鲁棒自适应控制系统研究

针对飞机模型中存在气动参数不确定性以及外界干扰等影响因素,设计了一种超机动飞行的非线性鲁棒自适应控制系统。控制系统设计过程中,模型不确定性和外界干扰由RBF神经网络在线补偿,控制律及神经网络权值自适应律由反步法得到。解决了系统中控制增益矩阵未知,同时存在外界干扰情况下的鲁棒飞行控制系统设计,并证明了闭环系统所有信号有界,系统跟踪误差和神经网络权值估计误差指数收敛到有界紧集内。对所研究的飞行控制系统进行了过失速Herbst机动仿真,结果验证了该系统在过失速机动条件下具有良好的控制性能。     

异结构不确定混沌系统的广义投影同步

针对一类参数随时间变化的不确定混沌系统,用鲁棒自适应方法实现异结构混沌系统的广义投影同步和参数辨识。基于李亚普诺夫稳定性理论,设计了鲁棒自适应控制器和参数自适应律。通过改变广义投影同步的比例矩阵,获得所有状态变量任意比例于原驱动系统的混沌信号,并辨识出系统所有未知参数。以R-ssler超混沌系统和Lü超混沌系统为例,数值仿真验证了所设计方法的有效性和可行性。     

ADRC based input disturbance rejection for minimum-phase plants with unknown orders and/or uncertain relative degrees

The capability of ADRC is studied for linear time-invariant SISO minimum-phase systems with unknown orders,uncertain relative degrees,and unknown input disturbances.It is proved that ADRC can reject the unknown input disturbance and guarantee the close-loop stability for the plants with unknown but bounded relative degrees.Meanwhile,some close-loop performances can be achieved. The influence of the sensor noise is also discussed.And it is demonstrated by numerical examples that one ADRC with fixed parameters can be applied to a group of plants of different orders,relative degrees, and parameters.     

Robust bounded control for uncertain flight dynamics using disturbance observer

The robust bounded flight control scheme is developed for the uncertain longitudinal flight dynamics of the fighter with control input saturation invoking the backstepping technique. To enhance the disturbance rejection ability of the robust flight control for fighters, the sliding mode disturbance observer is designed to estimate the compounded disturbance including the unknown external disturbance and the effect of the control input saturation. Based on the backstepping technique and the compounded disturbance estimated output, the robust bounded flight control scheme is proposed for the fighter with the unknown external disturbance and the control input saturation. The closed-loop system stability under the developed robust bounded flight control scheme is rigorously proved using the Lyapunov method and the uniformly asymptotical convergences of all closed-loop signals are guaranteed. Finally, simulation results are presented to show the effectiveness of the proposed robust bounded flight control scheme for the uncertain longitudinal flight dynamics of the fighter.     

Robust attitude control of a 3DOF helicopter with multi-operation points

A 3DOF (three degrees of freedom) helicopter attitude control system with multi-operation points is described as a MIMO time-varying uncertain nonlinear system with unknown constant parameters, bounded disturbance and nonlinear uncertainty, and a robust output feedback control method based on signal compensation is proposed. A controller designed by this method consists of a nominal controller and a robust compensator. The controller is linear time-invariant and can be realized easily. Robust attitude tracking property of closed-loop system is proven and experimental results show that the designed control system can guarantee high precision robust attitude control under multi-operation points. This research is supported by the National Natural Science Foundation of China under Grant Nos. 60674017 and 60736024.     

Disturbance Attenuation State-Feedback Control for Uncertain Interconnected Systems

This paper studies the problem of robust H∞ control design for a class of uncertain interconnected systems via state feedback. This class of systems are described by a state space model, which contains unknown nonlinear interaction and time-varying norm-bounded parametric uncertainties in state equation. Using the Riccati-equation-based approach we design state feedback control laws, which guarantee the decentralized stability with disturbance attenuation for the interconnected uncertain systems. A simple example of an interconnected uncertain linear system is presented to illustrate the results.     

基于干扰补偿的拦截弹新型反演姿态控制

针对同时具有未知干扰以及输入饱和与死区特性的大气层内拦截弹姿态控制系统,提出了一种基于干扰补偿的自适应动态面控制器设计方法。该方法通过设计改进的非线性干扰观测器(nonlinear disturbance observer, NDO)对未知干扰进行抑制,利用径向基函数(radial basis function,RBF)神经网络逼近输入饱和引起的非线性项,通过设计参数自适应律在线估计未知死区边界。通过构造合适的Lyapunov函数,证明闭环系统状态一致终结有界。仿真结果表明,所提方法鲁棒性良好,在输入非线性和未知干扰作用下,依然能良好地跟踪指令信号。     

服务航天器超近程逼近目标的相对姿轨耦合控制

针对服务航天器超近程逼近目标的相对姿态轨道耦合控制问题,推导了耦合动力学模型并设计了相应控制律。通过引入描述相对运动构型变化的期望相对位置矢量和位置误差矢量,将相对轨道跟踪控制问题转化为调节器的设计问题。推导了考虑对接机构安装位置的相对姿态轨道耦合动力学模型。利用李雅普诺夫稳定性理论,设计了考虑未知有界干扰的相对姿态轨道耦合控制律。考虑控制输入受限进行数学仿真,结果表明所设计的控制律是有效的,并具有较好的性能。     

非定常大气扰动下的MAV自主飞行智能控制研究

针对在非定常大气扰动作用下,微型飞行器MAV姿态稳定控制与导航都不同于常规的问题。研究了MAV飞行中大气扰动类型特征,建立了完整的非定常大气扰动工程化模型体系。在此基础上,提出了一种融合专家技术与模糊技术的MAV自主飞行智能控制,并建立了一个Lyapunov能量函数来分析MAV自主飞行系统稳定性。飞行仿真与试飞结果表明,MAV自主飞行系统在全局范围内具有渐进稳定性。     

A NOTE ON NONLINEAR ROBUST H∞ ALMOST DISTURBANCE DECOUPLING PROBLEM WITH STABILITY

1 IntroductionThe problem of a1most disturbance deco1lpling with stability(ADDPS fOr short) was orig-inally formulated and solved fOr linear systems by Willems in l98l([ll). Since then variousgeneralizations to nonlinear systems have been xnade(see, fOr e…     

Exponential Stability of the Euler-Bernoulli Beam Equation with External Disturbance and Output Feedback Time-Delay

This paper concerns the stability of a one-dimensional Euler-Bernoulli beam equation with external disturbance and output feedback time-delay, in which the disturbance is bounded by an exponential function. In order to estimate disturbance, the authors design an estimator of disturbance,which is composed of two parts: One is the system measurement that is called the eigen-measurement,another is a time-variant estimator of disturbance. Thus, the feedback controller which is based on the estimate of the disturbance is designed to stabilize the system. The finite-time stability of the system under this control law is proved by Lyapunov function method. Finally, some numerical simulations on the dynamical behavior of the closed-loop system is presented to show the correctness of the result.     

Robust adaptive neural network control with supervisory controller

The problem of direct adaptive neural network control for a class of uncertain nonlinear systems with unknown constant control gain is studied in this paper. Based on the supervisory control strategy and the approximation capability of multilayer neural networks (MNNs), a novel design scheme of direct adaptive neural network controller is proposed.The adaptive law of the adjustable parameter vector and the matrix of weights in the neural networks and the gain of sliding mode control term to adaptively compensate for the residual and the approximation error of MNNs is determined by using a Lyapunov method. The approach does not require the optimal approximation error to be square-integrable or the supremum of the optimal approximation error to be known. By theoretical analysis, the closed-loop control system is proven to be globally stable in the sense that all signals involved are bounded, with tracking error converging to zero.Simulation results demonstrate the effectiveness of the approach.     

考虑执行器故障的无人帆船事件触发控制

针对实际海洋环境下,无人帆船在艏向跟踪控制任务中存在的模型参数未知、控制输入频繁抖振和执行器磨损等问题,提出一种考虑执行器故障的无人帆船事件触发控制算法.首先,采用径向基函数神经网络(radius based function neural networks,RBF-NNs)对系统的未知模型参数进行在线逼近.其次,在无...     

一类切换系统的降阶输出反馈滑模控制

研究了一类含有非线性扰动切换系统的鲁棒镇定问题.基于滑模控制技术,提出了降阶输出反馈鲁棒控制策略,给出了系统的滑动模态可达条件,同时设计了该条件下各子系统的输出反馈滑模控制器,并根据李雅普诺夫函数和状态增益给出了离散切换策略,确保闭环切换系统是渐近稳定的.通过数值仿真验证了设计方法的有效性.     

空间电磁对接轨迹跟踪的自适应控制

面向在轨服务的空间电磁对接技术能克服传统基于推力器对接所固有的不足,应用前景广阔。航天器对接是一个相对距离逐渐减小的过程,应用于控制器设计的解析远场电磁力模型具有强非线性,且模型误差随相对距离的减小而逐渐增大。基于Lyapunov稳定性理论开展空间电磁对接轨迹跟踪控制器的自适应设计,通过控制参数在线修正以消除模型的不确定性以及外界干扰的影响;开展控制参数整定分析,证明了自适应控制策略的渐近稳定性。理论分析及仿真结果表明,空间电磁对接的自适应控制策略是可行的,并且具有渐近稳定性。     

滑模控制快速分段幂次趋近律设计与分析

针对滑模变结构控制中出现的抖振问题,提出了一种分段幂次趋近律。该趋近律采用分段函数方式设计,具有较快的收敛速率、较多的调节参数,并且针对不同阶段的趋近律分开设计互不影响。理论证明了该趋近律达到滑模面时无抖振、固定时间收敛,详细推导出了收敛时间的表达式。在系统存在不确定性和外界干扰时能收敛于干扰稳定界,求出了干扰稳定界范围,给出了各参数对收敛速率和干扰稳定界的影响程度。以小卫星姿态机动控制为例,通过对比仿真实验,证明了所提趋近律的优越性。     

未知非线性系统的神经网络跟踪控制与仿真研究

应用输入／输出反馈线性化方法和李亚普诺夫方法,研究了一类具有未知非线性函数的非线性动态系统的自适应鲁棒输出跟踪控制问题。首先通过坐标变换和输入变换,将非线性系统变换为部分线性可控系统。接着采用多层前向神经网络来逼近未知非线性函数,网络的权值根据李亚普诺夫原则来在线修正,这样就克服了多神经网络控制系统中存在的稳定性问题。同时,为了减少权值学习时间,应用遗传算法预先离线训练网络权值。最后提出了一个基于神经网络建模的自适应鲁棒控制律,给出了李亚普诺夫意义下的稳定性证明。所提出的控制律可确保相应闭环系统的状态及跟踪误差一致最终有界。所给的Van der pol系统的例子说明了所提控制方案的有效性与鲁棒性。     

New trajectory linearization control for nonlinear systems undergoing harmonic disturbance

This paper presents a new trajectory linearization control scheme for a class of nonlinear systems subject to harmonic disturbance. It is supposed that the frequency of the disturbance is known, but the amplitude and the phase axe unknown. A disturbance observer dynamics is constructed to estimate the harmonic disturbance,and then the estimation is used to implement a compensation control law to cancel the disturbance. By Lyapunov's direct method, a rigorous pool shows that the composite error of the closed-loop system can approach zero exponen-tially. Finally, the proposed method is illustrated by the application to control of an inverted pendulum. Compared with two existing methods, the proposed method demonstrates better performance in tracking error and response time.