基于神经网络的迟滞非线性补偿控制

提出了一种基于神经网络的迟滞非线性的补偿方法.首先构造一个Duhem逆算子来描述迟滞逆状态.然后利用神经网络来逼近此状态和输出之间的关系来得到神经网络迟滞逆模型,神经网络权值采用反馈误差学习方法来进行在线调整.系统的前馈控制器和反馈控制器分别为逆模型和PID控制器.该方法不需要建立迟滞的正模型,能够在线构造逆模型来实现迟滞补偿.最后通过仿真验证了该方法的有效性.     

基于开放平台和神经网络的自主飞行控制系统研究

开发了飞行控制软件的应用中间件，实现控制结构的动态变化和控制组件的动态重构. 基于模型逆技术，设计了某状态下的旋转逆和平移逆控制器，其它状态下的逆误差由在线神经网络补偿．实例仿真的结果表明：开放平台和神经网络的结合，能够很好地实现无人直升机的自主飞行，具有较大的理论意义和工程应用价值．     

一种基于DTFEL的非线性自适应逆控制

提出一种基于离散时间反馈误差学习(DTFEL)的两自由度非线性自适应逆控制(AIC)方法,其控制器由动态RBF神经网络(DRBFNN)前馈控制器和参数固定的PD反馈控制器构成.PD控制器用来保证闭环系统稳定,动态RBF神经网络以PD控制器输出和反馈误差的线性组合为学习信号,通过一种改进的NLMS(VS MNLMS)算法在线学习和逼近对象的动态逆,提高反馈控制器的性能.稳定性分析证明了该AIC系统稳定.数字仿真结果表明,该AIC具有良好的自适应能力和鲁棒性,是一种有效的非线性控制方法.     

严格反馈非线性系统的自适应神经网络输出反馈控制

基于非线性反馈函数,文章设计神经网络状态观测器,解决一类非线性系统的输出反馈控制问题.非线性反馈神经网络观测器在系统存在不确定性函数的情况下实时估计系统状态.利用所获得的状态信号,设计了自适应神经网络动态面控制器,同时保证了闭环系统的稳定性和所有信号的有界性.通过调节设计参数的取值能够达到期望的闭环跟踪性能.数值仿真表明,所设计的状态观测器不需要对原系统做状态变换,能够克服输出反馈滑模控制器带来的抖震问题.     

一种混合神经网络飞行控制方法研究

讨论了一种基于神经网络控制的飞行控制方法。针对复杂非线性系统难以建立精确模型的特点,利用神经网络的任意非线性逼近能力进行控制器设计,首先应用神经网络在线辨识对象逆模型,进行控制系统反馈线性化;接着利用circle theorem（圆定理）设计线性PID鲁棒控制器,控制系统输出跟随系统输入,然后应用神经网路自适应逆方法设计混合控制器,最后以F-8飞机纵向飞行控制模态为研究对象进行仿真。仿真结果表明,该控制方法具有较强的自适应和抗干扰能力。     

非线性系统的神经网络自适应逆控制

提出了非线性系统的神经网络自适应逆控制方法。设计中使用了2个神经网络，经离线训练的NN1实现非线性系统的逆，在线网络NN2用于补偿逆误差和系统的动态特性变化，对一非线性系统的仿真结果表明，神经网络自适应逆控制能够提高系统的动态性能，并且具有较好的鲁棒性。     

一种基于 DTFEL的非线性自适应逆控制

提出一种基于离散时间反馈误差学习(DTFEL)的两自由度非线性自适应逆控制(AIC)方法,其控制器由动态RBF神经网络(DRBFNN)前馈控制器和参数固定的PD 反馈控制器构成.PD 控制器用来保证闭环系统稳定,动态 RBF神经网络以 PD控制器输出和反馈误差的线性组合为学习信号,通过一种改进的 NLMS(VS MNLMS)算法在线学习和逼近对象的动态逆,提高反馈控制器的性能. 稳定性分析证明了该AIC 系统稳定. 数字仿真结果表明,该 AIC具有良好的自适应能力和鲁棒性,是一种有效的非线性控制方法.

     

输出非对称死区的非严格反馈非线性系统控制

本文研究了具有输出非对称死区和状态含未知控制方向的非严格反馈非线性系统, 设计了稳定的自适应 神经网络控制器. 首先, 针对输出非对称死区的问题, 本文采用死区逆的方法, 构造光滑模型逼近原死区模型. 其 次, 在控制器设计过程中, 基于障碍Lyapunov函数的构造, 动态面控制和反步法, 设计出自适应控制信号, 虚拟控制 信号和实际控制信号. 通过稳定性分析, 证明所设计的神经网络控制器可以保证闭环系统内所有信号是半全局一致 最终有界. 最后, 通过MATLAB数值仿真, 说明所设计控制器的有效性.     

无人机编队飞行神经网络自适应逆控制器设计

针对无人机编队飞行时存在的气动耦合和外部干扰等影响因素,提出基于“长-僚机”模式的神经网络自适应逆控制器设计方法.详细推导了气动耦合影响,建立了完整的编队飞行非线性数学模型,设计了非线性动态逆控制律,提出了改进的 BP 神经网络算法,自适应地逼近和在线补偿动态逆误差,改善了控制效果,并针对队形变换提出了简单有效的设计思想.仿真表明,该控制器能有效实现编队队形的保持或变换,控制系统结构具有良好的扩充性.     

基于小波神经网络的板形板厚综合系统逆控制

针对板形板厚综合系统具有强耦合、非线性、含纯滞后环节的特点,提出一种基于小波神经网络的逆控制方案.利用两个结构相同的小波神经网络构造Smith预估器,预估器的输入参数与时延阶次无关,能较好地解决小波神经网络对维数较为敏感的问题.采用神经网络逆控制的思想设计小波神经网络控制器,引入多步预测性能指标函数对控制器权值进行在线训练.仿真研究表明,该控制方案具有较快的响应速度和良好的动态性能.     

Iterative inversion of neural networks and its application toadaptive control

An iterative constrained inversion technique is used to find the control inputs to the plant. That is, rather than training a controller network and placing this network directly in the feedback or feedforward paths, the forward model of the plant is learned, and iterative inversion is performed on line to generate control commands. The control approach allows the controllers to respond online to changes in the plant dynamics. This approach also attempts to avoid the difficulty of analysis introduced by most current neural network controllers, which place the highly nonlinear neural network directly in the feedback path. A neural network-based model reference adaptive controller is also proposed for systems having significant dynamics between the control inputs and the observed (or desired) outputs and is demonstrated on a simple linear control system. These results are interpreted in terms of the need for a dither signal for on-line identification of dynamic systems.     

Adaptive Neural Network Control of Small Unmanned Aerial Rotorcraft

This paper proposes an online learning adaptive neural network for small unmanned aerial rotorcraft to improve control performance during flight. Based on state error information, the weight matrix of the adaptive neural network can be updated on line by using lyapunov function. Therefore, no prior training data is needed for the training of the adaptive neural network. Combined with feedback control, the adaptive neural network can construct the map between the state error information and disturbances to compensate for system disturbances. The effectiveness of the proposed method is validated by a series of simulations and flight tests. Compared with feedback control method, the adaptive neural network control method can estimate and eliminate disturbances quickly to yield a good tracking performance.     

高超声速飞行器的神经网络动态逆控制研究

针对通用的高超声速飞行器的纵向动力学设计一个神经网络动态逆补偿控制方法,并对其进行了分析;这种飞行器模型具有高度非线性、多变量、不稳定的特性,包括6个不确定参数;在4.5903km高度和15马赫的平衡巡航条件下的仿真研究,评价了飞行器对高度和空速的阶跃变化的响应;阶跃变化为速度30 m/s,高度40 m;通过仿真结果表明,采用神经网络补偿逆误差,弥补了非线性动态逆要求精确数学模型的缺点,而且可以简化动态逆控制律的设计,改善整个控制系统的性能。     

Nonlinear optimized adaptive trajectory control of helicopter

This paper attempts to develop an optimized adaptive trajectory control system for helicopters based on the dynamic inversion method. This control algorithm is implemented by three time-scale separation architectures. Pseudo control hedging (PCH) is used to protect the adaptive element from actuator saturation nonlinearities and also from the inner-outer-loop interaction. In addition, to augment the attitude control system, two online adaptive architectures that employ a neural network are used. By tuning the neural network based on the system model, a better and faster learning will be achieved, but this is a frustrating and time consuming process. Due to complexity in accurate tuning of neural network, this paper introduces a non-dominated sorting genetic algorithm II (NSGA-II) for off-line optimization of the neural network. Thus, in the proposed method, the neural network can compensate model inversion error caused by the deficiency of full knowledge of helicopter dynamics more accurately. The effectiveness of proposed method is demonstrated by numerical simulations.     

Real time adaptive nonlinear model inversion control of a twin rotor MIMO system using neural networks

This paper investigates the development and experimental implementation of an adaptive dynamic nonlinear model inversion control law for a Twin Rotor MIMO System (TRMS) using artificial neural networks. The TRMS is a highly nonlinear aerodynamic test rig with complex cross-coupled dynamics and therefore represents the control challenges of modern air vehicles. A highly nonlinear 1DOF mathematical model of the TRMS is considered in this study and a nonlinear inverse model is developed for the pitch channel of the system. An adaptive neural network element is integrated thereafter with the feedback control system to compensate for model inversion errors. The proposed on-line learning algorithm updates the weights and biases of the neural network using the error between the set-point and the real output. The real-time response of the method shows a satisfactory tracking performance in the presence of inversion errors caused by model uncertainty. The approach is therefore deemed to be suitable to apply real-time to other nonlinear systems with necessary modifications.     

Data-based construction of feedback-corrected nonlinear prediction model using feedback neural networks

We propose to fit a recurrent feedback neural network structure to input–output data through prediction error minimization. The recurrent feedback neural network structure takes the form of a nonlinear state estimator, which can compactly represent a multivariable dynamic system with stochastic inputs. The inclusion of the feedback error term as an input to the model allows the user to update the model based on feedback measurements in real-time uses. The model can be useful in a variety of applications including software sensing, process monitoring, and predictive control. A dynamic learning algorithm for training the recurrent neural network has been developed. Through some examples, we evaluate the efficacy of the proposed method and the prediction improvement achieved by the inclusion of the feedback error term.     

直接自适应动态递归模糊神经网络控制及其应用

针对某些仿射非线性系统中各状态变量间呈微分关系的特点,本文提出仅取某些可测状态变量 作为动态递归模糊神经网络(dynamic recurrent fuzzy neural network, DRFNN) 的输入,而由DRFNN 的反馈矩阵 描述系统内部动态关系的直接自适应DRFNN 控制算法,克服了将系统所有变量作为输入的传统模糊神经网 络(traditioanl fuzzy neural network, TFNN) 因某些不可测状态变量所导致的不可实现问题．在电液伺服系统中的 应用结果表明：直接自适应DRFNN 控制算法相对于TFNN 控制算法对系统稳态特性的改善具有较大的优越 性．     

基于BP神经网络的矿井提升机自校正容错PID控制

针对矿井提升机系统故障时动态性能难以用传统的解析方法获得的问题,提出了一种基于BP神经网络的矿井提升机自校正容错PID控制方法。该方法通过BP神经网络在线学习跟踪提升机系统的动态特性来预测系统输出值,并应用自适应控制中的自校正PID构建容错控制器,实现提升机系统故障下的稳定容错控制。仿真结果表明,该方法在提升机系统故障情况下能迅速跟踪系统故障状态,在线调整PID参数,快速恢复系统性能。     

Parallel Control for Optimal Tracking via Adaptive Dynamic Programming

This paper studies the problem of optimal parallel tracking control for continuous-time general nonlinear systems. Unlike existing optimal state feedback control, the control input of the optimal parallel control is introduced into the feedback system. However, due to the introduction of control input into the feedback system, the optimal state feedback control methods can not be applied directly. To address this problem, an augmented system and an augmented performance index function are proposed firstly. Thus, the general nonlinear system is transformed into an affine nonlinear system. The difference between the optimal parallel control and the optimal state feedback control is analyzed theoretically. It is proven that the optimal parallel control with the augmented performance index function can be seen as the suboptimal state feedback control with the traditional performance index function. Moreover, an adaptive dynamic programming (ADP) technique is utilized to implement the optimal parallel tracking control using a critic neural network (NN) to approximate the value function online. The stability analysis of the closed-loop system is performed using the Lyapunov theory, and the tracking error and NN weights errors are uniformly ultimately bounded (UUB). Also, the optimal parallel controller guarantees the continuity of the control input under the circumstance that there are finite jump discontinuities in the reference signals. Finally, the effectiveness of the developed optimal parallel control method is verified in two cases.