考虑LuGre 摩擦的伺服系统自适应模糊控制

针对摩擦非线性的存在会使伺服系统控制精度难以提高的问题,建立了考虑动态LuGre摩擦的伺服系统数学模型,在系统参数和负载转矩未知的情况下设计了自适应模糊控制器,用自适应模糊逻辑系统在线逼近包含LuGre摩擦在内的非线性环节,从而实现了伺服系统高精度的位置跟踪。利用Lyapunov函数证明了闭环系统的稳定性。仿真结果表明,该控制器能有效地补偿摩擦非线性的影响,并对负载转矩变化具有较强的鲁棒性。     

带有摩擦非线性的CMG框架伺服系统 有限时间自适应鲁棒控制

针对控制力矩陀螺框架伺服系统中存在的摩擦非线性及不确定性等问题,提出一种基于终端滑模的有限时间自适应鲁棒控制律,确保闭环控制系统跟踪误差能够在有限时间内快速收敛到包含原点在内的任意小邻域内.通过对不确定参数的在线估计提高系统对参数变化的鲁棒性,并抑制外部干扰及摩擦非线性带来的不利影响.采用Lyapunov稳定性理论对闭环控制系统的稳定性进行分析并证明.通过对陀螺框架伺服控制系统进行仿真来验证所提出的控制律的有效性.     

滑模自适应控制在光电稳定平台中的应用

针对高精度光电伺服稳定平台系统中摩擦和各种非线性干扰对跟踪精度的影响问题,提出了一种基于LuGre摩擦模型的积分型滑模自适应控制算法。首先建立了基于动态LuGre摩擦的伺服系统模型,根据LuGre模型,构造了一个非线性观测器来估计摩擦中的未知状态变量;然后设计积分型滑模自适应控制算法实现摩擦补偿和各种扰动的估计,通过设计最优的反馈控制律,保证了积分型滑模的收敛速度,并引入自适应思想设计滑模控制器,有效的减弱了滑模控制中的颤抖现象;最后利用Lyapunov理论证明了控制系统的稳定性。仿真结果表明:所提方法有效的抑制了摩擦等各种干扰对稳定平台系统的影响,在提高系统跟踪精度的同时增强了系统的鲁棒性能,该方法也简化了设计过程,具有一定的应用价值。     

LuGre摩擦模型对伺服系统的影响与补偿

摩擦是影响伺服系统性能的一个主要因素. 为了研究摩擦的影响与补偿, 本文首先建立了基于动态LuGre摩擦的机电伺服系统模型. 根据LuGre模型, 构造了一个非线性观测器来估计摩擦力矩. 然后, 积分反步自适应控制算法被设计从而实现了摩擦补偿和负载扰动估计, 并使用Lyapunov函数证明了闭环系统的稳定性. 仿真结果表明:LuGre摩擦会对伺服系统产生极限环振荡以及低速爬行的影响, 并且提出的补偿方法能够降低摩擦对伺服系统性能的影响以及提高了系统的跟踪精度和鲁棒性.     

基于LuGre 摩擦模型的机械臂模糊神经网络控制

针对未知摩擦非线性会使机械臂控制精度难以提高的缺陷,建立基于动态LuGre摩擦的机械臂模型.在系统参数未知和机械臂负载变化的情况下,设计一种自适应模糊神经网络控制器,采用基函数中心和宽度均自适应变化的模糊神经网络补偿器,实现对系统中包括LuGre摩擦在内的非线性环节的逼近,并利用滑模控制项减小逼近误差.通过Lyapunov方法证明了闭环系统的稳定性,并通过仿真结果验证了所提出控制方法的有效性.     

SGCMGs驱动的挠性航天器有限时间自适应鲁棒控制

针对挠性航天器系统中同时存在单框架控制力矩陀螺群(Single gimbaled control moment gyroscopes, SGCMGs) 摩擦非线性、电磁干扰力矩、惯量摄动以及外部干扰等问题, 提出了一种有限时间自适应鲁棒控制(Finite-time adaptive robust control, FTARC) 方法. 针对系统中存在未知参数的情况, 分别设计自适应更新律, 使得控制器的设计不依赖参数信息, 同时减小外部干扰对系统的不利影响. 应用Lyapunov稳定性理论证明了闭环系统姿态角误差和姿态角速度误差可在有限时间内收敛到原点附近的邻域内. 仿真结果表明, 所提控制律可实现挠性航天器姿态快速机动, 并获得甚高指向精度.     

基于不确定逼近的机械手自适应鲁棒预测控制

针对具有参数不确定性和未知外部干扰的机械手轨迹跟踪问题提出了一种多输入多输出自适应鲁棒预测控制方法. 首先根据机械手模型设计非线性鲁棒预测控制律, 并在控制律中引入监督控制项; 然后利用函数逼近的方法逼近控制律中因模型不确定性以及外部干扰引起的未知项. 理论证明了所设计的控制律能够使机械手无静差跟踪期望的关节角轨迹. 仿真验证了本文设计方法的有效性.     

运动控制中的鲁棒自适应死区补偿

在高精度PD控制器中,死区可能会产生极限环,而且,死区参数往往未知.本文针对有非对称死区的直流伺服系统,设计了一种鲁棒自适应预补偿控制器,这种控制器不仅对死区的不确定性具有鲁棒性,而且对惯性及粘性摩擦等参数的不确定性,及外部扰动都有较强的鲁棒性.采用Lyapunov理论证明了这种控制器能够保证跟踪误差一致最终有界.并且调整调节控制器的参数可以改变跟踪误差.仿真结果表明了这种方法的有效性.     

机械伺服系统基于模糊神经网络的复合控制

惯性参数大范围变化和低速状态下的非线性摩擦是制约机械伺服系统跟踪性能的主要因素,基于LuGre动态摩擦模型和干扰观测器的补偿控制可以实现非线性摩擦力矩的动态补偿,但状态观测器的设计是基于被控对象的数学模型,当负载惯性参数大范围变化时,上述控制系统性能无法保障,针对上述问题提出一种基于模糊神经网络补偿的状态观测器复合控制,分析了基于模糊神经网络补偿复合控制的理论与实现方法,并以直流电机飞行仿真转台作为被控对象进行了仿真试验,试验结果表明了控制方法的有效性。     

光电平台低速自适应摩擦补偿的研究

关于优化光电平台的稳定性控制问题,由于摩擦干扰引起平台低速不稳定.针对系统非线性摩擦对光电平台伺服系统低速性能的影响,为了提高平台跟踪系统的性能和准确定位,提出根据自适应控制理论、李雅普诺夫稳定理论和库仑摩擦模型,用Stribeck摩擦模型的摩擦补偿方法进行了系统设计.对自适应控制算法进行补偿的效果,进行仿真,结果证明Stri-beck摩擦模型的摩擦补偿算法效果好,接近工程实际,平台伺服系统的低速性能得到了改善和提高,为设计提供了依据.     

Robust adaptive attitude control for flexible spacecraft in the presence of SGCMG friction nonlinearity

This paper investigates attitude maneuver control issues of a flexible spacecraft with pyramid‐type single gimbaled control moment gyroscopes (SGCMGs) as the actuator. The LuGre friction model is adopted to precisely describe the nonlinearity of the SGCMG gimbal friction. Aiming at restraining the adverse effects of the friction existed in SGCMG on the attitude control performance, a robust adaptive attitude controller is proposed, and projection‐based adaptive laws are presented to estimate the friction parametric uncertainties and the bound of friction nonlinearity. By treating the flexible mode coupling effect and external disturbances as lump disturbances, the inertia uncertainties and the bound of the lump disturbances are also estimated and compensated simultaneously to reduce their adverse effect on the system. With the Lyapunov technique, the states of flexible spacecraft control system are proved to be uniformly ultimately bounded. Numerical simulations demonstrate the effectiveness of the proposed scheme.     

基于不确定逼近的机械手间接自适应鲁棒预测控制

为了使机械手系统在含有模型不确定项时具有良好的跟踪性能和较强的抗干扰能力,提出了一种间接自适应鲁棒预测控制。首先,针对机械手模型设计出非线性鲁棒预测控制器;然后,基于三次样条函数逼近控制律中因模型不确定性产生的未知项,并在控制律中引入一个D-控制项抑制外部干扰。理论证明了所设计的控制器能够使跟踪误差收敛到原点。仿真验证了所提方法的有效性。     

具有输入饱和的近空间飞行器鲁棒控制

针对近空间飞行器这一类存在外部扰动,输入饱和和参数不确定的多输入多输出线性系统,提出了一种基于干扰观测器的抗饱和鲁棒控制方案.将干扰观测器与抗饱和控制技术相结合,从而消除系统存在的未知外部扰动、输入饱和和不确定性对系统控制的影响.首先,设计干扰观测器对线性外部系统产生的未知扰动进行估计.然后根据干扰观测器输出,通过超前抗饱和方法设计抗饱和补偿器,并将其加入到鲁棒控制器的设计中,保证闭环系统存在输入饱和、未知外部扰动和参数不确定情况下的稳定性.为便于设计,干扰观测器、抗饱和补偿器和控制器设计矩阵均通过求解线性矩阵不等式得到.最后,将提出的鲁棒抗饱和控制方法应用于近空间飞行器,仿真结果验证了该控制方案的有效性.     

Adaptive integral backstepping sliding mode control for opto-electronic tracking system based on modified LuGre friction model

In order to improve the control accuracy and stability of opto-electronic tracking system fixed on reef or airport under friction and external disturbance conditions, adaptive integral backstepping sliding mode control approach with friction compensation is developed to achieve accurate and stable tracking for fast moving target. The nonlinear observer and slide mode controller based on modified LuGre model with friction compensation can effectively reduce the influence of nonlinear friction and disturbance of this servo system. The stability of the closed-loop system is guaranteed by Lyapunov theory. The steady-state error of the system is eliminated by integral action. The adaptive integral backstepping sliding mode controller and its performance are validated by a nonlinear modified LuGre dynamic model of the opto-electronic tracking system in simulation and practical experiments. The experiment results demonstrate that the proposed controller can effectively realise the accuracy and stability control of opto-electronic tracking system.     

Robust adaptive controller with disturbance observer for vehicular radar servo system

In vehicular radar servo system, parameter variations of the executive motor and external disturbance uncertainties have great effects on the position tracking precision of the system. In this paper, a robust adaptive controller with disturbance observer is designed for vehicular radar servo system, which combines the merits of disturbance observer, adaptive backstepping method and sliding mode control. The system is modeled, and a disturbance observer is employed to observe and compensate for the unknown uncertainties. Adaptive backstepping method is used to design the sliding model controller to guarantee the global stability of the overall system. Simulation results show that the proposed robust adaptive controller has good performance in position tracking and enhances the robustness of vehicular radar servo system while observing the uncertainties precisely and quickly.     

Robust and adaptive variable structure output feedback control of uncertain systems with input nonlinearity

This brief proposes a robust control algorithm for stabilization of a three-axis stabilized flexible spacecraft in the presence of parametric uncertainty, external disturbances and control input nonlinearity/dead-zone. The designed controller based on adaptive variable structure output feedback control satisfies the global reaching condition of sliding mode and ensures that the system state globally converges to the sliding mode. A modified version of the proposed control law is also designed for adapting the unknown upper bounds of the lumped uncertainties and perturbations. The stability of the system under the modified control law is established. Numerical simulations show that the precise attitude pointing and vibration suppression can be accomplished using the derived robust or adaptive controller.     

High-order sliding-mode observer based output feedback adaptive robust control of a launching platform with backstepping

A kind of launching platform driven by two permanent magnet synchronous motor (PMSM) motors which is used to launch kinetic load to hit the target, always faces strong parameter uncertainties and strong external disturbance such as the air current impulsion, which would degrade their tracking accuracy greatly. In this paper, an adaptive robust nonlinear controller is proposed for high-accuracy motion control of the launching platform, in which the adaption law is designed to estimate the unknown coupling coefficients of torque disturbance and feed-forward cancellation technique is used to compensate the coupling torque disturbance and some other constant disturbances. In addition, a nonlinear robust feedback term is designed to inhibit the influence of the parameter estimation error and the other model uncertainty to stabilise the closed-loop system. Considering that some system states are immeasurable due to cost-reduction, volume/weight limitations and structure restriction or heavy measurement noise is usually associated with the measurements, which may also deteriorate the achievable performance of full-state feedback controllers; a high-order sliding-mode observer is used to estimate the unmeasured system states, and it is synthesised with the adaptive robust controller via feed-forward cancellation method. The intermediary virtual control law and the final control law are derived by integrating the backstepping method. Furthermore, the controller theoretically guarantees a prescribed tracking transient performance and final tracking accuracy while achieving asymptotic tracking performance in the presence of parametric uncertainties only, which is very important for high-accuracy tracking control of launching platform. Extensive comparative experimental results are obtained to verify the high performance nature of the proposed control strategy.