A Novel Robust Attitude Control for Quadrotor Aircraft Subject to Actuator Faults and Wind Gusts

A novel robust fault tolerant controller is developed for the problem of attitude control of a quadrotor aircraft in the presence of actuator faults and wind gusts in this paper. Firstly, a dynamical system of the quadrotor taking into account aerodynamical effects induced by lateral wind and actuator faults is considered using the Newton-Euler approach. Then, based on active disturbance rejection control (ADRC), the fault tolerant controller is proposed to recover faulty system and reject perturbations. The developed controller takes wind gusts, actuator faults and measurement noises as total perturbations which are estimated by improved extended state observer (ESO) and compensated by nonlinear feedback control law. So, the developed robust fault tolerant controller can successfully accomplish the tracking of the desired output values. Finally, some simulation studies are given to illustrate the effectiveness of fault recovery of the proposed scheme and also its ability to attenuate external disturbances that are introduced from environmental causes such as wind gusts and measurement noises.      

基于模型信息的电静液作动器降阶线性自抗扰控制

针对电静液作动器(electro-hydrostatic actuators, EHA)系统存在内外部扰动、参数不确定性和变控制增益等问题,提出一种基于模型信息的降阶线性自抗扰位置控制方法.首先,基于系统模型信息选取控制增益.其次,通过降阶线性扩张观测器对系统总扰动进行估计,并在控制器中加入扰动项进行补偿.利用奇异摄动理论证明所提控制器可使闭环系统是半全局最终一致有界的,并且当观测器带宽足够大时,所提出的控制器理论上可以使系统输出以所需精度跟踪期望轨迹.仿真结果表明,所提控制方法响应速度较快,控制精度较高,对外部扰动和参数不确定性具有较强的鲁棒性.     

含有非匹配干扰和未知动态的非仿射系统滑模控制算法

针对含有非匹配干扰和未知动态的非仿射系统控制问题,提出了一种基于扩张状态观测器(ESO)的改进滑模控制(SMC)方案.本文首先利用扩张状态观测器,将原系统转变为一个包含干扰的二阶积分级联系统,使含有未知动态的非仿射系统控制器设计问题转化为二阶积分级联系统的控制器设计问题,从而使得控制器在设计过程中不需要对对象模型完全已...     

考虑控制饱和的连铸结晶器振动位移系统预设性能控制

针对伺服电机驱动的连铸结晶器控制系统执行器输入饱和和状态受限问题,同时考虑系统存在负载扰动、参数摄动等不确定性问题,提出一种基于扩张状态观测器的跟踪误差预设性能反步控制策略.首先,针对执行器输入饱和问题,建立系统的数学模型;然后,采用一种线性扩张状态观测器实时观测系统时变负载扰动、参数摄动等不确定性,并对观测误差的收敛性进行分析;接着,针对伺服电机电流饱和与跟踪误差预设性能控制问题,通过引入辅助状态变量确保系统跟踪误差限定在允许范围内,设计基于扩张状态观测器的反步(Backstepping)控制器;最后,根据Lyapunov稳定性理论证明闭环系统的稳定性,并通过系统仿真验证所提出控制策略的有效性.     

柴油机油量执行器的干扰估计滑模控制方法

油量执行器是电控分配泵的核心部件之一,其直接控制着柴油发动机的燃油喷射量.模型非线性与外部扰动是油量执行器系统中不可避免的影响因素,前期的许多研究忽略了这些非线性,使得闭环系统性能并不理想.本文考虑了旋转电磁铁和复位弹簧等非线性特性的建模,得到了油量执行器系统的数学模型.进而,在基于模型对系统非线性进行抵消之后引入扩张状态观测器对系统外部干扰和不确定性进行估计,设计了基于扩张状态观测器的滑模控制律.该控制律在保证鲁棒性的同时,可以使得切换增益幅值更小,有利于减小滑模控制的抖振问题.最后,通过MATLAB/Simulink仿真和dSPACE平台实验验证了所提方法的可行性和有效性.     

Quaternion-based attitude synchronisation for multiple rigid bodies in the presence of actuator saturation

This paper concentrates on the quaternion-based attitude synchronisation problems of networked rigid bodies under fixed and undirected communication topology without relative angular measurements in the presence of actuator saturation. We first consider the leaderless attitude synchronisation problem with zero final angular velocity. In this case, we not only discuss the performance under the acyclic communication topology with the proposed bounded control algorithm, but also analyse that if there exist cycles in the topology, the proposed bounded algorithm guarantees that all equilibrium points are unstable except that the attitudes of networked rigid bodies achieve synchronisation. We also expand the result to the case of attitude tracking synchronisation with a static leader in the presence of actuator saturation. Next, the tracking synchronisation problem with the desired time-varying attitude is addressed in the presence of actuator saturation. Numerical examples are provided to validate the effectiveness of the proposed bounded schemes and illustrate the performances of multiple rigid bodies.     

基于扩张状态观测器的二质量系统非奇异快速终端滑模控制

针对含未知负载信息的二质量伺服系统,提出一种基于有限时间扩张状态观测器的非奇异快速终端滑模控制方法.首先,利用电机侧位置信息设计有限时间扩张状态观测器估计系统的扰动,并将估计值融入到控制器中作为前馈项对系统的未知扰动进行补偿;然后,引入一种新型的滑模趋近律,该趋近律能够避免传统滑模控制中存在的奇异性问题,据此设计非奇异快速终端滑模控制器,保证系统状态在有限时间内收敛到原点,并根据李雅普诺夫稳定性理论分析闭环系统的稳定性;最后,通过仿真和实验验证所提出方法的优越性.结果表明,与传统的PID等控制相比较,所提出的基于扩张状态观测器的有限时间滑模控制方法能够提高系统的跟踪性能,并有效增强二质量伺服系统的抗扰动能力.     

移动机器人的线性自抗扰控制设计与实验验证

为了实现移动机器人的高精度轨迹跟踪控制, 设计了一种基于扩张状态观测器的扰动抑制方法和相应的 实验验证平台. 首先, 考虑到不确定扰动如车轮纵向和侧向滑动对移动机器人系统控制性能的影响, 建立了受扰下 的运动学模型; 然后, 基于扩张后的运动学模型设计了扩张状态观测器来估计系统扰动; 接着, 利用扰动估计构建 了线性自抗扰控制器, 并利用Lyapunov函数证明了闭环系统的稳定性; 同时, 基于MATLAB/Simulink软件和微控制 器搭建了所推荐控制算法的实验验证平台. 最后, 仿真和实验结果都验证了所提出控制方法的有效性.     

大射电望远镜馈源指向系统轨迹跟踪自抗扰控制

采用独立控制策略实现新一代大射电望远镜馈源指向跟踪系统的高精度轨迹跟踪 .将两组成子系统之间的动力学耦合及其他扰动视为对精调Stewart平台子系统的未知扰动 ,设计了强鲁棒自抗扰控制器实现扰动补偿 .大射电望远镜馈源指向系统 5 0m缩比模型实验 ,验证了独立控制策略和自抗扰控制器的工程有效性和可行性 .为将来建造新一代大射电望远镜工程奠定了坚实的基础     

基于ESO的Buck型变换器趋近律控制

针对Buck型变换器系统中存在的时变干扰,如输出负载波动,本文提出一种基于扩张状态观测器(ESO)的趋近律控制方法。首先,对系统中存在的时变干扰进行建模,把抑制时变干扰问题转换为抑制匹配和非匹配扰动问题。其次,设计一种扩张状态观测器,用于估计匹配和非匹配扰动。然后,根据提出的新型指数幂次趋近律设计滑模控制器,结合ESO,有效抑制时变干扰对系统的影响,并通过Lyapunov稳定性定理分析观测器的收敛性和闭环控制系统的稳定性。最后,仿真结果验证了所提方法的有效性。     

带宽化扰动观测复合滑模的闭链机构协调控制

针对闭链机构关节协调控制问题,在耦合空间中提出了一种带宽化扰动观测器复合等速趋近律的滑模控制方法.扰动观测器保留扩张状态观测器的计算结构,使用观测误差的比例、积分、微分(P, I, D)估计扰动;它与滑模控制复合,不但放宽了滑模切换增益的边界条件,而且消除了抖振.使用等速趋近律,切换增益可根据执行器饱和限制条件计算获得,其他控制参数结合带宽参数化法整定.仿真和实验表明,带宽化扰动观测器复合滑模控制,可以在系统限制允许的范围内有效解决闭链机构协调控制问题,且具有参数物理意义明确,易整定的优点.     

考虑有执行器故障和有界扰动的鲁棒自适应容错补偿控制

考虑在执行器故障和外界干扰下, 用直接自适应状态反馈控制策略解决线性时不变连续时间系统的鲁棒容错补偿控制问题. 提出更一般且更实际的执行器故障模型. 在执行器故障和扰动的上界都未知下, 提出自适应律在线估计未知控制器参数. 然后基于自适应策略的信息, 构造一类鲁棒自适应状态反馈控制器自动补偿故障和扰动的影响. 基于李亚普诺夫定理, 在执行器故障和干扰下, 所得的自适应闭环系统可以被保证渐进稳定. 最后给出一个火箭整流罩模型的例子和它的仿真结果.     

Error-constrained path-following control for a stratospheric airship with actuator saturation and disturbances

This paper is concerned with the path-following control problem for an under-actuated stratospheric airship with error constraint, actuator saturation, and external disturbances. To address the tracking error-constrained requirements of airship position and attitude, novel tan-type barrier Lyapunov functions are proposed and incorporated with the guidance and attitude control schemes, which calculate the desired attitude and angular velocity. An auxiliary design system in the form of anti-windup compensator is employed to deal with actuator saturation, and the stability of the saturated control solution is verified. Nonlinear disturbance observer is developed to estimate the unknown external disturbances. Rigorous stability analysis shows that the constrained requirements on the airship position and attitude will not be violated under the proposed control method and all closed-loop signals are uniformly ultimately bounded, despite the presence of actuator saturation and disturbances. Simulation results and comparisons illustrate the effectiveness of the proposed controller.     

压电驱动纳米定位台的线性自抗扰控制

压电驱动的纳米定位系统,磁滞严重降低其定位精度.基于磁滞逆模型的定位控制方法,可提高定位精度.然而,因其对模型依赖大,无法在内、外扰动因素存在时,仍保证良好的定位效果.为此,视磁滞为干扰,设计不基于磁滞及定位系统精确数学模型的自抗扰控制,利用扩张状态观测器主动估计磁滞,并实时补偿之,以保证定位精度.本文分析了扩张状态观测器的收敛性、闭环系统的稳定性;讨论了自抗扰控制参数与纳米定位系统动态响应间的关系;对比了PI控制和自抗扰控制的动态响应、时间与误差绝对值乘积积分、平均绝对误差和均方根误差,数值和实验结果均表明自抗扰控制优于PI控制,证实了自抗扰控制可主动估计磁滞、内部不确定性和外部扰动,在其降低定位精度之前即被补偿、保证良好的定位控制效果.     

An adaptive control architecture for leader–follower multiagent systems with stochastic disturbances and sensor and actuator attacks

In this paper, we develop a novel distributed adaptive control architecture for addressing networked multiagent systems subject to stochastic exogenous disturbances with compromised sensor and actuators. Specifically, for a class of linear leader–follower multiagent systems, we develop a new structure of the neighbourhood synchronisation error for the control design protocol of each follower. The proposed control algorithm addresses time-varying multiplicative sensor attacks on the leader state measurements. In addition, the framework addresses time-varying multiplicative actuator attacks on the followers that do not have a communication link with the leader and additive actuator attacks on all follower agents in the network. The proposed adaptive controller guarantees uniform ultimate boundedness of the state tracking error for each agent in a mean-square sense.     

Fault detection for output feedback control systems with actuator stuck faults: A steady‐state‐based approach

The paper studies the fault detection problem for output feedback control systems with bounded disturbances and nonzero constant reference inputs. A steady‐state‐based approach is proposed which can be used to detect small actuator stuck faults including actuator outage (the stuck value is zero). These small stuck faults, especially the outage faults, cannot be detected effectively using the existing techniques. A dynamic output feedback controller and a weighting matrix are designed simultaneously. The dynamic output feedback controller stabilizes the closed‐loop system for both fault‐free and faulty cases and attenuates the effects of disturbances. By manipulating the steady‐state values of system states with the detection weighting matrix, a residual is then generated, through which actuator stuck faults including actuator outages can be detected effectively. Simulation results are included to demonstrate our design procedure. Copyright © 2009 John Wiley & Sons, Ltd.     

双电机同步驱动伺服系统故障诊断与容错控制

本文针对双电机同步驱动伺服系统中执行器失效会导致系统性能下降甚至失稳的情况,提出了一种基于自适应滑模的故障诊断和容错控制策略.该方法通过设计各电机转速的自适应滑模状态观测器,在线估计各执行器的失效因子:当单个执行器部分失效时,通过自适应的方法调整控制器增益;当单个执行器全部失效时,重构系统的控制律.对于系统中存在非匹配不确定项的情况,提出在期望虚拟信号中引入基于扩张状态观测器的补偿项抑制方案;利用Lyapunov理论证明了闭环系统在正常和故障状况下的稳定性以及观测器的收敛性;仿真结果表明,所设计的控制策略能保证系统稳定跟踪指令信号,在单个执行器失效的情况下系统跟踪性能基本不下降.     

一种新型电静液作动飞机刹车系统

多电飞机已成为现代飞机的发展趋势,其刹车系统不再采用传统的液压刹车.提出一种用于多电飞机刹车系统的泵控和阀控相结合的电静液刹车系统.首先分析了电静液作动器的工作原理和数学模型,对电静液机构进行了单独的控制仿真;接着对飞机刹车系统进行数学建模,并将这种电静液作动飞机刹车系统进行控制仿真.仿真结果表明,基于电静液作动器的刹...     

Extended state observer-based pressure control for pneumatic actuator servo systems

A pneumatic actuator is a fast and economical tool that converts compressed air into mechanical motion.In this paper,an extended state observer(ESO)-based slidi...     

基于双曲正切函数的二阶时变参数扩张状态观测器

当传统扩张状态观测器(ESO)的状态初值与系统的状态初值相差较大时,普遍存在微分峰值现象.为了消除这种现象,本文给出了用双曲正切非线性函数构造ESO的一般形式,并且用Lyapunov函数证明了二阶ESO的误差系统为渐近稳定.然后又利用双曲正切函数自身的饱和特性,设计出一种时变ESO,可以实现微分峰值的有效抑制.最后,把这种ESO的仿真结果与经典ESO的仿真结果进行对比,表明这里提出的ESO能够有效抑制微分峰值现象,并可以获得系统状态变量和非线性扰动的精确估计.