Quantitative feedback theory and zero phase error tracking control combined robust control for radar truck leveling simulator

Radar leveling system is the key equipment for improving the radar mobility and survival capability. A combined quantitative feedback theory (QFT) controller is designed for the radar truck leveling simulator in this paper, which suffers from strong nonlinearities and system parameter uncertainties. QFT can reduce the plant uncertainties and stabilize the system, but it fails to obtain high-precision tracking. This drawback can be solved by a robust QFT control scheme based on zero phase error tracking control (ZPETC) compensation. The combined controller not only possesses high robustness, but greatly improves the system performance. To verify the effiectiveness and the potential of the proposed controller, a series of experiments have been carried out. Experimental results have demonstrated its robustness against a large range of parameters variation and high tracking precision performance, as well as its capability of restraining the load coupling among channels. The combined QFT controller can drive the radar truck leveling platform accurately, quickly and stably.

Nonlinear Attitude Tracking Control of a Spacecraft with Thrusters Based on Error Quaternions

The multi axis coupling attitude control of a spacecraft with thrusters for attitude tracking is investigated. The attitude kinematics and dynamics are both described by error quaternions. The four error quaternion dynamic equations are then transformed into four perturbed double integrators via linear transformations. An on off controller is designed based on the perturbed double integrators. The controller is determined by parabolic switching functions of the scalar error quaternion and the transfor...

Robust adaptive tracking control of robotic systems with uncertainties

To deal with the uncertainty factors of robotic systems, a robust adaptive tracking controller is proposed. The knowledge of the uncertainty factors is assumed to be unidentified; the proposed controller can guarantee robustness to parametric and dynamics uncertainties and can also reject any bounded, immeasurable disturbances entering the system. The stability of the proposed controller is proven by the Lyapunov method. The proposed controller can easily be implemented and the stability of the closed system can be ensured; the tracking error and adaptation parameter error are uniformly ultimately bounded （UUB）. Finally, some simulation examples are utilized to illustrate the control performance.

A hybrid multi-degree-of-freedom vibration isolation platform for spacecrafts by the linear active disturbance rejection control

The hybrid vibration isolation, which takes advantages of both the passive and active approaches, has been an important solution for space missions. The objective of this paper is to design a vibration isolation platform for payloads on spacecrafts with the robust, wide bandwidth, and multi-degree-of-freedom(MDOF). The proposed solution is based on a parallel mechanism with six voice-coil motors(VCMs) as the actuators. The linear active disturbance resistance control(LADRC) algorithm is used for the active control. Numerical simulation results show that the vibration isolation platform performs effectively over a wide bandwidth, and the resonance introduced by the passive isolation is eliminated. The system robustness to the uncertainties of the structure is also verified by simulation.

Decentralized PD Control for Non-uniform Motion of a Hamiltonian Hybrid System

In this paper, a decentralized proportional-derivative （PD） controller design for non-uniform motion of a Hamiltonian hybrid system is considered. A Hamiltonian hybrid system with the capability of producing a non-uniform motion is developed. The structural properties of the system are investigated by means of the theory of Hamiltonian systems. A relationship between the parameters of the system and the parameters of the proposed decentralized PD controller is shown to ensure local stability and tracking performance. Simulation results are included to show the obtained non-uniform motion.

Stabilizing Hybrid Stochastic Interval Systems by Feedback Controls

The problem of stabilizing a hybrid stochastic interval system is studied in this article. A hybrid interval system with suitable controls will become stable in the sense of mean-square exponential stability. State-feedback controls are designed based on the discrete-time state observations. Controls are put both in the drift and diffusion parts of the system. Criteria are derived in terms of linear matrix inequalities( LMI) to get the controllers. Also one example is given to illustrate our techniques.

Research on Airborne Electro-Optical Tracking and Sighting System Based on Fuzzy PID and H_∞ Control

Airborne electro-optical tracking and sighting system is a three-degree-of-freedom angular position servo system which is influenced by multi-disturbance,and its control system consists of stabilizing and tracking components.Stabilizing control is applied to track angular velocity order and control multi-disturbance under airborne condition,and its robustness should be very good;tracking control is applied to compensate tracking error of angular position.A mathematical model is established by taking the control of yaw loop as example.H∞ stabilizing controller is designed by taking the advantage of H∞ control robustness and combining with Kalman filter.A fuzzy control is introduced in general PID control to design a decoupled fuzzy Smith estimating PID controller for tracking control.Simulation research shows that the control effect of airborne electro-optical tracking and sighting system based on fuzzy PID and H∞ control is good,especially when the model parameters change and the multi-disturbance exists,the system capability has little fall,but this system still can effectively track a target.

Adaptive Sensor-Fault Tolerant Control of Unmanned Underwater Vehicles With Input Saturation

This paper investigates the tracking control problem for unmanned underwater vehicles(UUVs)systems with sensor faults,input saturation,and external disturbance caused by waves and ocean currents.An active sensor fault-tolerant control scheme is proposed.First,the developed method only requires the inertia matrix of the UUV,without other dynamic information,and can handle both additive and multiplicative sensor faults.Subsequently,an adaptive fault-tolerant controller is designed to achieve asymptotic tracking control of the UUV by employing robust integral of the sign of error feedback method.It is shown that the effect of sensor faults is online estimated and compensated by an adaptive estimator.With the proposed controller,the tracking error and estimation error can asymptotically converge to zero.Finally,simulation results are performed to demonstrate the effectiveness of the proposed method.

STUDY ON GAIN-SCHEDULING PROBLEM IN FLIGHT CONTROL

Gain-scheduling has got its wide applications in modern flight control, in which control gains are scheduled with variables such as dynamic pressure and Mach number, to meet dynamic response requirements in different flight conditions. Classical gain-scheduling approaches may result in some problems, which can not guarantee global robustness and stability in transitions of different flight conditions. Gain-scheduling problem is systematically investigated from robustness point of view in the paper. Detailed procedures for gain-scheduled controller to achieve both robustness and stability performance are given and applied to a typical flight control system. For switching stability problems of different flight conditions in flight control systems, a new approach is proposed, in which different flight conditions are reduced into a parameter varying plant using interpolation firstly, and then parameter-varying controller design goes next. Though interpolation errors may exist, the robust parameter varying controller design can compensate for those uncertainties and errors, and finally achieve good performance of robustness and switching stability during transitions. Illustrative simulation at last shows satisfactory results.

Robust backstepping global integral terminal sliding mode controller to enhance dynamic stability of hybrid AC/DC microgrids

In this paper,a Backstepping Global Integral Terminal Sliding Mode Controller(BGITSMC)with the view to enhancing the dynamic stability of a hybrid AC/DC microgrid has been presented.The proposed approach controls the switch-ing signals of the inverter,interlinking the DC-bus with the AC-bus in an AC/DC microgrid for a seamless interface and regulation of the output power of renewable energy sources(Solar Photovoltaic unit,PMSG-based wind farm),and Battery Energy Storage System.The proposed control approach guarantees the dynamic stability of a hybrid AC/DC microgrid by regulating the associated states of the microgrid system to their intended values.The dynamic stabil-ity of the microgrid system with the proposed control law has been proved using the Control Lyapunov Function.A simulation analysis was performed on a test hybrid AC/DC microgrid system to demonstrate the performance of the proposed control strategy in terms of maintaining power balance while the system’s operating point changed.Furthermore,the superiority of the proposed approach has been demonstrated by comparing its performance with the existing Sliding Mode Control(SMC)approach for a hybrid AC/DC microgrid.

线性自抗扰控制系统的稳定性分析方法

针对二阶线性系统和二阶线性自抗扰控制,提出了基于误差的稳定性分析方法。该方法通过观测误差、跟踪误差状态量建立闭环系统状态空间模型,借助状态空间模型的特征值分析闭环系统的收敛性,并运用李雅普诺夫法判断系统的稳定性。与基于劳斯判据的稳定性分析方法相比较,二者的分析结论一致,算例和仿真结果验证了所提方法的简单性和有效性。此外,通过仿真和蒙特卡洛实验验证了自抗扰控制相比于PID控制在跟踪性能、抗扰能力和鲁棒性等方面的优势。

挖掘机液压混合动力系统跟踪控制研究

由于挖掘机混合动力系统参数的不确定性和系统的非线性给挖掘机的跟踪控制带来了巨大的困难。对此,构建了挖掘机液压混合动力系统模型,并采用改进的自适应鲁棒控制(ARC)实现挖掘机液压混合动力系统的跟踪控制。根据挖掘机液压混合动力系统,对液压系统、挖掘机动力学和发动机进行数学建模。利用线性稳定反馈控制规律,采用改进的自适应鲁棒控制,使挖掘机液压混合动力系统具有足够大的反馈增益。最后对斗杆、动臂和铲斗的倾角进行跟踪仿真实验,给出了系统模型位置和速度的跟踪误差,并与PI控制进行比较分析。结果表明:相比于PI控制,ARC控制下的斗杆、动臂和铲斗倾角的最大振幅波动率和倾角的波动范围都有所降低,且回转位置和速度的跟踪误差超调较小。说明采用ARC控制的挖掘机混合动力系统控制方法,能够更好的补偿系统模型的非线性,具有较好的控制稳定性以及跟踪精度。

基于高阶递归神经网络的AUV鲁棒控制方法

目的 提出一种基于高阶递归神经网络的AUV鲁棒控制方法。方法 利用结构简单但逼近效果优越的高阶递归神经网络,对建模不确定性和外部未知干扰进行估计,并将其补偿到输入控制律中,以提高控制性能。之后,基于HJI理论和Lyapunov稳定性分析导出神经网络权重自适应更新律和AUV自适应控制律,设计反步滑模方法作为对比方法,并进行仿真实验。结果 设计的基于高阶递归神经网络的AUV鲁棒控制方法的跟踪误差、调节时间等控制指标均优于反步滑模方法。设计的鲁棒控制方法可以控制AUV精确跟踪目标轨迹,同时具有优秀的控制性能和鲁棒性。结论 这一研究为AUV轨迹跟踪控制领域提供了一种高效且有效的方法,有望在复杂、不确定的水下环境中得到应用。

Stability and weighted sensitivity analysis of robust controller for heat exchanger

This study presents a parametric system identification approach to estimate the dynamics of a chemical plant from experimental data and develops a robust PID controller for the plant.Parametric system identification of the heat exchanger system has been carried out using experimental data and prediction error method.The estimated model of the heat exchanger system is a time-delay model and a robust PID controller for the time-delayed model has been designed considering weighted sensitivity criteria.The mathematical background of parametric system identification,stability analysis,and H∞ weighted sensitivity analysis have been provided in this paper.A graphical plot has been provided to determine the stability region in the(Kp,Ki),(Kp,Kd)and(KuKd)plane.The stability region is a locus dependent on parameters of the controller and frequency,in the parameter plane.

LCL并网逆变器改进型重复控制策略

对于采用"比例—积分(PI)+重复控制"的LCL并网逆变器控制系统进行了详细分析,并指出其动态性能仍有待进一步改善并且其补偿函数形式复杂,实现困难。结合零相位误差跟踪控制和干扰观测器,提出了一种改进型重复控制策略。一方面,利用零相位误差跟踪控制原理改善了重复控制系统的动态性能并且其补偿函数设计简单;另一方面利用干扰观测器克服了零相位误差跟踪控制参数依赖性强的缺点。最后,仿真和实验表明,与"PI+重复控制"相比较,所提控制策略在保证稳态控制精度的同时能够获得更好的动态性能,并且同样具有鲁棒性强的优点。

动态双足机器人的控制与优化研究进展

对动态双足机器人的可控周期步态的稳定性、鲁棒性和优化控制策略的国内外研究现状与发展趋势进行了探讨.首先,介绍动态双足机器人的动力学数学模型,进一步,提出动态双足机器人运动步态和控制系统原理;其次,讨论动态双足机器人可控周期步态稳定性现有的研究方法,分析这些方法中存在的缺点与不足;再次,研究动态双足机器人的可控周期步态优化控制策略,阐明各种策略的优缺点;最后,给出动态双足机器人研究领域的难点问题和未来工作,展望动态双足机器人可控周期步态与鲁棒稳定性及其应用的研究思路.

基于动态逆和鲁棒轨迹跟踪控制的导弹控制系统设计

基于动态逆方法及鲁棒轨迹跟踪控制理论提出了一种新的导弹控制系统设计方法。首先基于导弹的非线性模型设计快、较慢回路的动态逆控制器以实现其非线性解耦,然后在较慢回路中设计鲁棒控制律以补偿整个控制系统的总不确定性及干扰。即对较慢回路进行动态逆控制的基础上,通过引入一种辅助控制输入信号以抵消不确定性及外部干扰对系统性能的影响。稳定性分析表明了闭环系统稳定且系统跟踪误差能满足给定的性能指标。最后通过对所设计控制系统的仿真分析,验证了该方法的有效性。

光电跟踪系统快速捕获时间最优滑模控制技术

针对光电跟踪系统目标的快速捕获过程,本文提出了时间最优滑模控制方法。该控制的滑模面函数为时间最优控制系统状态最优运动轨迹,保证系统状态变量沿着最优轨迹滑动;设计相应的指数趋紧率,使状态变量快速平稳趋近滑模面。以180°、90°、60°阶跃信号为捕获目标进行仿真与实验研究,实验结果为时间最优滑模控制调节时间比时间最优控制和滑模控制分别减小了约43.66%、59.67%,超调量为0,稳态波动量为0,稳态误差减小了约为44.94%和62.34%,与仿真结果相吻合。结果表明该方法调节时间短,超调小,稳态值平稳,稳态误差小,鲁棒性强等优点适合应用于光电跟踪系统目标快速捕获,具有重要的研究与应用价值。

改进的强跟踪滤波算法及其在3PTT-2R伺服系统中的应用

为解决3PTT-2R伺服系统由于模型不准确和负载扰动而引起的控制精度下降的问题,以5自由度3PTT-2R伺服系统为研究对象,建立包含执行系统、进给系统和驱动系统等若干子系统的3PTT-2R伺服系统数学模型,提出一种基于改进强跟踪滤波(Strong track filter,STF)的3PTT-2R伺服系统控制算法,并在理论上证明了稳定性.通过仿真分析,比较了STF、改进的STF算法稳定性,及对模型不确定性的鲁棒性,表明所提算法具有跟踪速度快、抑制噪声、精度高等优点.对试样进行表面粗糙度和表面轮廓度检测,实验结果进一步说明所建立的3PTT-2R伺服系统模型与实际非线性系统模型匹配,改进的STF算法具有较好的跟踪能力,鲁棒性强、控制精度高,进而提高了加工精度.

基于PD控制的机器人轨迹跟踪性能研究与比较

定义同一个 L yapunov函数 ,分析了基于 PD的 3种常用机器人轨迹跟踪算法的稳定性和鲁棒性 ,得到了新的结论。PD加前馈控制按指数收敛到 0 ,PD及修改的 PD加前馈控制收敛到一封闭球 ,增大反馈系数可使球半径任意小。基于 PD的轨迹跟踪算法对模型误差及有界不确定性干扰具有鲁棒性。实验研究验证了分析结果 ,并对 3种轨迹跟踪算法的控制性能进行比较。