STUDY ON DYNAMICS, STABILITY AND CONTROL OF MULTI-BODY FLEXIBLE STRUCTURE SYSTEM IN FUNCTIONAL SPACE

The dynamics, stability and control problem of a kind of infinite dimensional system are studied in the functional space with the method of modern Mathematics. First, the dynamical control model of the distributed parameter system with multi-body flexible and multi-topological structure was established which has damping, gyroscopic parts and constrained damping. Secondly, the necessary and sufficient condition of controllability and observability, the stability theory and asymptotic property of the system were obtained. These results expand the theory of the field about the dynamics and control of the system with multi-body flexible structure, and have important engineering significance.

Adaptable and Dynamic Access Control Decision-Enforcement Approach Based on Multilayer Hybrid Deep Learning Techniques in BYOD Environment

Organizations are adopting the Bring Your Own Device(BYOD)concept to enhance productivity and reduce expenses.However,this trend introduces security challenges,such as unauthorized access.Traditional access control systems,such as Attribute-Based Access Control(ABAC)and Role-Based Access Control(RBAC),are limited in their ability to enforce access decisions due to the variability and dynamism of attributes related to users and resources.This paper proposes a method for enforcing access decisions that is adaptable and dynamic,based on multilayer hybrid deep learning techniques,particularly the Tabular Deep Neural Network Tabular DNN method.This technique transforms all input attributes in an access request into a binary classification(allow or deny)using multiple layers,ensuring accurate and efficient access decision-making.The proposed solution was evaluated using the Kaggle Amazon access control policy dataset and demonstrated its effectiveness by achieving a 94%accuracy rate.Additionally,the proposed solution enhances the implementation of access decisions based on a variety of resource and user attributes while ensuring privacy through indirect communication with the Policy Administration Point(PAP).This solution significantly improves the flexibility of access control systems,making themmore dynamic and adaptable to the evolving needs ofmodern organizations.Furthermore,it offers a scalable approach to manage the complexities associated with the BYOD environment,providing a robust framework for secure and efficient access management.

Three-dimensional Numerical Simulation of the Movement of the Flexible Body under Different Constraints

For the large deformation of the flexible body may cause the fluid grid distortion,which will make the numerical calculation tedious,even to end,the numerical simulation of the flexible body coupling with the fluid is always a tough problem.In this paper,the flexible body is under two kinds of constrained conditions and the ratio of length-diameter is 1:30.The Reynolds number of the airflow is 513,belonging to the area of low Reynolds number.The control equations of the coupling of flexible body with airflow are built and the adaptive grid control method is adopted to conduct the three-dimensional numerical simulation of the movement of the flexible body.The numerical results show that it is possible to simulate the characteristics of the flexible body's movement in the low Reynolds number airflow when the appropriate control equations are modeled and suitable equation-solving method is adopted.Unconstrained flexible body would turn over forward along the airflow's diffusion direction,while constrained flexible body in the flow field will make periodic rotation motion along the axis of the flexible body,and the bending deformation is more obvious than that of unconstrained flexible body.The preliminary three-dimensional numerical simulation can provide references for further research on the characteristics of the yam movement in high Reynolds number airflow.

Attitude tracking control of flexible spacecraft with large amplitude slosh

This paper is focused on attitude tracking control of a spacecraft that is equipped with flexible appendage and partially filled liquid propellant tank. The large amplitude liquid slosh is included by using a moving pulsating ball model that is further improved to estimate the settling location of liquid in microgravity or a zero-g environment. The flexible appendage is modelled as a three-dimensional Bernoulli–Euler beam, and the assumed modal method is employed.A hybrid controller that combines sliding mode control with an adaptive algorithm is designed for spacecraft to perform attitude tracking. The proposed controller has proved to be asymptotically stable. A nonlinear model for the overall coupled system including spacecraft attitude dynamics,liquid slosh, structural vibration and control action is established. Numerical simulation results are presented to show the dynamic behaviors of the coupled system and to verify the effectiveness of the control approach when the spacecraft undergoes the disturbance produced by large amplitude slosh and appendage vibration. Lastly, the designed adaptive algorithm is found to be effective to improve the precision of attitude tracking.

Model Based Adaptive Control and Disturbance Compensation for Underwater Vehicles

Underwater vehicles are being emphasized as highly integrated and intelligent devices for a significant number of oceanic operations. However, their precise operation is usually hindered by disturbances from a tether or manipulator because their propellers are unable to realize a stable suspension. A dynamic multi-body model-based adaptive controller was designed to allow the controller of the vehicle to observe and compensate for disturbances from a tether or manipulator. Disturbances, including those from a tether or manipulator, are deduced for the observation of the controller. An analysis of a tether disturbance covers the conditions of the surface, the underwater area, and the vehicle end point. Interactions between the vehicle and manipulator are mainly composed of coupling forces and restoring moments.To verify the robustness of the controller, path-following experiments on a streamlined autonomous underwater vehicle experiencing various disturbances were conducted in Song Hua Lake in China. Furthermore,path-following experiments for a tethered open frame remote operated vehicle were verified for accurate cruising with a controller and an observer, and vehicle and manipulator coordinate motion control during the simulation and experiments verified the effectiveness of the controller and observer for underwater operation. This study provides instructions for the control of an underwater vehicle experiencing disturbances from a tether or manipulator.

基于直流电压动态修正的柔性多状态开关自适应下垂控制

为了满足配电网的多种互联需求,柔性多状态开关(flexible multi-state switch,FMSS)已衍生出多种互联应用的技术形态,多端FMSS与双端FMSS相比更具经济性和可靠性,已成为研究热点。传统下垂控制通过改变直流侧电压实现不平衡功率的消纳,但直流侧电压的偏离会影响系统安全可靠运行。针对模块化多电平换流器(modular multilevel converter,MMC)的多端FMSS系统,提出了一种改进型下垂控制策略,根据换流器消纳的有功功率实时动态改变直流电压的参考值和下垂增益,实现了直流电压的无偏差运行,既能避免换流站过载,又能解决不平衡功率消纳引起的电压偏离问题,提高了系统的稳定性。另外,由于MMC自身结构特性和PI参数整定困难,将传统的电流内环改为模型预测控制,并采用典型的二阶Runge-Kutta法对状态方程进行离散化,提高了控制精度。最后基于MATLAB/Simulink仿真软件搭建了四端FMSS系统模型,验证了所提控制策略的可行性与有效性。

多自由度柔性机械臂非线性连续时变反馈控制方法

针对当前多自由度柔性机械臂控制过程中,机械臂定位控制系数选择合理性较低,导致多自由度柔性机械臂控制时延较长且运动轨迹与预设轨迹存在较大差异的问题,提出多自由度柔性机械臂非线性连续时变反馈控制方法。将拉格朗日算子作为计算基础,以能量的方式构建多自由度柔性机械臂动力学模型。考虑到机械臂的负载状态,计算机械臂的重力矩,识别机械臂非线性连续时变反馈控制参数。设定非线性连续时变反馈控制规则,构建机械臂非线性控制器,实现机械臂定位控制。构建实验环节,实验结果表明:该方法可有效提升机械臂运动轨迹与预设轨迹的一致性,缩短机械臂定位控制时延,进一步提升机械臂应用效果。

A novel variable topology design for a multi-flexible ejection mechanism

The airborne missile launch mechanism often subjects to significant deformations induced by the large ejection force during high-speed actuations in missile ejection process,leading to a substantial deviation of separation parameters from designed values that threats safety of the carrier.This study proposes a novel variable topology design for launch mechanism,achieved via a Prsmatic-Revolute-Revolute pair(PR-R)motion formed by the structural gap with a specific direction.It enables launch mechanism variability during missile ejection process and optimizes the ejection force given by the front and back ejection arms,and greatly optimizes the separation parameters during missile ejection.The kinetics simulation analysis is conducted under working conditions of the original ejection mechanism and the novel mechanism with variable topology design,respectively.The results show that the novel variable topology design is more befitting for the launch process in terms of system safety and controllability,effectively improving the separation posture,restraining the flexible effect of the mechanism,and fulfilling the effectiveness of the design value of multi-rigid body.

柔性关节的复合动态面控制仿真研究

针对柔性关节机械臂轨迹跟踪控制中存在参数不确定性、建模误差和未知扰动等问题,为了保证柔性关节系统的控制精度,在建立其等效动力学模型的基础上,提出了一种新的复合动态面控制策略.该策略包含动态面控制技术、参数自适应算法、神经网络逼近器、鲁棒补偿器以及约束处理方案.首先,利用动态面控制技术进行控制器的设计,消除了反步法的“复杂性爆炸”问题.其次,采用参数自适应算法处理柔性关节系统动力学模型中的参数不确定性,神经网络逼近器用于在线逼近和补偿模型中的不连续摩擦、建模误差和未知扰动,鲁棒补偿器负责前两部分的残余误差,同时设计约束处理方案满足误差规定性能约束和提高控制器对神经网络近似误差和未知扰动的鲁棒性.再次,构建具有预测误差的复合学习自适应律,提高控制器对模型不确定项的补偿精度.李雅普诺夫稳定性分析表明,所提出的策略保证了闭环系统中的所有信号都是半全局一致最终有界的,跟踪误差最终以规定性能收敛到零附近的一个小邻域.最后,在Simulink环境中,基于单连杆柔性关节系统对该控制策略进行对比仿真验证,结果表明:该复合动态面控制策略能够显著提高柔性关节系统的跟踪性能并降低其超调量和稳定时间,验证了该复合动态面控制策略的有效性和优越性.

大型抛物柱面天线展开动力学分析与展开过程控制

为揭示大型抛物柱面天线在轨展开过程中各部件的动力学特性,保障可展天线在轨展开过程稳定性,提出了一种基于模块组装的大型抛物柱面可展天线支撑机构动力学快速建模方法与非线性展开过程反馈控制策略。首先,基于绝对节点坐标法建立了天线可展支撑机构基本模块的动力学方程集与约束方程集。然后,通过子模块组装的方式实现对超大型支撑机构的动力学快速建模,并进一步提出逐块缩聚与递归的动力学微分方程高效求解算法。最后,基于非线性展开过程反馈控制策略实现了抛物柱面可展支撑机构该类强非线性系统的展开稳定控制。结果表明,该控制方法能显著降低可展支撑机构展开过程中的速度峰值,有效提高了大型抛物柱面天线展开过程中的展开同步性。

一种新型商用车驾驶室多轴道路虚拟试验研究

为了提高商用车驾驶室多轴道路模拟试验台的控制精度,精确复现路谱采集信号,提出了一种基于运动学与动力学分析的驾驶室多轴道路虚拟试验台控制策略。依据机构学原理描述了试验台的结构,并进行了运动学分析和计算,利用位姿反解算法及含雅可比矩阵正解算法进行了闭环反馈的自由度解耦。实测驾驶室相关参数并与ADAMS软件相结合建立了驾驶室、部分车架及试验台的刚柔耦合多体动力学模型,创建Femfat-lab、MATLAB/Simulink和ADAMS软件接口进行自适应联合仿真计算,实现了试验台的自由度解耦控制。将多轴虚拟试验台与实车试验内部响应信号相结合,选择信噪比较高的信号为目标信号进行迭代分析,获取实车位置等效位移激励。选取典型的比利时路面载荷谱作为模型输入条件,从而重现与道路试验相结合的真实路谱。研究结果表明,与室内道路模拟试验台架及常规虚拟迭代结果相比,驾驶室采用多轴虚拟试验台的迭代次数明显减少,得到的时域、频域响应信号与目标信号的变化趋势相吻合,且各通道相对误差均方根值(RMS)均小于设定值,迭代精度高,从而验证了所提方法的可行性,为后续驾驶室疲劳寿命预测提供了可靠的载荷谱。

全动舵系统柔性多体动力学建模方法

全动舵系统作为航天飞行器控制飞行姿态、调整飞行方向的部件,其动态特性对飞行器的正常工作起重要作用。为了开展带有电机伺服系统和舵轴间隙的全动舵系统动力学特性分析,提出基于柔性多体动力学方法的全动舵系统建模方法:采用Craig-Bampton方法建立典型舵面刚柔耦合降阶模型,采用多体动力学方法建立电动舵机连接机构与全动舵面连接,采用偶极子网格法建立基于模态的广义气动力模型。仿真结果表明,自建的模型预测颤振速度为1270 m/s,与商用软件预测对比的偏差小于2%,验证了该建模方法的正确、可行。研究表明,伺服系统的存在会令典型舵面响应存在较大跳跃现象,而舵轴间隙的存在则极大降低了舵面产生极限环振荡的临界速度。

多体柔性筛管水平井眼下入阻力分析

柔性筛管是超短半径水平井防砂的重要防砂工具,对于柔性筛管下入阻力的研究,有利于提高超短半径水平井技术的完井作业能力,提高采油效率。基于多体动力学理论,建立了柔性筛管井下运动时的数学模型,推导了筛管通过弯曲段的临界参数以及井下摩擦力的计算方法。采用ADAMS软件对柔性筛管进行仿真模拟,并基于柔性筛管的结构参数进行了动力学分析,确定了影响柔性筛管延伸能力的主要因素,揭示了在有限推力下,筛管单元长度以及井下作业环境对多体柔性筛管延伸长度的关系曲线,并给出了提高延伸能力的推荐方法。结果表明:较低的摩擦系数有利于提高井下柔性筛管的作业长度;在许用单元长度范围内,存在一个下入阻力最小的筛管单元长度的区间范围,能使多体柔性筛管的延伸能力达到最大;考虑井下柔性筛管摩擦力的累积速度,对柔性筛管进行局部减质量能达到提高延伸长度,同时降低作业成本的效果。研究成果可为提高水平井眼中运动柔性筛管的极限长度提供借鉴。

大型柔性航天器动力学与振动控制研究进展

随着航天重大工程的逐步实施,航天器正朝着超高速、超大尺度、多功能的方向发展,其面临的发射和运行环境也更加恶劣.航天器发射过程中的振动及其主/被动控制、在轨运行中大型柔性航天器动力学建模与动态响应分析、结构振动与飞行器姿态的混合控制等问题越来越复杂且难于处理;航天器结构的大型化和柔性化(如大阵面天线和太阳翼等)也对其地面试验和半实物仿真提出了挑战.本文着重介绍大型柔性航天器涉及到的动力学与振动控制问题,包括航天器发射过程中的整星隔振,大型柔性结构动力学建模与振动响应分析,大型柔性航天器的结构振动与姿轨控耦合动力学及其混合控制等.提炼出航天动力学与控制领域中亟待解决的若干基础科学问题,包括:多刚柔体系统动力学建模与模型降阶(涉及大变形柔性体动力学建模、多求解器合作仿真、模型降阶、组合结构动力学建模的解析方法等);复杂结构状态空间模型构建方法与能控性(涉及状态空间模型构建的理论与实验方法、复杂结构振动控制系统的能观性与能控性等);航天器姿态运动与大型柔性结构振动的混合控制律设计(涉及姿态机动与结构振动的鲁棒混合控制、执行机构与压电控制器的协同控制等).

多柔体系统碰撞动力学研究综述

多柔体系统碰撞动力学研究具有重要的研究价值和工程实际意义，本文针对多柔体系统碰撞动力学研究中的几个基本问题进行了全面的分析和评述，其中包括多柔体系统动力学方程的描述、碰撞模型的建立、铰接间隙引起的碰撞问题、数值算法、实验研究、控制等几个方面，并根据目前的发展现状和研究中存在的问题。

空间可展开天线结构研究进展

扼要综述了空间可展开天线结构的发展及目前的国际动态 ,叙述了空间可展开天线结构、设计及分析中的主要研究课题及其目前的进展。指出“把多体动力学与有限元法相结合的综合动力学建模法”、“辩识模型后 ,用预测控制和优化的思想进行展开过程控制”、“用多约束优化法调整网状天线反射面形状精度”

基于时变内流的柔性立管自适应边界控制

针对具有系统结构参数不确定的海洋柔性立管不确定性系统,为了提高其振动控制效果和品质,通过对立管结构参数进行估计,采用自适应控制技术和Lyapunov综合法,设计了自适应边界控制算法对耦合内流动力学的立管振动进行控制.所设计的自适应控制器能补偿系统参数不确定性,以及避免了控制溢出,并能保证系统的稳定性和一致有界性.仿真结果进一步验证了该控制算法对抑制立管振动的有效性.

一种挠性航天器的对偶四元数姿轨耦合控制方法

为解决复杂的挠性航天器的姿轨控制问题,对于挠性航天器的姿轨耦合动力学建模与控制展开研究。基于对偶四元数原理,推导给出一套挠性航天器的姿轨一体化动力学模型。此种模型能够紧凑描述航天器的轨道和姿态,且能够自动引入航天器平动、转动与挠性附件振动三者之间的关联耦合作用。基于此模型设计了一种自适应位置姿态跟踪控制器,该控制器能够在航天器质量特性参数未知的情况下,对其位置和姿态进行轨迹跟踪控制,并使位置和姿态误差收敛。该自适应控制器还可对航天器上挠性附件对系统的耦合作用进行估计,进而在控制输出中对其进行补偿,提高卫星控制系统的稳定性。通过仿真对控制律进行校验,结果表明该控制律对挠性航天器控制效果良好,具有一定的工程应用参考价值。

柔性机器人基于自适应模糊动态面的实用稳定控制

针对单连杆柔性机器人系统,提出了一种基于自适应模糊动态面的实用稳定控制方法。对于未知或时变函数,采用自适应模糊逼近,进而予以补偿。通过动态面控制避免了Backstepping设计带来的计算膨胀问题,简化了控制器的结构。所设计的控制器保证了闭环系统的实用稳定性。仿真结果验证了所提出控制器的有效性。

柔性多体卫星自抗扰控制系统的研究

设计了一种新型的姿态控制器—姿态自抗扰控制器。采用简化了的刚体动力学模型,即把柔性太阳帆板与柔性天线等的振动都看作外干扰,对象的不确定性、未建模动态与外干扰的总量都由自抗扰控制器估计出,再用该估计总量实现动态反馈补偿。该姿态控制器,只需控制输入转换矩阵的估计值,无需精确的卫星动力学模型。改变星体转动惯量或设置干扰力矩情况下的数学仿真表明,所设计的自抗扰控制器具有较小的稳态误差、较快的动态响应及对干扰有较强的抑制能力。