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Boundary Control Problem of Infinite Order Distributed Hyperbolic Systems Involving Time Lags 被引量:2
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作者 Bahaa Gaber Mohamed 《Intelligent Control and Automation》 2012年第3期211-221,共11页
Various optimal boundary control problems for linear infinite order distributed hyperbolic systems involving constant time lags are considered. Constraints on controls are imposed. Necessary and sufficient optimality ... Various optimal boundary control problems for linear infinite order distributed hyperbolic systems involving constant time lags are considered. Constraints on controls are imposed. Necessary and sufficient optimality conditions for the Neumann problem with the quadratic performance functional are derived. 展开更多
关键词 boundary control (n × n) Hyperbolic Systems Time Lags DISTRIBUTED control problems NEUMANN Conditions Existence and UNIQUENESS of Solutions Infinite Order Operator
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An Optimization Problem of Boundary Type for Cooperative Hyperbolic Systems Involving Schrodinger Operator 被引量:1
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作者 Ahlam Hasan Qamlo 《Intelligent Control and Automation》 2014年第4期262-271,共10页
In this paper, we consider cooperative hyperbolic systems involving Schr?dinger operator defined on ?Rn. First we prove the existence and uniqueness of the state for these systems. Then we find the necessary and suffi... In this paper, we consider cooperative hyperbolic systems involving Schr?dinger operator defined on ?Rn. First we prove the existence and uniqueness of the state for these systems. Then we find the necessary and sufficient conditions of optimal control for such systems of the boundary type. We also find the necessary and sufficient conditions of optimal control for same systems when the observation is on the boundary. 展开更多
关键词 Hyperbolic Systems Schrodinger Operator boundary control problem boundary Observation COOPERATIVE
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Four Algorithms for Boundary Control with Breaking in Space and Time
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作者 Vladimir Arabadzhi 《Journal of Applied Mathematics and Physics》 2019年第11期2891-2901,共11页
Typically, active control systems either have a priori complete information about the boundary-value problem and damped waves before switching on, or get it during the measurement process or accumulate and update info... Typically, active control systems either have a priori complete information about the boundary-value problem and damped waves before switching on, or get it during the measurement process or accumulate and update information online (identification process in adaptive systems). In this case, the boundary problem is completely imprinted in the information arrays of the control system. However, very often complete information about a boundary-value problem is not available in principle or this info is changing in time faster than the process of its accumulation. The article considers examples of boundary control algorithms based almost without any information. The algorithms presented in the article cannot be obtained within the framework of the harmonic representation of the problem by complex amplitudes. And these algorithms carry out fast control in microstructured boundary problems. It is shown that in some cases it is possible to find simple solutions if we remove restrictions: 1) on the spatio-temporal resolution of controlling elements of a boundary-value problem;2) on the high-frequency radiation of the controlled boundary. 展开更多
关键词 INCIDENT Low FREQUENCY Wave High FREQUENCY Technological Radiation Fast control in Microstructured boundary problems Binary BREAKER Breaker-Inverter Length of Damping SPINNING Acoustic BLADES Gas Stream SEICHE Waves
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Skewperiodic Boundary Value Problems for Second Order Nonlinear Differential Equations
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作者 翟延慧 黄庆道 韩月才 《Northeastern Mathematical Journal》 CSCD 2002年第1期73-78,共6页
In this paper a uniqueness theorem for a skewperiodic boundary value problem is obtained. By using the optimal control method, we derive the best estimate for the integration mean ensuring that the results hold.
关键词 Skewperiodic boundary value problem optimal control theory Schauder's fixed point theorem.
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Global Optimization for Solving Linear Non-Quadratic Optimal Control Problems
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作者 Jinghao Zhu 《Journal of Applied Mathematics and Physics》 2016年第10期1859-1869,共11页
This paper presents a global optimization approach to solving linear non-quadratic optimal control problems. The main work is to construct a differential flow for finding a global minimizer of the Hamiltonian function... This paper presents a global optimization approach to solving linear non-quadratic optimal control problems. The main work is to construct a differential flow for finding a global minimizer of the Hamiltonian function over a Euclid space. With the Pontryagin principle, the optimal control is characterized by a function of the adjoint variable and is obtained by solving a Hamiltonian differential boundary value problem. For computing an optimal control, an algorithm for numerical practice is given with the description of an example. 展开更多
关键词 Linear Non-Quadratic Optimal control Pontryagin Principle Global Optimization Hamiltonian Differential boundary Value problem
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Adaptive Finite Element Method for Steady Convection-Diffusion Equation
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作者 Gelaw Temesgen Mekuria Jakkula Anand Rao 《American Journal of Computational Mathematics》 2016年第3期275-285,共12页
This paper examines the numerical solution of the convection-diffusion equation in 2-D. The solution of this equation possesses singularities in the form of boundary or interior layers due to non-smooth boundary condi... This paper examines the numerical solution of the convection-diffusion equation in 2-D. The solution of this equation possesses singularities in the form of boundary or interior layers due to non-smooth boundary conditions. To overcome such singularities arising from these critical regions, the adaptive finite element method is employed. This scheme is based on the streamline diffusion method combined with Neumann-type posteriori estimator. The effectiveness of this approach is illustrated by different examples with several numerical experiments. 展开更多
关键词 convection-diffusion problem Streamline Diffusion Finite Element Method boundary and Interior Layers A Posteriori Error Estimators Adaptive Mesh Refinement
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Control strategy of optimal deployment for spacecraft solar array system with initial state uncertainty 被引量:1
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作者 Xinsheng GE Qijia YAO Liqun CHEN 《Applied Mathematics and Mechanics(English Edition)》 SCIE EI CSCD 2018年第10期1437-1452,共16页
A control strategy combining feedforward control and feedback control is presented for the optimal deployment of a spacecraft solar array system with the initial state uncertainty. A dynamic equation of the spacecraft... A control strategy combining feedforward control and feedback control is presented for the optimal deployment of a spacecraft solar array system with the initial state uncertainty. A dynamic equation of the spacecraft solar array system is established under the assumption that the initial linear momentum and angular momentum of the system are zero. In the design of feedforward control, the dissipation energy of each revolute joint is selected as the performance index of the system. A Legendre pseudospectral method(LPM) is used to transform the optimal control problem into a nonlinear programming problem. Then, a sequential quadratic programming algorithm is used to solve the nonlinear programming problem and offline generate the optimal reference trajectory of the system. In the design of feedback control, the dynamic equation is linearized along the reference trajectory in the presence of initial state errors. A trajectory tracking problem is converted to a two-point boundary value problem based on Pontryagin’s minimum principle. The LPM is used to discretize the two-point boundary value problem and transform it into a set of linear algebraic equations which can be easily calculated. Then, the closed-loop state feedback control law is designed based on the resulting optimal feedback control and achieves good performance in real time. Numerical simulations demonstrate the feasibility and effectiveness of the proposed control strategy. 展开更多
关键词 optimal control trajectory tracking spacecraft solar array system twopoint boundary value problem Legendre pseudospectral method(LPM)
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A posteriori error estimates for optimal control problems constrained by convection-diffusion equations
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作者 Hongfei FU Hongxing RUI Zhaojie ZHOU 《Frontiers of Mathematics in China》 SCIE CSCD 2016年第1期55-75,共21页
We propose a characteristic finite element evolutionary type convection-diffusion optimal control discretization of problems. Non- divergence-free velocity fields and bilateral inequality control constraints are handl... We propose a characteristic finite element evolutionary type convection-diffusion optimal control discretization of problems. Non- divergence-free velocity fields and bilateral inequality control constraints are handled. Then some residual type a posteriori error estimates are analyzed for the approximations of the control, the state, and the adjoint state. Based on the derived error estimators, we use them as error indicators in developing efficient multi-set adaptive meshes characteristic finite element algorithm for such optimal control problems. Finally, one numerical example is given to check the feasibility and validity of multi-set adaptive meshes refinements. 展开更多
关键词 Optimal control problem characteristic finite element convection-diffusion equation multi-set adaptive meshes a posterior error estimate
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Inverse Problem of a Tumor Model
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作者 魏英超 陶有山 郭谦 《Journal of Donghua University(English Edition)》 EI CAS 2010年第5期649-655,共7页
This paper considers a model for the growth of a solid tumor with a single anticancer agent application.The model is a free boundary problem of a nonlinear reaction-diffusion-advection equation,where the free boundary... This paper considers a model for the growth of a solid tumor with a single anticancer agent application.The model is a free boundary problem of a nonlinear reaction-diffusion-advection equation,where the free boundary is the surface of the tumor.Since multicellular spheroids are routinely used as in vitro(i.e.,outside live organisms)models of cancer growth and they can be observed and controlled in the laboratory,the following inverse problem is studied:given observed dynamics of tumor growth,a certain parameter is determined.The Lipschitz stability of solutions to the above-mentioned inverse problem is established,and this inverse problem is solved by control theory.Numerical methods for solving the inverse problem are also given. 展开更多
关键词 TUMORS free boundary problem inverse problem STABILITY control theory
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The Bezier Control Points Method for Solving Delay Differential Equation
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作者 Fateme Ghomanjani Mohammad Hadi Farahi 《Intelligent Control and Automation》 2012年第2期188-196,共9页
In this paper, Bezier surface form is used to find the approximate solution of delay differential equations (DDE’s). By using a recurrence relation and the traditional least square minimization method, the best contr... In this paper, Bezier surface form is used to find the approximate solution of delay differential equations (DDE’s). By using a recurrence relation and the traditional least square minimization method, the best control points of residual function can be found where those control points determine the approximate solution of DDE. Some examples are given to show efficiency of the proposed method. 展开更多
关键词 BEZIER control POINTS Delay Differential Equation RESIDUAL Function boundary Value problem Proportional DELAYS
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A POSTERIORI ERROR ESTIMATE FOR BOUNDARY CONTROL PROBLEMS GOVERNED BY THE PARABOLIC PARTIAL DIFFERENTIAL EQUATIONS 被引量:3
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作者 Wei Gong Ningning Yan 《Journal of Computational Mathematics》 SCIE CSCD 2009年第1期68-88,共21页
In this paper, we discuss the a posteriori error estimate of the finite element approximation for the boundary control problems governed by the parabolic partial differential equations. Three different a posteriori er... In this paper, we discuss the a posteriori error estimate of the finite element approximation for the boundary control problems governed by the parabolic partial differential equations. Three different a posteriori error estimators are provided for the parabolic boundary control problems with the observations of the distributed state, the boundary state and the final state. It is proven that these estimators are reliable bounds of the finite element approximation errors, which can be used as the indicators of the mesh refinement in adaptive finite element methods. 展开更多
关键词 boundary control problems Finite element method A posteriori error estimate Parabolic partial differential equations.
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A new class of generalized quasi-variational inequalities with applications to Oseen problems under nonsmooth boundary conditions
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作者 Shengda Zeng Akhtar A.Khan Stanislaw Migórski 《Science China Mathematics》 SCIE CSCD 2024年第2期315-338,共24页
In this paper, we study a generalized quasi-variational inequality (GQVI for short) with twomultivalued operators and two bifunctions in a Banach space setting. A coupling of the Tychonov fixedpoint principle and the ... In this paper, we study a generalized quasi-variational inequality (GQVI for short) with twomultivalued operators and two bifunctions in a Banach space setting. A coupling of the Tychonov fixedpoint principle and the Katutani-Ky Fan theorem for multivalued maps is employed to prove a new existencetheorem for the GQVI. We also study a nonlinear optimal control problem driven by the GQVI and givesufficient conditions ensuring the existence of an optimal control. Finally, we illustrate the applicability of thetheoretical results in the study of a complicated Oseen problem for non-Newtonian fluids with a nonmonotone andmultivalued slip boundary condition (i.e., a generalized friction constitutive law), a generalized leak boundarycondition, a unilateral contact condition of Signorini’s type and an implicit obstacle effect, in which themultivalued slip boundary condition is described by the generalized Clarke subgradient, and the leak boundarycondition is formulated by the convex subdifferential operator for a convex superpotential. 展开更多
关键词 generalized quasi-variational inequality existence theorem optimal control Kakutani-Ky Fan theorem Oseen problem non-Newtonian fluid nonmonotone slip boundary condition
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CONTROLLABILITY OF QUASI-LINEAR IMPULSIVE FUNCTIONAL BOUNDARY VALUE PROBLEMS 被引量:1
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作者 Shujie Yang Bao Shi +1 位作者 Xiaolei Liu Wenfei Zhao 《Annals of Applied Mathematics》 2017年第1期90-101,共12页
By employing the Schauder fixed-point theorem, we establish new suffi- cient conditions for the controllability of impulsive functional boundary value problems.
关键词 controlLABILITY boundary value problems (BVPs) fixed points
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螺旋桨升力面设计边界条件的处理分析 被引量:4
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作者 辛公正 唐登海 董世汤 《船舶力学》 EI 2004年第2期16-24,共9页
本文对螺旋桨升力面设计方法中边界条件的处理问题进行了分析。通过对边界条件的不同处理方法进行实例计算,根据计算结果的比较来分析边界条件的不同简化方法对设计计算结果的影响。从而得出螺旋桨升力面设计所采用的合理边界条件处理... 本文对螺旋桨升力面设计方法中边界条件的处理问题进行了分析。通过对边界条件的不同处理方法进行实例计算,根据计算结果的比较来分析边界条件的不同简化方法对设计计算结果的影响。从而得出螺旋桨升力面设计所采用的合理边界条件处理方法。 展开更多
关键词 船舶动力学 螺旋桨 升力面设计 边界条件 精细化处理 桨叶厚度 涡格
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求解最优控制问题的混合变量变分方法及其航天控制应用 被引量:8
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作者 彭海军 高强 +1 位作者 吴志刚 钟万勰 《自动化学报》 EI CSCD 北大核心 2011年第10期1248-1255,共8页
针对非线性最优控制导出的Hamiltonian系统两点边值问题,提出一种以离散区段右端状态和左端协态为混合独立变量的数值求解方法,将非线性Hamiltonian系统两点边值问题的求解通过混合独立变量变分原理转化为非线性方程组求解.所提出的算... 针对非线性最优控制导出的Hamiltonian系统两点边值问题,提出一种以离散区段右端状态和左端协态为混合独立变量的数值求解方法,将非线性Hamiltonian系统两点边值问题的求解通过混合独立变量变分原理转化为非线性方程组求解.所提出的算法综合了求解最优控制的"直接法"和"间接法"的特征,既满足最优控制理论的一阶必要条件,又不需要对协态初值的准确猜测,避免了求解大规模非线性规划问题.通过两个航天控制算例讨论了本文算法的精度和效率等问题.与近年来在航空航天控制中备受关注的高斯伪谱方法相比较,本文算法无论是在精度还是效率上都具有明显的优势. 展开更多
关键词 非线性最优控制 两点边值 对偶变量 变分原理 HAMILTONIAN系统
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高超声速飞行器上升段最优制导间接法研究 被引量:22
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作者 李惠峰 李昭莹 《宇航学报》 EI CAS CSCD 北大核心 2011年第2期297-302,共6页
高超声速飞行器的机身-推进一体化设计使得气动和推进之间存在强非线性耦合,本文针对高超声速飞行器的特点,提出了求解最优上升轨迹的一种可行方案。在零侧滑角和力矩瞬间平衡假设下对上升段飞行问题进行最优建模,将质量引入为状态量,... 高超声速飞行器的机身-推进一体化设计使得气动和推进之间存在强非线性耦合,本文针对高超声速飞行器的特点,提出了求解最优上升轨迹的一种可行方案。在零侧滑角和力矩瞬间平衡假设下对上升段飞行问题进行最优建模,将质量引入为状态量,以最省燃料为指标,以推力方向为最优控制量,根据极大值原理推导一阶最优条件。为数值求解两点边值问题,以解析解作为初始猜想,应用经典的有限差分方法和改进的牛顿法,在满足攻角过程约束下,通过同伦算法迭代求解最优轨迹。仿真在给定的初始约束和终端约束下进行,结果表明该制导算法能够实现对高超声速飞行器上升轨迹的优化,以参考面积为同伦参数的迭代方法,能够保证算法的收敛性和快速性。 展开更多
关键词 高超声速飞行器 最优控制 两点边值问题 上升段制导 轨迹优化
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基于交会概念的最省燃料共面有限推力轨道转移方法 被引量:5
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作者 荆武兴 吴瑶华 杨涤 《哈尔滨工业大学学报》 EI CAS CSCD 北大核心 1997年第4期132-135,25,共5页
基于交会概念研究了卫星在平面内的最省燃料有限推力轨道转移问题。假设有一个飞行器已经在目标轨道上运动,此飞行器称为虚拟卫星。发动机推力大小为常值,方向可调。提供了适合于同平面轨道转移的卫星相对运动动力学模型,用Pontryagin... 基于交会概念研究了卫星在平面内的最省燃料有限推力轨道转移问题。假设有一个飞行器已经在目标轨道上运动,此飞行器称为虚拟卫星。发动机推力大小为常值,方向可调。提供了适合于同平面轨道转移的卫星相对运动动力学模型,用Pontryagin极大值原理导出了最省燃料的推力控制策略,建立了状态和共轭状态的初始边界条件。给出了两点边值问题的迭代变量与迭代算法。仿真例子考虑卫星由低圆轨道向同平面高圆轨道的小推力过渡,仿真结果验证了所提供方法的有效性。 展开更多
关键词 轨道转移 交会 最优控制 有限推力 卫星
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基于交会概念的最省燃料异面有限推力轨道转移研究 被引量:9
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作者 荆武兴 吴瑶华 《哈尔滨工业大学学报》 EI CAS CSCD 北大核心 1998年第2期124-128,共5页
基于交会概念研究了卫星在三维空间的最省燃料有限推力轨道转移问题。假设有一个飞行器已经在目标轨道上运动,此飞行器称为虚拟卫星。只要控制真实卫星与虚拟卫星软交会,就实现*了真实卫星向目标轨道的转移。假定发动机推力大小为... 基于交会概念研究了卫星在三维空间的最省燃料有限推力轨道转移问题。假设有一个飞行器已经在目标轨道上运动,此飞行器称为虚拟卫星。只要控制真实卫星与虚拟卫星软交会,就实现*了真实卫星向目标轨道的转移。假定发动机推力大小为常值,方向可调。提供了真实卫星的相对运*动动力学模型,用Pontryagin极大值原理导出了最省燃料的推力控制策略,建立了状态和共轭状态的初始边界条件。导出的两点边值问题由牛顿代方法求解。仿真结果验证了所提供方法的有效性。 展开更多
关键词 轨道转移 交会 最优控制 有限元推力 飞行器
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基于转换模板的三维实体全六面体网格生成方法 被引量:10
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作者 关振群 单菊林 顾元宪 《计算力学学报》 EI CAS CSCD 北大核心 2005年第1期32-37,共6页
以四面体-六面体基本转换模板为基础,提出一系列具有伸缩性的扩展转换模板,可根据需要选择不同模板及其组合,将四面体分解为不同数量、不同密度过渡形式的六面体单元。这样,初始四面体网格不需要划分得很细,生成的六面体单元数量也可以... 以四面体-六面体基本转换模板为基础,提出一系列具有伸缩性的扩展转换模板,可根据需要选择不同模板及其组合,将四面体分解为不同数量、不同密度过渡形式的六面体单元。这样,初始四面体网格不需要划分得很细,生成的六面体单元数量也可以通过采用不同规格的扩展转换模板而得到控制。提出了基于CAD几何造型的边界节点坐标修正方法,从而使边界网格更好地拟合几何模型边界。 展开更多
关键词 有限元 网格生成 六面体 模板法
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AOTV的极小时间控制 被引量:4
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作者 荆武兴 杨涤 吴瑶华 《宇航学报》 EI CAS CSCD 北大核心 1992年第4期9-16,共8页
本文研究了在共面圆轨道HEO-LEO的过程中,气动辅助轨道转移飞行器(AOTV)在大气内飞行的极小时间控制问题。应用Pontriagin极大值原理导出了AOTV在大气内飞行的极小时间控制规律。以AOTV从地球同步轨道向同平面500公里高度圆轨道过渡为例... 本文研究了在共面圆轨道HEO-LEO的过程中,气动辅助轨道转移飞行器(AOTV)在大气内飞行的极小时间控制问题。应用Pontriagin极大值原理导出了AOTV在大气内飞行的极小时间控制规律。以AOTV从地球同步轨道向同平面500公里高度圆轨道过渡为例,大气密度采用US.62标准大气密度,仿真结果表明,按照极小时间控制规律,AOTV一次经过大气层进入LEO需要的特征速度增量仅为纯推力Hohmann转移所需特征速度增量的43.8%,大气内飞行的时间约20分钟。 展开更多
关键词 轨道转移 系统控制 边值问题
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