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Unified numerical predictor-corrector guidance based on characteristic model
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作者 MENG Bin ZHANG Hangning ZHAO Yunbo 《中国空间科学技术(中英文)》 CSCD 北大核心 2024年第4期40-49,共10页
Aerocapture is one of the key technologies for low-cost transportation,with high demands of autonomy,accuracy,and robustness of guidance and control,due to its high reliability requirements for only one chance of tryi... Aerocapture is one of the key technologies for low-cost transportation,with high demands of autonomy,accuracy,and robustness of guidance and control,due to its high reliability requirements for only one chance of trying.A unified numerical predictor-corrector guidance method based on characteristic models for aerocapture is proposed.The numerical predictor-corrector guidance method is used to achieve autonomy and high accuracy,and the characteristic model control method is introduced to achieve robustness.At the same time,by transforming path constraints,characteristic model equations including apogee deviation and altitude differentiation are established.Based on the characteristic model equations,a unified guidance law which can satisfy path constraints and guidance objectives simultaneously is designed.In guidance problems,guidance deviation is not directly obtained from the output of the dynamics at present,but is calculated through integral and algebraic equations.Therefore,the method of directly discretizing differential equations cannot be used to establish characteristic models,which brings great difficulty to characteristic modeling.A method for characteristic modeling of guidance problems is proposed,and convergence analysis of the proposed guidance law is also provided.Finally,a joint numerical simulation of guidance and control considering navigation deviation and various uncertainties is conducted to verify the effectiveness of the proposed method.The proposed unified method can be extended to general aerodynamic entry guidance designs,providing theoretical and methodological support for them. 展开更多
关键词 aerocapture path constraint characteristic model unified numerical predictor-corrector guidance CONVERGENCE
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Fast and Accurate Predictor-Corrector Methods Using Feedback-Accelerated Picard Iteration for Strongly Nonlinear Problems
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作者 Xuechuan Wang Wei He +1 位作者 Haoyang Feng Satya N.Atluri 《Computer Modeling in Engineering & Sciences》 SCIE EI 2024年第5期1263-1294,共32页
Although predictor-corrector methods have been extensively applied,they might not meet the requirements of practical applications and engineering tasks,particularly when high accuracy and efficiency are necessary.A no... Although predictor-corrector methods have been extensively applied,they might not meet the requirements of practical applications and engineering tasks,particularly when high accuracy and efficiency are necessary.A novel class of correctors based on feedback-accelerated Picard iteration(FAPI)is proposed to further enhance computational performance.With optimal feedback terms that do not require inversion of matrices,significantly faster convergence speed and higher numerical accuracy are achieved by these correctors compared with their counterparts;however,the computational complexities are comparably low.These advantages enable nonlinear engineering problems to be solved quickly and accurately,even with rough initial guesses from elementary predictors.The proposed method offers flexibility,enabling the use of the generated correctors for either bulk processing of collocation nodes in a domain or successive corrections of a single node in a finite difference approach.In our method,the functional formulas of FAPI are discretized into numerical forms using the collocation approach.These collocated iteration formulas can directly solve nonlinear problems,but they may require significant computational resources because of the manipulation of high-dimensionalmatrices.To address this,the collocated iteration formulas are further converted into finite difference forms,enabling the design of lightweight predictor-corrector algorithms for real-time computation.The generality of the proposed method is illustrated by deriving new correctors for three commonly employed finite-difference approaches:the modified Euler approach,the Adams-Bashforth-Moulton approach,and the implicit Runge-Kutta approach.Subsequently,the updated approaches are tested in solving strongly nonlinear problems,including the Matthieu equation,the Duffing equation,and the low-earth-orbit tracking problem.The numerical findings confirm the computational accuracy and efficiency of the derived predictor-corrector algorithms. 展开更多
关键词 predictor-corrector method feedback-accelerated Picard iteration nonlinear dynamical system real-time computation
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A Full Predictor-Corrector Finite Element Method for the One-Dimensional Heat Equation with Time-Dependent Singularities
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作者 Jake L. Nkeck 《Journal of Applied Mathematics and Physics》 2024年第4期1364-1382,共19页
The energy norm convergence rate of the finite element solution of the heat equation is reduced by the time-regularity of the exact solution. This paper presents an adaptive finite element treatment of time-dependent ... The energy norm convergence rate of the finite element solution of the heat equation is reduced by the time-regularity of the exact solution. This paper presents an adaptive finite element treatment of time-dependent singularities on the one-dimensional heat equation. The method is based on a Fourier decomposition of the solution and an extraction formula of the coefficients of the singularities coupled with a predictor-corrector algorithm. The method recovers the optimal convergence rate of the finite element method on a quasi-uniform mesh refinement. Numerical results are carried out to show the efficiency of the method. 展开更多
关键词 SINGULARITIES Finite Element Methods Heat Equation predictor-corrector Algorithm
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基于预估-校正算法的分数阶Boost变换器倍周期分岔研究
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作者 谢玲玲 杨雨晴 +1 位作者 姚浚义 秦龙 《电源学报》 CSCD 北大核心 2024年第2期10-18,共9页
基于电感电容本质是分数阶的事实,对分数阶Boost变换器的非线性动力学特性进行了深入研究。采用分数阶微积分的预估-校正算法,建立了Boost变换器的预估-校正模型,在此基础上得到了以参考电流、输入电压以及电容电感阶数为分岔参数的分岔... 基于电感电容本质是分数阶的事实,对分数阶Boost变换器的非线性动力学特性进行了深入研究。采用分数阶微积分的预估-校正算法,建立了Boost变换器的预估-校正模型,在此基础上得到了以参考电流、输入电压以及电容电感阶数为分岔参数的分岔图,研究了变换器的倍周期分岔和混沌行为,同时与整数阶Boost变换器的非线性动力学行为进行了比较。研究结果表明,在一定的工作条件下,随着变换器某些电路参数的变化,分数阶Boost变换器会出现分岔和混沌等非线性现象;在相同电路参数的条件下,整数阶和分数阶变换器的稳定参数域之间存在差异,与整数阶变换器相比,分数阶变换器的参数稳定区域更小,更真实地反映了Boost变换器的非线性动力学特性。 展开更多
关键词 分数阶 BOOST变换器 混沌 预估-校正算法 倍周期分岔
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基于自适应横程走廊的再入滑翔飞行器改进预测校正算法 被引量:1
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作者 贺杨超 李炯 +2 位作者 邵雷 周池军 雷虎民 《系统工程与电子技术》 EI CSCD 北大核心 2024年第2期692-702,共11页
针对再入滑翔飞行器(reentry gliding vehicle,RGV)预测校正制导算法中规避逻辑和制导逻辑相分离的问题,提出了一种基于自适应横程走廊的融合算法。首先,通过飞行器侧向运动轨迹与禁飞区的相交关系,动态引入规避逻辑;同时,提出禁飞区有... 针对再入滑翔飞行器(reentry gliding vehicle,RGV)预测校正制导算法中规避逻辑和制导逻辑相分离的问题,提出了一种基于自适应横程走廊的融合算法。首先,通过飞行器侧向运动轨迹与禁飞区的相交关系,动态引入规避逻辑;同时,提出禁飞区有效映射横程来量化影响飞行轨迹的禁飞区区域;最后,设计自适应横程走廊,动态调整走廊边界,控制倾侧角的翻转,实现规避逻辑和侧向制导逻辑的融合。仿真结果表明,在本文方法下,飞行器可以针对不同情况的禁飞区实现有效制导,对再入扰动具有一定的鲁棒性,并与制导逻辑和规避逻辑分离设计的算法相比,在保证制导精度的同时,具备更少的倾侧角翻转次数。 展开更多
关键词 预测校正算法 自适应横程走廊 禁飞区有效映射横程
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基于改进预测校正的时间协同再入制导方法 被引量:1
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作者 高源 胡钰 +2 位作者 陈锦涌 张杰 周锐 《北京航空航天大学学报》 EI CAS CSCD 北大核心 2024年第5期1721-1730,共10页
针对高超声速飞行器再入滑翔过程的时间协同问题,提出一种基于开环式协同结构的时间协同预测校正制导律。所提制导律不依赖于各飞行器之间的实时通信,通过预先设置期望飞行时间进行协同信息共享。纵向制导律在传统预测校正的基础上进行... 针对高超声速飞行器再入滑翔过程的时间协同问题,提出一种基于开环式协同结构的时间协同预测校正制导律。所提制导律不依赖于各飞行器之间的实时通信,通过预先设置期望飞行时间进行协同信息共享。纵向制导律在传统预测校正的基础上进行改进,引入归一化加权误差,同时考虑剩余航程误差与剩余飞行时间误差,采用全弹道积分预测剩余航程和剩余飞行时间,每个制导周期通过牛顿迭代法求解倾侧角幅值,完成兼顾时间协同和空间精度的纵向制导过程。仿真实例表明:通过选择合适的加权误差系数,所提制导律可实现对再入飞行时间的有效调节,导引多飞行器在期望飞行时间到达指定再入交班点。蒙特卡罗仿真验证了所提制导律的鲁棒性。 展开更多
关键词 高超声速飞行器 再入制导 预测校正 时间协同 归一化加权误差
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适应多射程与路径约束的再入预测校正制导
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作者 郭浩辰 黄汉斌 +1 位作者 郭涛 杨业 《导弹与航天运载技术(中英文)》 CSCD 北大核心 2024年第5期48-55,共8页
针对存在不同分布的路径约束与不同航程需求的升力式飞行器再入飞行任务,设计二次曲线形式的倾侧角剖面以增强飞行器的侧向机动能力,通过预测校正的迭代过程修正倾侧角剖面以满足航程需求,采用改进人工势场法设计侧向制导方法导引飞行... 针对存在不同分布的路径约束与不同航程需求的升力式飞行器再入飞行任务,设计二次曲线形式的倾侧角剖面以增强飞行器的侧向机动能力,通过预测校正的迭代过程修正倾侧角剖面以满足航程需求,采用改进人工势场法设计侧向制导方法导引飞行器满足路径约束,最后通过粒子群算法优化制导参数以获得性能最优的轨迹。仿真结果验证了该算法能够适应多种航程需求与路径约束且以较高精度满足终端约束。 展开更多
关键词 升力式飞行器 路径约束 预测校正制导 人工势场 粒子群优化
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一类非线性Burgers型问题的预测校正紧差分方法 被引量:1
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作者 王佳威 张海湘 杨雪花 《湖南工业大学学报》 2024年第1期98-104,共7页
针对一类非线性Burgers型方程,提出一种预测-校正紧差分方法。首先,对时间一阶导数采用一阶Euler格式,时间积分项运用一阶卷积求积公式进行离散,并以MacCormack方法的两步预测-校正方法处理非线性项;然后采用四阶紧差分离散空间的一阶... 针对一类非线性Burgers型方程,提出一种预测-校正紧差分方法。首先,对时间一阶导数采用一阶Euler格式,时间积分项运用一阶卷积求积公式进行离散,并以MacCormack方法的两步预测-校正方法处理非线性项;然后采用四阶紧差分离散空间的一阶和二阶导数,构造了Euler预测-校正紧差分全离散格式。最后通过案例验证了所提出算法的有效性。 展开更多
关键词 计算数学 非线性Burgers方程 预测-校正算法 紧差分方法
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高超声速飞行器时间协同预测校正鲁棒制导
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作者 魏昀鹏 都延丽 +1 位作者 王文凯 刘燕斌 《宇航学报》 EI CAS CSCD 北大核心 2024年第3期421-432,共12页
针对存在参数不确定性的多高超声速飞行器滑翔段协同制导问题,提出了一种时间协同的预测校正鲁棒制导方法。首先,基于剩余飞行时间的动态航向角误差走廊实现了横向协同制导,为调整飞行时间提供了有利条件;设计了随协同飞行任务进程变化... 针对存在参数不确定性的多高超声速飞行器滑翔段协同制导问题,提出了一种时间协同的预测校正鲁棒制导方法。首先,基于剩余飞行时间的动态航向角误差走廊实现了横向协同制导,为调整飞行时间提供了有利条件;设计了随协同飞行任务进程变化的权值函数,将剩余飞行时间引入纵向制导的预测校正过程中,确保协同飞行任务落点和协同时间的精度。其次,基于改进无迹卡尔曼滤波估计的方法对气动参数的不确定性进行估计,通过对剩余飞行时间与剩余能量的综合分析,修正了航向角误差走廊和标称迎角剖面,以提高协同制导系统的鲁棒性能。最后,分别在标称环境和参数不确定环境下开展了仿真实验,其结果证明了该协同制导方法的可行性和鲁棒性。 展开更多
关键词 高超声速飞行器 预测校正 时间协同制导 鲁棒制导 无迹卡尔曼滤波
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基于DDPG的高速飞行器预测校正制导律设计
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作者 王晓威 殷玮 +2 位作者 杨亚 沈昱恒 颜涛 《航天控制》 CSCD 2024年第2期22-28,共7页
针对高速飞行器在再入滑翔过程中的多约束、强时变问题,本文结合深度确定性策略梯度算法(Deep Deterministic Policy Gradient, DDPG)的在线自主决策优势,根据威胁区信息,实时生成规避策略来进行动态禁飞区规避航迹规划。进一步为增强... 针对高速飞行器在再入滑翔过程中的多约束、强时变问题,本文结合深度确定性策略梯度算法(Deep Deterministic Policy Gradient, DDPG)的在线自主决策优势,根据威胁区信息,实时生成规避策略来进行动态禁飞区规避航迹规划。进一步为增强高速飞行器对环境不确定因素的抗干扰能力,在规避轨迹基础上选取航路特征点集合,采用预测校正在线制导方式,根据飞行任务需求和终端约束,实时校正高速飞行器飞行状态,最终实现高速飞行器精确制导。同时,为验证方法的有效性,开展了相应的数值仿真分析。结果表明,本文方法能够有效规避禁飞区,增强了对不确定因素的适应性,具有一定的工程应用价值。 展开更多
关键词 高速飞行器 禁飞区 DDPG算法 预测校正制导
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空间运动方程快速求解器设计与实现
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作者 王晓蕾 黄章骞 +1 位作者 房旭 宋宇鲲 《合肥工业大学学报(自然科学版)》 CAS 北大核心 2024年第1期54-61,共8页
文章基于四阶经典龙格库塔法(classical Runge-Kutta method of order four,RK-4)和四阶Adams预测校正法(fourth-order Adams predictor-corrector method,Adams-4),提出一种现场可编程逻辑门阵列(field programmable gate array,FPGA)... 文章基于四阶经典龙格库塔法(classical Runge-Kutta method of order four,RK-4)和四阶Adams预测校正法(fourth-order Adams predictor-corrector method,Adams-4),提出一种现场可编程逻辑门阵列(field programmable gate array,FPGA)实现的数据路径可动态配置的空间运动方程快速求解器(space motion equation fast solver,SMEFS)。SMEFS采用折叠式结构,借助高效的任务映射和精准的状态管理,通过资源复用和动态配置运算器内部连接关系实现数据路径的动态配置,快速求解空间运动方程,并有效节省硬件资源。采用某型运载火箭的相关数据对SMEFS进行大批量空间运动方程求解的性能评估,实验结果表明SMEFS能够快速可靠地求解发射坐标系下的五自由度空间运动方程,与软件求解的平均加速比为12.765,求解结果最大相对误差小于9×10^(-5,)具备较好的加速效果和较高的计算可靠性。 展开更多
关键词 四阶经典龙格库塔法(RK-4) 四阶Adams预测校正法(Adams-4) 空间运动方程 折叠技术 现场可编程逻辑门阵列(FPGA)
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摩擦对平行圆盘间隙中一维可压缩流动的影响分析
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作者 郭良斌 李玉立 《机床与液压》 北大核心 2024年第9期81-86,共6页
以平行圆盘间隙中一维可压缩理想流动分析结果为基础,在考虑平行圆盘间隙内面积变化和壁面摩擦时,通过理论推导及程序编制,利用预估-校正方法得到了平行气膜区气膜对称线上一维模型的马赫数及摩擦因数的分布规律。结果表明:对于一维模... 以平行圆盘间隙中一维可压缩理想流动分析结果为基础,在考虑平行圆盘间隙内面积变化和壁面摩擦时,通过理论推导及程序编制,利用预估-校正方法得到了平行气膜区气膜对称线上一维模型的马赫数及摩擦因数的分布规律。结果表明:对于一维模型而言,气膜对称线上的马赫数始终呈现下降的趋势,摩擦因数始终呈现上升的趋势,但摩擦因数在整个平行圆盘间隙中变化很小;对于不同材料的轴承圆盘,由于精加工工艺的不同会导致壁面相对粗糙度发生变化,进而使壁面摩擦因数发生显著变化,即摩擦因数受到相对粗糙度的影响很大;在计算过程中采用平均摩擦因数可得到相似的计算结果,并满足计算精度要求。 展开更多
关键词 高压圆盘气体轴承 一维绝热定常流动 预估-校正法 马赫数 摩擦因数
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A Predictor-Corrector Scheme for the Microscopic Depletion Solver of the COCAGNE Core Code
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作者 Fabrice Hoareau Nadine Schwartz David Couyras 《Journal of Energy and Power Engineering》 2012年第3期369-378,共10页
EDF R&D is developing a new calculation scheme based on the transport-Simplified Pn (SPn) approach. The lattice code used is the deterministic code APOLLO2, developed at CEA. The core code is the code COCAGNE, deve... EDF R&D is developing a new calculation scheme based on the transport-Simplified Pn (SPn) approach. The lattice code used is the deterministic code APOLLO2, developed at CEA. The core code is the code COCAGNE, developed at EDF R&D. The latter can take advantage of a microscopic depletion solver expected to improve the treatment of spectral history effects. However, the direct use of the microscopic depletion solver is computationally very intensive because very small evolution steps (typically 100 MWd/t) are needed to reach a good accuracy, which is not always compatible with industrial applications. In order to reduce the calculation time associated with the use of the microscopic depletion solver, a predictor-corrector scheme has been implemented within COCAGNE. It enables the use of larger evolution steps, up to 1000 MWd/t. Tests show that the predictor-corrector procedure gives fairly accurate results while significantly reducing the calculation time. 展开更多
关键词 Neutronic simulation microscopic depletion predictor-corrector.
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AN INFEASIBLE-INTERIOR-POINT PREDICTOR-CORRECTOR ALGORITHM FOR THE SECOND-ORDER CONE PROGRAM 被引量:11
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作者 迟晓妮 刘三阳 《Acta Mathematica Scientia》 SCIE CSCD 2008年第3期551-559,共9页
A globally convergent infeasible-interior-point predictor-corrector algorithm is presented for the second-order cone programming (SOCP) by using the Alizadeh- Haeberly-Overton (AHO) search direction. This algorith... A globally convergent infeasible-interior-point predictor-corrector algorithm is presented for the second-order cone programming (SOCP) by using the Alizadeh- Haeberly-Overton (AHO) search direction. This algorithm does not require the feasibility of the initial points and iteration points. Under suitable assumptions, it is shown that the algorithm can find an -approximate solution of an SOCP in at most O(√n ln(ε0/ε)) iterations. The iteration-complexity bound of our algorithm is almost the same as the best known bound of feasible interior point algorithms for the SOCP. 展开更多
关键词 Second-order cone programming infeasible-interior-point algorithm predictor-corrector algorithm global convergence
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A POLYNOMIAL PREDICTOR-CORRECTOR INTERIOR-POINT ALGORITHM FOR CONVEX QUADRATIC PROGRAMMING 被引量:4
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作者 余谦 黄崇超 江燕 《Acta Mathematica Scientia》 SCIE CSCD 2006年第2期265-270,共6页
This article presents a polynomial predictor-corrector interior-point algorithm for convex quadratic programming based on a modified predictor-corrector interior-point algorithm. In this algorithm, there is only one c... This article presents a polynomial predictor-corrector interior-point algorithm for convex quadratic programming based on a modified predictor-corrector interior-point algorithm. In this algorithm, there is only one corrector step after each predictor step, where Step 2 is a predictor step and Step 4 is a corrector step in the algorithm. In the algorithm, the predictor step decreases the dual gap as much as possible in a wider neighborhood of the central path and the corrector step draws iteration points back to a narrower neighborhood and make a reduction for the dual gap. It is shown that the algorithm has O(√nL) iteration complexity which is the best result for convex quadratic programming so far. 展开更多
关键词 Convex quadratic programming predictor-corrector interior-point algorithm
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Numerical simulation of standing wave with 3D predictor-corrector finite difference method for potential flow equations 被引量:3
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作者 罗志强 陈志敏 《Applied Mathematics and Mechanics(English Edition)》 SCIE EI 2013年第8期931-944,共14页
A three-dimensional (3D) predictor-corrector finite difference method for standing wave is developed. It is applied to solve the 3D nonlinear potential flow equa- tions with a free surface. The 3D irregular tank is ... A three-dimensional (3D) predictor-corrector finite difference method for standing wave is developed. It is applied to solve the 3D nonlinear potential flow equa- tions with a free surface. The 3D irregular tank is mapped onto a fixed cubic tank through the proper coordinate transform schemes. The cubic tank is distributed by the staggered meshgrid, and the staggered meshgrid is used to denote the variables of the flow field. The predictor-corrector finite difference method is given to develop the difference equa- tions of the dynamic boundary equation and kinematic boundary equation. Experimental results show that, using the finite difference method of the predictor-corrector scheme, the numerical solutions agree well with the published results. The wave profiles of the standing wave with different amplitudes and wave lengths are studied. The numerical solutions are also analyzed and presented graphically. 展开更多
关键词 three-dimensional (3D) nonlinear potential flow equation predictor-corrector finite difference method staggered grid nested iterative method 3D sloshing
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Two new predictor-corrector algorithms for second-order cone programming 被引量:1
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作者 曾友芳 白延琴 +1 位作者 简金宝 唐春明 《Applied Mathematics and Mechanics(English Edition)》 SCIE EI 2011年第4期521-532,共12页
Based on the ideas of infeasible interior-point methods and predictor-corrector algorithms, two interior-point predictor-corrector algorithms for the second-order cone programming (SOCP) are presented. The two algor... Based on the ideas of infeasible interior-point methods and predictor-corrector algorithms, two interior-point predictor-corrector algorithms for the second-order cone programming (SOCP) are presented. The two algorithms use the Newton direction and the Euler direction as the predictor directions, respectively. The corrector directions belong to the category of the Alizadeh-Haeberly-Overton (AHO) directions. These algorithms are suitable to the cases of feasible and infeasible interior iterative points. A simpler neighborhood of the central path for the SOCP is proposed, which is the pivotal difference from other interior-point predictor-corrector algorithms. Under some assumptions, the algorithms possess the global, linear, and quadratic convergence. The complexity bound O(rln(εo/ε)) is obtained, where r denotes the number of the second-order cones in the SOCP problem. The numerical results show that the proposed algorithms are effective. 展开更多
关键词 second-order cone programming infeasible interior-point algorithm predictor-corrector algorithm global convergence complexity analysis
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An Explicit-Implicit Predictor-Corrector Domain Decomposition Method for Time Dependent Multi-Dimensional Convection Diffusion Equations 被引量:1
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作者 Liyong Zhu Guangwei Yuan Qiang Du 《Numerical Mathematics(Theory,Methods and Applications)》 SCIE 2009年第3期301-325,共25页
The numerical solution of large scale multi-dimensional convection diffusion equations often requires efficient parallel algorithms.In this work,we consider the extension of a recently proposed non-overlapping domain ... The numerical solution of large scale multi-dimensional convection diffusion equations often requires efficient parallel algorithms.In this work,we consider the extension of a recently proposed non-overlapping domain decomposition method for two dimensional time dependent convection diffusion equations with variable coefficients. By combining predictor-corrector technique,modified upwind differences with explicitimplicit coupling,the method under consideration provides intrinsic parallelism while maintaining good stability and accuracy.Moreover,for multi-dimensional problems, the method can be readily implemented on a multi-processor system and does not have the limitation on the choice of subdomains required by some other similar predictor-corrector or stabilized schemes.These properties of the method are demonstrated in this work through both rigorous mathematical analysis and numerical experiments. 展开更多
关键词 Convection diffusion equation parallel algorithm domain decomposition modifiedupwind differences predictor-corrector explicit-implicit scheme convergence analysis.
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New Predictor-Corrector Methods Based on Exponential Time Differencing forSystems of Nonlinear Differential Equations 被引量:1
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作者 TANGChen YANHai-Qing ZHANGHao LIWen-Run LIUMing ZHANGGui-Min 《Communications in Theoretical Physics》 SCIE CAS CSCD 2004年第2期219-224,共6页
We present the new predictor-corrector methods for systems of nonlinear differential equations, based on the method of exponential time differencing. We compare the present schemes with the explicit multistep exponent... We present the new predictor-corrector methods for systems of nonlinear differential equations, based on the method of exponential time differencing. We compare the present schemes with the explicit multistep exponential time differencing and Adams–Bashforth–Moulton method. The numerical results show that the schemes are more accurate and more efficient than Adams predictor-corrector method. The exponential time differencing method has been developed and perfected by the present studies. 展开更多
关键词 predictor-corrector methods of exponential time differencing nonlinear system CHAOS
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Finite Volume Element Predictor-corrector Method for a Class of Nonlinear Parabolic Systems 被引量:1
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作者 高夫征 《Northeastern Mathematical Journal》 CSCD 2005年第3期305-314,共10页
A finite volume element predictor-corrector method for a class of nonlinear parabolic system of equations is presented and analyzed. Suboptimal L^2 error estimate for the finite volume element predictor-corrector meth... A finite volume element predictor-corrector method for a class of nonlinear parabolic system of equations is presented and analyzed. Suboptimal L^2 error estimate for the finite volume element predictor-corrector method is derived. A numerical experiment shows that the numerical results are consistent with theoretical analysis. 展开更多
关键词 predictor-corrector method finite volume element error estimate
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