Parallel Algorithms for Forward and Back Substitution in Direct Solution of Sparse Linear S
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lammps 计算二面角LAMMPS计算二面角引言:在材料科学和化学领域,二面角是描述分子结构的重要参数之一。
它指的是由四个原子组成的面,其中三个原子共面,而第四个原子与这个平面垂直。
LAMMPS(Large-scale Atomic/Molecular Massively Parallel Simulator)是一种分子动力学模拟软件,可以用于计算和模拟材料的结构和性质。
本文将介绍如何使用LAMMPS 计算二面角。
一、LAMMPS简介LAMMPS是一种开源的分子动力学模拟软件,广泛应用于材料科学、化学和生物物理学等领域。
它可以模拟原子和分子在时间和空间上的运动,计算材料的力学性质、热学性质和电学性质等。
其计算精度高,模拟效率也很高,被广泛应用于各种研究领域。
二、二面角的定义二面角是描述分子结构的重要参数之一。
对于四个原子A、B、C和D来说,二面角由向量AB和向量BC的夹角来定义。
当向量AB和向量BC共面时,二面角为0度;当向量AB和向量BC垂直时,二面角为90度。
三、计算二面角的步骤在LAMMPS中,计算二面角可以通过以下步骤实现:1. 定义分子结构:首先,需要定义分子的结构,包括原子的坐标和连接关系。
可以使用LAMMPS提供的输入文件格式,例如atom 文件或data文件。
2. 添加计算命令:在LAMMPS输入文件中,添加计算二面角的命令。
可以使用“dihedral_style”命令来定义二面角的计算方法,常用的方法包括CHARMM、OPLS和AMBER等。
3. 运行计算:运行LAMMPS软件,通过输入文件来进行计算。
LAMMPS将根据输入文件中的命令对分子进行模拟,并计算二面角的数值。
4. 分析结果:根据计算结果,可以得到二面角的数值。
可以使用LAMMPS提供的输出命令将结果输出到文件中,以便后续的分析和可视化。
四、应用案例以蛋白质分子为例,我们可以使用LAMMPS计算蛋白质中的二面角。
首先,需要准备蛋白质的结构文件,可以从PDB数据库中下载蛋白质的原子坐标信息。
§6.5 染色应用举例—求图的边色数及色数的算法一、排课表问题—求二部图的正常)(G χ′边染色1. 问题: 有m 位教师m x x x ,,,21 ,n 个班级n y y y ,,,21 。
教师x i 每周需要给班级y j 上p ij 次(节)课。
要求制订一张周课时尽可能少的课程表。
2. 图论模型:构造二部图),(Y X G =,其中X ={m x x x ,,,21 },Y ={n y y y ,,,21 },顶点i x 与j y 之间连ij p 条边。
一个课时的安排方案对应于二部图G 的一个匹配。
排课表问题等价于:将E (G )划分成一些匹配,使得匹配的数目尽可能地少。
按)(G χ′的定义,这个最小的数目便是)(G χ′。
由定理6.2.1,()()G G χ′=Δ。
因此,排课表问题等价于:求二部图G 的边正常)(G Δ染色。
如§6.1中所述,虽然求简单图的正常(1+Δ)边染色存在多项式时间算法,但求简单图G 的边色数)(G χ′及其相应的正常边染色是一个NPC 问题[28]。
尽管如此,求二部图的边正常Δ染色却有多项式时间算法。
求图的边色数的近似算法可参考文献[29]~[51]。
[28] I. Holyer, The NP-completeness of edge-coloring, SIAM J. Computing , 10: 4(1981), 718-720.[29] E. Petrank, The hardness of approximation: gap location, Computational Complexity , 4 (1994), 133-157.[30] D. Leven and Z. Galil, NP completeness of finding the chromatic index of regular graphs, J. Algorithms , 4(1983) 35-44.[31] P. Crescenzi, V . Kann, R. Silvestri, and L. Trevisan, Structure in approximation classes, SIAM J. Comp., 28 (1999), 1759-1782.[32] J. Misra and D. Gries, A constructive proof of Vizing's theorem. Inform. Process. Lett. 41 (1992), 131-133.[33] O. Terada, and T. Nishizeki, Approximate algorithms for the edge-coloring of graphs, Trans. Inst. Eletron. Commun. Engr. Japan J65-D , 11(1982), 1382-1389.[34] M. Chrobak, and T. Nishizeki, Improved edge-coloring algorithms for planar graphs, J. Algorithms , 11(1990), 102-116.[35] I. Caragiannis, A. Ferreira, C. Kaklamanis, S. Perennes, P. Persiano and H. Rivano, Approximate constrained bipartite edge coloring, Discrete Applied Mathematics , 143(2004), 54-61[36] M. R. Salavatipour, A polynomial time algorithm for strong edge coloring of partial k -trees, Discrete Applied Mathematics , 143(2004), 285-291.[37] D.A. Grable, A. Panconesi, Nearly optimal distributed edge coloring in O (log log n ) rounds, Proceedings of the Eighth Annual ACM-SIAM Symposium on Discrete Algorithms, January, (1997), 278–285.[38] Yijie Han, Weifa Liang and Xiaojun Shen, Very fast parallel algorithms for approximate edge coloring, Discrete Applied Mathematics, 108(2001), 227-238.[39] M. Fürer and B. Raghavachari, Parallel edge coloring approximation, Parallel Process. Lett. , 6 (1996), 321–329.[40] H.J. Karloff and D.B. Shmoys, Efficient parallel algorithms for edge coloring problems. J. Algorithms 8 (1987), 39–52.[41] W. Liang, Fast parallel algorithms for the approximate edge-coloring problem. Inform. Process. Lett. 56 (1995), 333–338.[42] W. Liang, X. Shen and Q. Hu, Parallel algorithms for the edge-coloring and edge-coloring update problems. J. Parallel Distrib. Comput. 32 (1996), 66-73.[43] R. Motwani, J. Naor and M. Naor, The probabilistic method yields deterministic parallel algorithms. J. Comput. System Sci. 49 (1994), 478-516.[44] D. Bertsimas, C-P. Teo, and R. V ohra, On dependent randomized rounding algorithms, Proc. 5th Int. Conf. on Integer Prog. and Combinatorial Optimization , Lecture Notes in Comput. Sci. 1084, Springer-Verlag, (1996), 330-344.[45] M.K. Goldberg, Edge-colorings of multigraphs: recoloring technique, J. Graph Theory , 8(1984), 123-127.[46] D.S. Hochbaum, T. Nishizeki and D.B. Shmoys, Better than “Best Possible” algorithm to edge color multi graphs, Journal of Algorithms , 7(1986), 79-104[47] T. Nishizeki and K. Kashiwagi, On the 1.1 edge-coloring of multigraphs, SIAM J. Disc. Math. , 3(1990), 391-410.[48] J. Kahn, Asymptotics of the chromatic index for multigraphs, Journal of Combinatorial Theory (Ser. B ), 68(1996), 233-254.[49] X. Zhou H. Susuki, and T. Nishizeki, A linear algorithm for edge-coloring series-parallel multigraphs, J. Algorithms , 20(1996), 174-201.[50] X. Zhou H. Susuki, and T. Nishizeki, An NC parallel algorithm for edge-coloring series-parallel multigraphs, J. Algorithms , 23(1997), 359-374.[51] B. Berger and J. Rompel, Simulating (log c n )-wise independence in NC. J. ACM 38 (1991), 1026–1046.3. 求二部图),(Y X G =的边正常)(G Δ染色的算法z 算法思想:给G 添加必要的顶点使得||||Y X =,再添加必要的边使得G 成为)(G Δ正则二部图,所得图记为*G ,然后反复运用匈牙利算法求*G 的完美匹配。
计算机学科领域高质量国际学术会议分区表1.AREA: Data Bases一区 (332)1.SIGMOD: ACM SIGMOD Conf on Management of Data (78)2.PODS: ACM SIGMOD Conf on Principles of DB Systems(30)3.VLDB: Very Large Data Bases (96)4.SIGKDD –ACM International Conference on Knowledge Discovery andData Mining (128)二区 (230)1.ICDE: Intl Conf on Data Engineering (93)2.EDBT /ICDT: EDBT/ICDT joint conference (27)3.ICDM - IEEE International Conference on Data Mining (70)4.SDM - SIAM Conference on Data Mining (40)2.AREA: Software Engineering:一区(225)1.ICSE: International Conference on Software Engineering (56)2.FSE: ACM Conference on the Foundations of Software Engineering (42)3.OOPSLA: ACM SIGPLAN Conference on Object-Oriented ProgrammingSystems, Languages and Applications (33)4.ASE: IEEE International Conference on Automated Software Engineering(94)二区 (230)1.ISSTA: ACM SIGSOFT International Symposium on Software Testing andAnalysis (33)2.ECOOP: European Conference on Object-Oriented Programming (27)3.ESEC: European Software Engineering Conference (50)4.ICSM: IEEE International Conference on Software Maintenance (40)5.RE: IEEE International Conference on Requirements Engineering (39)6.ICSR: International Conference on Software Reuse (41)3.AREA: Security:一区 (102)1.S&P: IEEE Symposium on Security and Privacy (28)S: ACM Conference on Computer and Communications Security (51)enix security: Usenix Symposium on Security (23)二区 (68)1.NDSS: ISOC Network and Distributed System Security Symposium (22)2.ACSAC: Annual Computer Security Applications (46)4.AREA: Architecture一区 (136)1.ISCA: ACM/IEEE Symp on Computer Architecture (37)2.MICRO: Intl Symp on Microarchitecture (35)3.HPCA: IEEE Symp on High-Perf Comp Architecture (34)4.PACT: IEEE Intl Conf on Parallel Architectures and CompilationTechniques (30)二区(22)1.ISPASS: IEEE International Symposium on Performance Analysis ofSystems and Software (22)5.AREA: Programming Languages:一区(95)1.PLDI: ACM-SIGPLAN Symposium on Programming Language Design &Implementation (34)2.POPL: ACM-SIGACT Symposium on Principles of ProgrammingLanguages (35)3.PPoPP: ACM SIGPLAN Symposium on Principles and Practice of ParallelProgramming(26)二区 (21)1.CGO: International Symposium on Code Generation and Optimization6.AREA: System Technology一区(114)1.OSDI: USENIX Operating Systems Design and Implementation (26/2=13)2.SOSP: ACM SIGOPS Symp on OS Principles (25/2=13)3.ASPLOS: Architectural Support for Prog Lang and OS (31)4.FAST: USENIX Conference on File and Storage Technologies (23)enix: Annual Usenix Technical Conference (34)二区(155)1.DSN: Annual IEEE/IFIP International Conference on Dependable Systemsand Networks (59)2.Eurosys: European Conference in Computer Systems (26)3.HOTOS: Workshop on Hot Topics in Operating Systems (24)4.SRDS: Symp on Reliable Distributed Systems (28)5.VEE: International Conference on Virtual Execution Environments. 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Lammps静水压力引言Lammps是一个经典分子动力学软件包,广泛应用于材料科学和生物物理学领域。
其中一个重要的应用是计算系统的静水压力。
本文将深入探讨如何使用Lammps计算静水压力,并介绍相关的理论和方法。
理论背景在分子动力学模拟中,静水压力是指系统受到的压力,当系统达到平衡状态时,压力保持不变。
静水压力可以通过计算系统的压强得到,压强定义为单位面积上受到的力。
在Lammps中,可以通过计算压强张量的平均值来获得静水压力。
Lammps计算压强的命令在Lammps中,可以使用compute pressure命令来计算压强。
该命令需要定义一个计算区域,并指定计算压强所需要的参数。
下面是一个示例命令:compute pressure all pressure thermo_temp上述命令中,all表示计算区域为整个系统,pressure表示计算压强,thermo_temp 表示使用系统温度来计算压强。
计算静水压力的步骤要计算系统的静水压力,可以按照以下步骤进行:1.创建模拟系统:使用Lammps创建一个包含水分子的模拟系统。
2.定义计算区域:使用Lammps的region命令定义计算区域。
3.计算压强:使用compute pressure命令计算压强。
4.平均压强:使用Lammps的thermo_style命令设置输出格式,并使用thermo_modify命令设置平均压强的时间间隔。
5.运行模拟:运行Lammps模拟以达到平衡状态。
6.输出结果:使用Lammps的thermo命令输出平均压强。
示例代码下面是一个使用Lammps计算静水压力的示例代码:# Lammps input script for calculating static water pressure# Step 1: Create simulation systemunits realatom_style full# Step 2: Define compute regionregion box block 0 10 0 10 0 10create_box 1 boxcreate_atoms 1 box# Step 3: Compute pressurecompute pressure all pressure thermo_temp# Step 4: Average pressurethermo_style custom step temp pressthermo_modify flush yesthermo 100# Step 5: Run simulationvelocity all create 300 12345fix 1 all nverun 1000# Step 6: Output resultsvariable avg_press equal c_pressure[1]print "Average pressure: ${avg_press}"结论本文介绍了如何使用Lammps计算静水压力的方法。
一、概述在材料科学与工程领域,对材料的机械性能进行模拟与分析是十分重要的。
LAMMPS作为一款开源的分子动力学模拟软件,可以用来模拟原子尺度的材料性能,包括应变、应力、位移等参数的计算。
本文将以模拟Cu三点弯曲为例,介绍LAMMPS软件的使用与编写相应的案例代码。
二、案例代码编写1. 创建Cu原子模型首先需要在LAMMPS中创建Cu原子模型,可以使用内建的原子模型创建指令,例如:```units metaldimension 3boundary p p patom_style atomiclattice fcc 3.615region box block 0 20 0 20 0 20create_box 1 boxcreate_atoms 1 box```2. 定义模拟参数接下来需要定义模拟所需的参数,包括弯曲速度、模拟时间等,示例代码如下:```p本人r_style eam/fsp本人r_coeff * * Cu_u3.eamvariable str本人n equal 0.05variable steps equal xxxvariable d equal 0.05/v_stepsfix 1 all nvefix 2 all setforce 0.0 0.0 0.0fix 3 all move box delta v_d 0 0 sum v_str本人n 0 0```其中,p本人r_style为相互作用模型,p本人r_coeff为相互作用参数,variable为定义参数,fix为模拟中的固定条件。
3. 运行模拟需要运行模拟并输出结果,可以使用以下指令:```timestep 0.001thermo xxxthermo_style custom step temp etotal pressdump 1 all custom 1000 mmpstrj id type x y z vx vy vz fx fy fzrun xxx```三、结果分析通过对模拟结果的分析,可以得到Cu材料在三点弯曲载荷下的应变、应力分布情况,以及原子间的位移和相互作用力等信息,这对于理解材料在应力作用下的行为具有重要意义。
nature science上关于计算机视觉的一些原创文献1. D. Marr; T. Poggio.Cooperative Computation of Stereo Disparity.Science, New Series, Vol. 194, No. 4262. (Oct. 15, 1976), pp. 283-287. 这一篇是marr计算机视觉框架的开创性论文,到目前为止,计算机视觉基本上都在这个框架里做。
2. LONGUET-HIGGINS H C.A computer algorithm for reconstructing a scene from two projections[J].Nature,1981,293:133-135. 这一篇奠定了计算机视觉三维重构的基础,又称"八点算法”,导致计算机视觉三维重构热了20多年。
3. H. Bülthoff*, J. Little & T. Poggio.A parallel algorithm for real-time computation of optical flow.Nature 337, 549 - 553 (09 February 1989) ,光流实时并行算法的原始创新链接:/nature/journal/v337/n6207/abs/337549a0.html。
4. Hurlbert, A., and Poggio, T. 1986. Visual information: Do computers need attention?Nature 321(12).5. Dov Sagi* & Bela Julesz.Enhanced detection in the aperture of focal attention during simple discrimination tasks.Nature 321, 693 - 695 (12 June 1986)6. Gad Geiger; Tomaso Poggio.Science, New Series, Vol. 190, No. 4213. (Oct. 31, 1975), pp. 479-480.7. Gad Geiger; Tomaso Poggio.The Müller-Lyer Figure and the Fly.Science, New Series, Vol. 190, No. 4213. (Oct. 31, 1975), pp. 479-480.8. P. Sinha and T. Poggio.Role of Learning in Three-dimensional Form Perception," . Nature, Vol. 384, No. 6608, 460-463, 1996.9. Hubel DH,Wiesel TN.Cells sensitive to binocular depth in area 18 of the macaque monkey cortex.Nature,1970,225∶41~42 10.Livingstone M and Hubel D.Segregation of form, color, movement and depth: Anatomy, physiology and perception. Science, 1988, 240∶740~-749. 被引用1372次,关于眼睛立体视觉机制的原创论文。
lammps扩散系数概述扩散是物质在空间中的自由移动过程,它在自然界和工程应用中起着重要的作用。
为了研究扩散现象,科学家们提出了各种数学模型和实验方法。
在计算科学中,使用分子动力学模拟是一种常见的方法来研究扩散系数。
LAMMPS(Large-scale Atomic/Molecular Massively Parallel Simulator)是一种基于分子动力学模拟的开源软件,它能够模拟原子和分子在材料中的运动。
本文将探讨如何使用LAMMPS计算扩散系数。
LAMMPS简介LAMMPS是一种高性能的分子动力学软件,可以用于模拟原子、分子和大分子的动力学行为。
它支持多种势函数和算法,并能够进行并行计算,适用于从纳米尺度到宏观尺度的研究。
LAMMPS的输入文件是通过脚本语言来定义模拟的参数和条件。
扩散系数的计算方法扩散系数描述了物质在单位时间内通过单位面积的扩散量。
在分子动力学模拟中,可以使用Einstein关系来计算扩散系数。
Einstein关系可以用来将扩散系数与物质的平均方均位移(MSD)相关联:D=⟨r2⟩6t其中,D表示扩散系数,⟨r2⟩表示物质的平均方均位移,t表示时间。
LAMMPS计算扩散系数的步骤步骤一:创建输入文件首先,需要创建一个LAMMPS的输入文件。
输入文件可以使用文本编辑器创建,后缀名为.in。
在输入文件中,需要定义原子类型、势函数、初始位置和速度等参数。
步骤二:定义分子动力学模拟参数在输入文件中,需要定义分子动力学模拟的参数。
这些参数包括模拟的时间步长、模拟的时间长度、温度等。
步骤三:运行分子动力学模拟在命令行中运行LAMMPS软件,并指定输入文件。
步骤四:分析模拟结果使用LAMMPS的后处理工具分析模拟结果。
这些工具可以计算平均方均位移等参数。
步骤五:计算扩散系数使用Einstein关系,将平均方均位移与时间相关联,计算扩散系数。
实例演示以下是一个使用LAMMPS计算扩散系数的示例:1.创建一个输入文件diffusion.in,定义模拟的系统和参数。
distributeddataparallel reduce [DistributedDataParallel reduce]: Exploring Distributed Data Parallel Reduce in Deep LearningIntroduction:Deep learning has revolutionized the field of artificial intelligence by enabling us to train complex neural networks with massive amounts of data. However, as the size of the datasets and models continue to grow, the computational demands needed to train these models also increase. To tackle this challenge, distributed computing has emerged as a powerful technique to distribute the workload across multiple devices and machines. In this article, we will delve into the concept of distributed data parallel reduce, a key component in distributed deep learning, and walk through its implementation step by step.1. What is Distributed Data Parallel?Distributed Data Parallel (DDP) is a training strategy that divides large deep learning models across multiple devices or machines for simultaneous training. Each device or machine works on a portion of the dataset and computes gradients on a subset of the model parameters. By utilizing all available computing resources, DDPsignificantly reduces training time for large-scale models.2. The Need for Reduce Operation:During the training process, the gradients computed on different devices need to be synchronized and averaged to update the model parameters. The reduce operation plays a crucial role in this step by aggregating the gradients across all devices and calculating the average. Without the reduce operation, each device would only have access to its own local gradients, resulting in inconsistent updates and suboptimal convergence.3. The Process of Distributed Data Parallel Reduce:Let's outline the steps involved in performing distributed data parallel reduce:Step 1: Model Initialization and Data PartitioningFirst, the model is initialized on each device or machine. Then, the dataset is divided into multiple partitions, with each partition assigned to a specific device or machine. This ensures that each device trains on a different subset of the data.Step 2: Forward and Backward PassDuring the training process, each device performs a forward pass on its assigned data batch and computes the corresponding gradients during the backward pass. These gradients are the local gradients specific to each device and need to be aggregated for the next step.Step 3: All-Reduce OperationThe all-reduce operation, a collective communication step, is responsible for gathering all the gradients from each device, adding them together, and then broadcasting the sum back to all devices. Popular methods for implementing all-reduce include ring-based algorithms or tree-based algorithms. This process ensures that all devices have access to the aggregated gradients.Step 4: Gradient Averaging and Parameter UpdateAfter the all-reduce operation, each device receives the averaged gradients. These averaged gradients are then used to update the model parameters simultaneously across all devices. By synchronizing the parameter update, DDP ensures that consistency is maintained across all devices.4. Performance and Scalability Considerations:Implementing distributed data parallel reduce can significantly improve training efficiency and scalability. However, various factors need to be considered to maximize performance. These include the network bandwidth between devices, the computational power of each device, the latency of the all-reduce operation, and the load balancing among devices. Optimizing these factors is crucial for achieving efficient distributed training.Conclusion:Distributed data parallel reduce is a critical component in distributed deep learning, allowing us to train large-scale models efficiently across multiple devices or machines. By dividing the workload and aggregating gradients through the all-reduce operation, we make the most of available computing resources and reduce training time. As researchers continue to explore distributed computing techniques, we can expect even faster and more scalable training methods in the future.。
lammps 单原子应力引言LAMMPS(Large-scale Atomic/Molecular Massively Parallel Simulator)是一种用于分子动力学模拟的开源软件。
通过LAMMPS,我们可以模拟原子和分子在不同条件下的行为,如温度、压力和应力等。
本文将讨论使用LAMMPS模拟单原子的应力。
在分子动力学模拟中,应力是一个非常重要的物理量,它可以帮助我们理解材料的力学性质和行为。
什么是单原子应力?在模拟中,单原子应力指的是通过对单个原子施加外力来计算其受力情况。
这种方法通过施加一个负责的力来扰动原子,并通过观察原子的响应来计算应力。
这种技术广泛应用于研究纳米材料和纳米器件。
模拟设置为了模拟单原子的应力,我们需要考虑以下几个关键设置:1. 原子模型在LAMMPS中,我们使用原子模型来描述材料的结构。
不同的材料需要使用不同的原子模型。
在单原子应力模拟中,我们可以选择一个适合的原子模型,如简单立方格子结构或面心立方格子结构。
2. 相互作用势函数相互作用势函数是描述原子之间相互作用的数学公式。
通过选择适当的相互作用势函数,我们可以模拟不同材料的行为。
在单原子应力模拟中,我们可以使用经典的势函数,如Lennard-Jones势函数。
3. 温度和压力为了模拟原子的应力,我们需要指定适当的温度和压力条件。
可以通过设置温度和压力来模拟不同的物理环境,如恒温和恒压条件。
4. 模拟时间和步长在模拟中,我们需要指定模拟的时间范围和时间步长。
较小的时间步长可以提高模拟的准确性,但也会增加计算的时间。
因此,需要在时间步长和模拟时间之间进行权衡。
模拟步骤下面是模拟单原子应力的一般步骤:1.创建原子模型:使用LAMMPS的命令或脚本创建适当的原子模型,并设定原子的初始位置和速度。
2.设定相互作用势函数:选择适当的相互作用势函数,并配置模拟中的参数。
3.设置温度和压力:设定模拟中的温度和压力条件,如恒温和恒压条件。
Parallel Algorithms for Forward and Back Substitution in Direct Solution of Sparse LinearSystems∗A NSHUL G UPT AIBM T.J.W A TSON R ESEARCH C ENTERY ORKTOWN H EIGHTS,NY10598ANSHUL@WA V IPIN K UMARD EP ARTMENT OF C OMPUTER S CIENCEU NIVERSITY OF M INNESOT AM INNEAPOLIS,MN55455KUMAR@AbstractA few parallel algorithms for solving triangular systemsresulting from parallel factorization of sparse linear sys-tems have been proposed and implemented recently.Wepresent a detailed analysis of parallel complexity and scal-ability of the best of these algorithms and the results ofits implementation on up to256processors of the CrayT3D parallel computer.It has been a common belief thatparallel sparse triangular solvers are quite unscalable dueto a high communication to computation ratio.Our anal-ysis and experiments show that,although not as scalableas the best parallel sparse Cholesky factorization algo-rithms,parallel sparse triangular solvers can yield reason-able speedups in runtime on hundreds of processors.Wealso show that for a wide class of problems,the sparse tri-angular solvers described in this paper are optimal and areasymptotically as scalable as a dense triangular solver.1IntroductionThe process of obtaining a direct solution to a sparse system of linear equations usually consists of four phases:reordering,symbolic fac-torization,numerical factorization,and solving the lower-and upper-triangular systems resulting from factorization.Since numerical fac-torization is computationally the most expensive phase,a significant research effort has been directed towards developing efficient and scalable parallel sparse factorization algorithms.We have recently proposed[4]a parallel sparse Cholesky factorization algorithm that is optimally scalable for a wide class of problems.Experiments have shown that this algorithm can easily speedup Cholesky factorization by a factor of at least a few hundred on up to1024processors.With such speedups in numerical factorization,it is imperative that the re-maining phases of the solution process be parallelized effectively in order to scale the performance of the overall solver.Furthermore, without an overall parallel solver,the size of the sparse systems that can be solved may be severely restricted by the amount of memory available on a uniprocessor system.In this paper,we address the problem of performing thefinal phase of forward and backward substitution in parallel on a distributed mem-ory multiprocessor.We present a detailed analysis of the parallel complexity and scalability of parallel algorithm described briefly in[5] to obtain a solution to the system of sparse linear equations of the forms LY=B and U X=Y,where L is a lower triangular matrix and U is an upper triangular matrix.Here L and U are obtained from the numerical factorization of a sparse coefficient matrix A of the original system AX=B to be solved.If A,L,and U are N×N matrices,then X,Y,and B are N×m matrices,where m is the number of right-hand side vectors for which the solution to the sparse linear system with A as the coefficient matrix is desired.Our analysis and experi-ments show that,although not as scalable as the best parallel sparse Cholesky factorization algorithms,parallel sparse triangular solvers can yield reasonable speedups in runtime on hundreds of processors. We also show that for a wide class of problems,the sparse triangular solvers described in this paper are optimal and are asymptotically as scalable as a dense triangular solver.For a single right-hand side(m=1),our experiments show a 256-processor performance of up to435MFLOPS on a Cray T3D,on which the single-processor performance for the same problem is≈8.6 MFLOPS.With m=30,the maximum single-processor and256-processor performance observed in our experiments is≈30MFLOPS and≈3050MFLOPS,respectively.T o the best of our knowledge,this is the highest performance and speedup for this problem reported on any massively parallel computer.In addition to the performance and scalability analysis of parallel sparse triangular solvers,we discuss the redistribution of the triangu-lar factor matrix among the processors between numerical factoriza-tion and triangular solution,and its impact on performance.In[4],we describe an optimal data-distribution scheme for Cholesky factoriza-tion of sparse matrices.This distribution leaves groups of consecutive columns of L with identical pattern of non-zeros(henceforth called supernodes)with a two-dimensional partitioning among groups of processors.However,this distribution is not suitable for the triangular solvers,which are scalable only with a one-dimensional partition-ing of the supernodal blocks of L.We show that if the supernodes are distributed in a subtree-to-subcube manner[2]then the cost of converting the two-dimensional distribution to a one-dimensional dis-tribution is only a constant times the cost of solving the triangular systems.From our experiments,we observed that this constant is fairly small on the Cray T3D—at most0.9for a single right-hand side vector among the test cases used in our experiments.Of course,if more than one systems need to be solved with the same coefficient matrix,then the one-time redistribution cost is amortized.2Algorithm DescriptionIn this section,we describe parallel algorithms for sparse forward elimination and backward substitution,which have been discussed briefly in[5].The description in this section assumes a single right-hand side vector;however,the algorithm can easily be generalized to multiple right-hand sides by replacing all vector operations by the corresponding matrix operations.1234567891011121314151718160123456789101112131415161718X X X X X X X X X X X X X X X X X X X X X X X X X X X X X X X X X X X X X X X X X X X X X X X X X X X X X X X X X X X X X X X X X X X X X X X X X X X X X X X X X X X X X X X X X X X X X X X 0134910121325111467815161718Level 3Level 0Level 1Level 2P P P P P P P P 1234567P P P P P P P 0,102,34,56,70,1,2,34,5,6,70,1,2,3,4,5,6,7(a)(b)Figure 1:A symmetric sparse matrix and the associated elimination tree with subtree-to-subcube mapping onto 8processors.The nonzeros in the original matrix are denoted by the symbol “×”and fill-ins are denoted by the symbol “◦”.2.1Forward eliminationThe basic approach to forward elimination is very similar to that of multifrontal numerical factorization [12]guided by an elimination tree [13,8]with the distribution of computation determined by a subtree-to-subcube mapping [2].A symmetric sparse matrix,its lower triangular Cholesky factor,and the corresponding elimination tree with subtree-to-subcube mapping onto 8processors is shown in Figure 1.The computation in forward elimination starts with the leaf supernodes of the elimination tree and progresses upwards to terminate at the root supernode.A supernode is a set of columns i 1,i 2,...,i t of the sparse matrix such that all of them have non-zeros in identical locations and i j +1is the parent of i j in the elimination tree for 1≤j <t .For example,in Figure 1,nodes 6,7,and 8form a su-pernode.The portion of the lower triangular matrix L corresponding to a supernode is a dense trapezoidal block of width t and maximum height n ,where t is the number of nodes in the supernode and n is the number of non-zeros in the leftmost column of the supernode.Figure 2outlines the forward elimination process across three levels of the left half of the elimination tree of Figure 1.One of the blocks of L shown in Figure 2is the dense trapezoidal supernode consisting of nodes 6,7,and 8.For this supernode,n =4and t =3.As in the case of multifrontal numerical factorization [12],the com-putation in forward and backward triangular solvers can also be or-ganized in terms of dense matrix operations.In forward elimination (see Figure 2),before the computation starts at a supernode,theLRHS 0134Figure 2:Pictorial representation of forward elimination along three levels of an elimination tree.The color of an RHS box is determined by the color(s)of the box(es)at the next lower level that contribute to its value.elements of the right-hand side vector with the same indices as the nodes of the supernode are collected in the first t contiguous loca-tions in a vector of length n .The remaining n −t entries of this vector are filled with zeros.The computation corresponding to a trapezoidal supernode,which starts at the leaves,consists of two parts.The first computation step is to solve the dense triangular system at the top of the trapezoid (above the dotted line in Figure 2).The second step is to subtract the product of the vector of length t (above the dotted line)with the (n −t )×t submatrix of L (below the dotted line)from the vector of length n −t (below the dotted line).After these two computation steps,the entries in the lower part of the vector of length n −t are subtracted from the corresponding (i.e.,with the same index in the original matrix)entries of the vector accompany-ing the parent supernode.The computation at any supernode in the tree can commence after the contributions from all its children have been collected.The algorithm terminates after the computation at the triangular supernode at the root of the elimination tree.In a parallel implementation on p processors,a supernode at level l (see Figure 1)from the top is distributed among p /2l processors.The computation at a level greater than or equal to log p is performedsequentially on a single processor assigned to that subtree.However, the computation steps mentioned above must be performed in parallel on p/2l processors for a supernode with0≤l<log p.In[6],Heath and Romine describe efficient pipelined or wavefront algorithms for solving dense triangular systems with block-cyclic row-wise and column-wise partitioning of the triangular matrices.We use variations of the same algorithms on the dense trapezoidal supern-odes at each of the parallel levels of the elimination tree.the number of processors among which a supernode is partitioned varies with its level in the tree,but the same basic parallel algorithm is used for each supernode.Figure3(a)shows hypothetical forward elimination on a supernode with an unlimited number of processors on an EREW-PRAM.From thisfigure,it is clear that,due to data dependencies,at a time only max(t,n/2)processors can remain busy.Since the com-putation proceeds along a diagonal wave from the upper-left to the lower-right corner of the supernode,at any given time,only one block per row and one element per column is active.From this observation, it can be shown that an efficient parallel algorithm(an algorithm ca-pable of delivering a speedup of (p)using p processors)for forward elimination must employ a one-dimensional row-wise or column-wise partitioning of the supernode so that all processor can be busy at all times(or most of the time).From a practical perspective,we chose a row-wise block-cyclic partitioning because n≥t and a more uniform partitioning with reasonable block sizes can be obtained if the rows are partitioned.Figures3(b)and(c)illustrate two variations of the pipelined forward elimination with block-cyclic row-wise partitioning of the supernode.Each box in thefigure can be regarded as a b×b square block of the supernode(note that the diagonal boxes repre-sent lower triangular blocks).In the column-priority algorithm,the computation along a column of the supernode isfinished before a new column is started.In the row-priority algorithm,the computation along a row isfinished before a new row is started.2.2Backward substitutionThe algorithm for parallel backward substitution is very similar.Since an upper triangular system is being solved,the supernodes are or-ganized as dense trapezoidal matrices of height t and width n(n≥t) and a column-wise block-cyclic partitioning is used at the top log p levels of the elimination tree.In backward substitution,the computa-tion starts at the root of the elimination tree and progresses down to the leaves.First,the entries from the right-hand side vector with the same indices as the nodes of a supernode are collected in thefirst t contiguous locations of a vector of length n.The remaining n−t entries of this vector are copied from the entries with same indices in the vector accompanying the parent supernode.This step is not per-four processors. with cyclic mapping of rows onto (b) Row-priority pipelined computation number of processors. EREW-PRAM with unlimited(a) Pipelined computation on anonto four processors.tation with cyclic mapping of rows (c) Column-priority pipelined compu-Figure 3:Progression of computation consistent with data dependencies in parallel pipelined forward elimination in a hypothetical supernode of the lower-triangular factor matrix L .The number in each box of L represents the time step in which the coresponding element of L is used in the munication delays are ignored in this figure and the computation time for each box is assumed to be identical.In parts (b)and (c),the supernode is partitioned among the processors using a cyclic mapping.A block-cyclic mapping can be visualized by regarding each box as a b ×b block (the diagonal boxes will represent triangular blocks).formed for the root supernode,which does not have a parent and for which n =t .The computation at a supernode consists of two steps and can proceed only after the computation at its parent supernode is finished.The first computation step is to subtract the product of the t ×(n −t )rectangular portion of the supernode with the lower part of the vector of size n −t from the upper part of the vector of size t .The second step is to solve the triangular system formed by the t ×t triangle of the trapezoidal supernode and the upper part of the vector of size t .Just like forward elimination,these steps are carried out serially for supernodes at levels greater than or equal to log p in the elimination tree.For the supernodes at levels 0through log p −1,the computation is performed using a pipelined parallel algorithm.Figure 4illustrates the pipelined algorithm on four processors with column-wise cyclic mapping.The algorithm with a block-cyclic map-ping can be visualized by regarding each box in Figure 4as a square block (the blocks along the diagonal of the trapezoid are triangular)of size b ×b .In both forward and backward triangular solvers described in this section,if the system needs to be solved with respect to more than one,say m ,right-hand sides,then the vectors of length n are replaced by rectangular n ×m matrices.The overall algorithms remain identicaltnFigure 4:Column-priority pipelined backward substitution on a hypothetical su-pernode distributed among 4processors using column-wise cyclic mapping.except that all vector operations are replaced by the corresponding matrix operations,the size of the matrix being the length of the vector times the number of vectors.3AnalysisIn this section we derive expressions for the communication over-heads and analyze the scalability of the sparse supernodal multi-frontal triangular solvers described in Section 2.We will present the analysis for the forward elimination phase only;however,the reader can verify that the expressions for the communication overhead are identical for backward substitution.3.1Communication overheadsIt is difficult to derive analytical expressions for general sparse ma-trices because the location and amount of fill-in,and hence,the distribution and the number if non-zeros in L ,is a function of the the number and position of nonzeros in the original matrix.Therefore,we will focus on the problems in which the original matrix is the adja-cency matrix of a two-or three-dimensional neighborhood graph [14].These classes of matrices include the coefficient matrices generated in all two-and three-dimensional finite element and finite difference problems.We also assume as that a nested-dissection based fill-reducing ordering is used,which results in an almost balanced elim-ination tree.The subtree-to-subcube assignment of the elimination tree to the processors relies heavily on a balanced tree.Although there are bound to be overheads due to unequal distribution of work,it is not possible to model such overheads analytically because the ex-tent of such overheads is data-dependent.From our experience withactual implementations of parallel triangular solvers as well as par-allel factorization codes[4],we have observed that such overheads are usually not excessive.Moreover,the overhead due to load imbal-ance in most practical cases tends to saturate at32to64processors for most problems and does not continue to increase as the number of processors are increased.In the remainder of this section,we will concentrate on overheads due to inter-processor communication only.Consider the column-priority pipelined algorithm for forward elimi-nation shown in Figure3(c).Let b be the block size in the block-cyclic mapping.A piece of the vector of size b is transferred from a proces-sor to its neighbor in each step of the algorithm until the computation moves below the upper triangular part of the trapezoidal supernode. If a supernode is distributed among q processors,then during the entire computation at a supernode,q+t/b−1such communication steps are performed;q−1steps are required for the computation to reach the last processor in the pipeline and t/b steps to pass the entire data(of length t)through the pipeline.Thus,the total com-munication time is proportional to b(q−1)+t,which is O(q)+O(t), assuming that b is a constant.Besides the communication involved in the pipelined processing over a supernode,there is some more communication involved in collecting the contributions of the vectors associated with the children of a supernode into the vector associated with the parent supernode. If the two child supernodes are each distributed among q processors, then this communication is equivalent to an all-to-all personalized communication[8]among2q processors with a data size of roughly t/q on each processor.This communication can be accomplished in time proportional to t/q,which is asymptotically smaller than the O(q)+O(t)time spent during the pipelined computation phase at the child supernodes.Therefore,in the remainder of this section,we will ignore the communication required to transfer the contributions of the vector across the supernodes at different levels of the elimination tree.So far we have established that a time proportional to b(q−1)+t (or roughly,bq+t)is spent while processing an n×t trapezoidal supernode on q processors with a block-cyclic mapping that uses blocks of size b.We can now derive an expression for the overall communication time for the entire parallel forward elimination process by substituting for q and t in the expression bq+t for a supernode at level l and summing up the resulting expression over all levels.Let usfirst consider a sparse linear system of N equations resulting from a two-dimensionalfinite element problem being solved on p pro-cessors.As a result of using the subtree-to-subcube mapping,q at a level l is p/2l.If a nested-dissection based ordering scheme is usedto number the nodes of the graph corresponding to the coefficient ma-trix,then the number of nodes t in a supernode at level l isαN/2l), which is O(p)+O(√p )+O(√p)+O(N2/3)+O(p).(2) If more than one(say m)right-hand side vectors are present in the system,then each term in Equations1and2is multiplied with m. 3.2Scalability analysisThe scalability of a parallel algorithm on a parallel architecture refers to the capacity of the algorithm-architecture combination to effectively utilize an increasing number of processors.In this section we use the isoefficiency metric[8,9,3]to characterize the scalability of the algorithm described in Section2.The isoefficiency function relates the problem size to the number of processors necessary to maintain afixed efficiency or to deliver speedups increasing proportionally with increasing number of processors.Let W be the size of a problem in terms of the total number of basic operations required to solve a problem on a serial computer.N)For example,W=O(N2)for multiplying a dense N×N matrix with an N-vector.The serial run time of a problem of size W is given by T S=t c W,where t c is the time to perform a single basic computation step.If T P is the parallel run time of the same problem on p proces-sors,then we define an overhead function T o as pT P−T S.Both T P and T o are functions of W and p,and we often write them as T P(W,p) and T o(W,p),respectively.The efficiency of a parallel system with p processors is given by E=T S/(T S+T o(W,p)).If a parallel system is used to solve a problem instance of afixed size W,then the effi-ciency decreases as p increases.This is because the total overhead T o(W,p)increases with p.For many parallel systems,for afixed p,if the problem size W is increased,then the efficiency increases because for a given p,T o(W,p)grows slower than O(W).For these parallel systems,the efficiency can be maintained at a desired value (between0and1)with increasing p,provided W is also increased. We call such systems scalable parallel systems.Note that for differ-ent parallel algorithms,W may have to increase at different rates with respect to p in order to maintain afixed efficiency.As the number of processors are increased,the smaller the growth rate of problem size required to maintain afixed efficiency,the more scalable the parallel system is.Given that E=1/(1+T o(W,p)/(t c W)),in order to maintain afixed efficiency,W should be proportional to T o(W,p).In other words, the following relation must be satisfied in order to maintain afixed efficiency:W=eN).(4) Balancing W against thefirst term in the expression for T o yields the following(see Appendix A for details):W∝p2,(5)and balancing it against the second term in the expression for T o yieldsp2W∝forward and backward triangular solvers are asymptotically as scal-able as their dense counterparts.From this observation,it can beargued that the sparse algorithms,at least in the case of matricesassociated with three-dimensional neighborhood graphs are optimal. The topmost supernode in such a matrix is an N2/3×N2/3dense triangle.Solving a triangular system corresponding to this supern-ode involves asymptotically a computation of the same complexity assolving the entire sparse triangular system.Thus,the overall scal-ability cannot be better than that of solving the topmost N2/3×N2/3 dense triangular system in parallel,which is O(p2).4Data Distribution for Efficient Triangular SolutionIn Section2and in[8],we discuss that in order to implement the stepsof dense triangular solution efficiently,the matrix must be partitionedamong the processors along the rows or along the columns.However,as we have shown in[4],the dense supernodes must be partitioned along both dimensions for the numerical factorization phase to be effi-cient.The table in Figure5shows the communication overheads and the isoefficiency functions for parallel dense and sparse factorization and triangular solution using one-and two-dimensional partitioning schemes.The most efficient scheme in each category is denoted by a shaded box in the table.The last column of the table shows the overall isoefficiency function of the combination of factorization and triangular solvers.Note that the triangular solvers are unscalable by themselves if the dense supernodal blocks of the triangular factor are partitioned in two dimensions.However,the asymptotic communica-tion overhead of the unscalable formulation of the triangular solvers does not exceed the communication overhead of the factorization process.As a result,the overall isoefficiency function is dominated by that of factorization.Hence,for a solving a system with a single right-hand side vectors(or a small constant number of them),the unscalability of the triangular solvers should not be of much concern. However,if solutions with respect to a number of right-hand side vec-tors are required,then for both the factorization and triangular solution to be efficient together,each supernode must be redistributed among the processors that share it.This redistribution must convert the orig-inal two-dimensional block-cyclic partitioning into a one-dimensional block-cyclic partitioning.In this section we show that the time spent in this redistribution is not asymptotically higher than the parallel run time of the triangular solvers.Consider an n×t dense supernode mapped onto a√q logical grid of processors using a two dimensional partitioning.As shownFigure5:A table of communication overheads and isoefficiency functions for sparse factorization and triangular solution with different partitioning schemes.in Figure6,the redistribution is equivalent to a transposition of each (n/√q proces-sor on which it is horizontally partitioned.This is an all-to-all person-alized communication operation[8]among√tnFigure 6:Converting the two-dimensional partitioning of a supernode into one-dimensional partitioning.in [4].Figures 7and 8show the performance of the parallel triangular solvers on a Cray T3D.In the table in Figure 7,we show the time in seconds and the perfor-mance in MFLOPS on a selected number of processors for five test matrices with the number of right-hand side vectors varying from 1to 30.T o facilitate a comparison of the times for various phases of the solution processes,the table also contains the factorization run time and MFLOPS,as well as the time to redistribute the factor matrix to convert the supernodes from a two-dimensional to a one-dimensional partitioning among the processors.As shown in Figure 7,for a single right-hand side vector,the highest performance achieved on a 256-processor Cray T3D is approximately 435MFLOPS,which increases to over 3GFLOPS if a solution with 30right-hand side vectors is paring with the single-processor performance for BC-SSTK15,this represents roughly 50-and 100-fold enhancement in performance on 256processors for 1and 30right-hand side vec-tors,respectively.There are two other important observations to be made from the table in Figure 7.First,despite a highly scalable im-plementation of sparse Cholesky factorization,parallelization of the relatively less scalable triangular solvers can speed them enough so that their runtime is still a small fraction of the factorization time.Sec-ond,although efficient implementations of factorization and triangular solvers use different data partitioning schemes,the redistribution of the data,on an average,takes much less time than the triangular solvers for a single right-hand side vector on the T3D.Figure 8shows the plots of MFLOPS versus number of processorsBCSSTK15: N = 3948; Factorization Opcount = 85.5 Million; Nonzeros in factor = 0.49 Million NRHS FBsolve time (sec.)FBsolve MFOLPS 521.510203026.529.430.018.6213.7.228.284.452.740 1.33 1.92Factorization time = .721 sec.Factorization MFLOPS = 3871Time to redistribute L = .035 sec.Factorization MFLOPS = 800Time to redistribute L = .009 sec.Factorization time = .107 sec.Factorization time = 5.59 sec.Factorization MFLOPS = 499Time to redistribute L = .071 sec.Factorization time = 2.46 sec.Factorization MFLOPS = 34.8Time to redistribute L = 0.0 sec.p = 64p = 1NRHS FBsolve time (sec.)FBsolve MFOLPS 51020301281.5145285405527583.024.027.034.048.074.100BCSSTK31: N = 35588; Factorization Opcount = 2791 Million; Nonzeros in factor = 6.64 Million NRHS FBsolve time (sec.)FBsolve MFOLPS 510203012NRHS FBsolve time (sec.)FBsolve MFOLPS 510203012.073363.082646.1071240.1521738.24221992385.334HSCT21954: N = 21954; Factorization Opcount = 2822 Million; Nonzeros in factor = 5.84 Million p = 16.227115.274194.398330.614427 1.05498 1.51523COPTER2: N = 55476; Factorization Opcount = 8905 Million; Nonzeros in factor = 12.77 Million p = 256NRHS FBsolve time (sec.)FBsolve MFOLPS 510203012p = 256NRHS FBsolve time (sec.)FBsolve MFOLPS 510203012.117.130.167.232.364.5004347851526219528053053CUBE35: N = 42875; Factorization Opcount = 7912 Million; Nonzeros in factor = 9.95 Million.108.120.154.216.340.4683696651289183823452548NRHS FBsolve time (sec.)FBsolve MFOLPS 510203012p = 64.186.220.320.492.832 1.10274463795103612261277NRHS FBsolve time (sec.)FBsolve MFOLPS 510203012NRHS FBsolve time (sec.)FBsolve MFOLPS510203012p = 32.113.133.189.284.472.6722033476098099731025p = 32.245.296.436.681 1.21 1.72162269456583660693p = 256NRHS FBsolve time (sec.)FBsolve MFOLPS 510203012.091.122.099.161.234.312255471953145219912244p = 256Factorization time = 2.48 sec.Factorization MFLOPS = 1138Factorization time = 7.528 sec.Factorization MFLOPS = 1051Time to redistribute L = .13 sec.Factorization time = .619 sec.Factorization MFLOPS = 4560Time to redistribute L = .067 sec.Time to redistribute L = .10 sec.Factorization time = 1.846 sec.Time to redistribute L = .07 sec.Factorization time = 1.43 sec.Time to redistribute L = .08 sec.Factorization time = 5.764 sec.Factorization MFLOPS = 1545Time to redistribute L = .11 sec.Factorization MFLOPS = 4825Factorization MFLOPS = 5527Figure 7:A partial table of experimental results for sparse forward and backward substitution on a Cray T3D.In the above table,“NRHS”denotes the number of right-hand side vectors,“FBsolve time”denotes the total time spent in both the forward and the backward solvers,and “FBsolve MFLOPS”denotes the average performance of the solvers in million floating point operations per second.。