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电推进粒子网格法模拟中计算加速方法的研究综述

Research review of computational acceleration methods for particle-in-cell simulations of electric propulsion
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摘要 粒子网格法(PIC)模拟电推进装置等离子体时具有很强的第一性,但是模拟过程中计算负载很大,故PIC模拟的计算加速方法不可或缺。本文从电推进装置基本性质、低温等离子体物理特性和PIC算法特点作为切入点,明确了PIC方法在电推进装置模拟过程中计算负载高的原因;结合国内外的研究现状,从建模、时空尺度、算法与并行三个层面介绍了对应计算加速方法的原理和效果;对各类计算加速方法进行了总结和展望。 Particle-in-cell(PIC)simulation has a strong characteristic of first principle when simulating plasma in electric propulsion(EP)devices,but the calculation load is heavy during the simulation process.Thus,the acceleration methods for PIC algorithms are essential for the simulation.The calculation bottlenecks of PIC algorithm simulating EP devices are analyzed first,which are derived by the fundamental characteristics of EP devices,the physical properties of low-temperature plasmas,and the features of the PIC algorithm.At the same time,with the current research status at home and abroad,the principles and effects of corresponding calcu⁃lation acceleration methods are introduced from three aspects:modeling,spatiotemporal scales,as well as the al⁃gorithm and parallelization.Finally,a summary is made to outlook the various calculation acceleration methods.
作者 汤海滨 潘若剑 毛仁凡 崔云蔚 任军学 TANG Haibin;PAN Ruojian;MAO Renfan;CUI Yunwei;REN Junxue(School of Astronautics,Beihang University,Beijing 102206,China;Key Laboratory of Spacecraft Design Optimization and Dynamic Simulation Technologies,Ministry of Education,Beijing 102206,China;Laboratory of Space Environment Monitoring and Information Processing,Ministry of Industry and Information Technology,Beijing 102206,China;School of Space and Environment,Beihang University,Beijing 102206,China)
出处 《推进技术》 EI CAS CSCD 北大核心 2024年第8期1-25,共25页 Journal of Propulsion Technology
基金 国家自然科学基金(12372291) 基础加强计划重点基础研究项目(2022JCJQZD20600)。
关键词 电推进 PIC模拟 计算加速方法 并行计算 综述 Electric propulsion Particle-in-Cell(PIC)simulation Computational acceleration meth⁃ods Parallel computing Review
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  • 1于全芝,李玉同,张杰.Thomson散射诊断技术的新进展[J].物理,2004,33(6):446-451. 被引量:4
  • 2张郁.电推进技术的研究应用现状及其发展趋势[J].火箭推进,2005,31(2):27-36. 被引量:42
  • 3张天平.国外离子和霍尔电推进技术最新进展[J].真空与低温,2006,12(4):187-193. 被引量:61
  • 4樊箐 沈青.直接模拟蒙特卡罗方法中的一个新算法--随机取样频率法,计算流体力学的理论、方法和应用[M].科学出版社,1992..
  • 5蔡国飙,王慧玉,祖国君,张振鹏.真空小喷管羽流场的Monte Carlo直接模拟[J].推进技术,1997,18(2):44-49. 被引量:11
  • 6Burton R L, Turchi P J. Pulsed plasma thruster [ J ]. Journal of Propulsion and Power, 1998, 14 (5) : 716.
  • 7Keidar M, Boyd I D. Device and plume model of an electrothermal pulsed plasam thruster [ C ]//AIAA 2000-3430, 36th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, Huntsville, AL, 2000.
  • 8Yin X. Axisymmetric hybrid numerical modeling of pulsed plasma thruster plumes [ D ]. USA:Worcester Polytechnic Institute( Doctor), 1999.
  • 9Birdsall C K, Langdon A B. Plasma physics via computer simlation [ M]. New York: McGraw-Hill, 1955.
  • 10A Gatsonis N, Zwahlcn J, Wheelock A, et al. Pulsed plasma thruster plume investigation using a current-mode quadruple probe method [ J ]. Journal of Propulsion and Power, 2004, 20 (2): 243.

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