彈道學(xué)報(bào)第29卷總目次

2017年第1期(總第111期)

基于特征模型的高超聲速飛行器再入多約束預(yù)測(cè)控制

張 軍 李亞輝 朱晟楨 1∶1

火箭垂直回收著陸段在線(xiàn)制導(dǎo)凸優(yōu)化方法

張志國(guó) 馬 英 耿光有,等 1∶9

制導(dǎo)炮彈可控滾轉(zhuǎn)執(zhí)行機(jī)構(gòu)模型分析

劉源翔 崔 巖 李 睿,等 1∶17

飛行器航跡測(cè)量數(shù)據(jù)的粗差探測(cè)模型優(yōu)選方法

涂先勤 谷德峰 易東云,等 1∶22

基于改進(jìn)混雜擴(kuò)展卡爾曼濾波的炮彈阻力系數(shù)辨識(shí)

楊 靖 常思江 王中原 1∶28

某鴨式布局彈箭的俯仰動(dòng)導(dǎo)數(shù)計(jì)算與分析

鄧 維 陳少松 1∶34

拋索火箭系統(tǒng)主動(dòng)段繩索動(dòng)力學(xué)特性研究

陸 鳴 顧文彬 涂善超,等 1∶39

水下航行體表面凹槽數(shù)對(duì)超空泡流場(chǎng)影響的數(shù)值模擬

施紅輝 孫亞亞 周楊潔,等 1∶44

高速射彈出水過(guò)程中水彈道問(wèn)題研究

侯 健 施紅輝 孫亞亞,等 1∶51

基于藥料膨脹和流動(dòng)均勻性的單孔藥模具設(shè)計(jì)

呂勝濤 季丹丹 廖 昕,等 1∶57

超聲速和高超聲速燃燒的數(shù)值研究

李恩義 樂(lè)貴高 馬大為,等 1∶62

大長(zhǎng)徑比中心炸管式拋撒定容階段兩相流模擬

郭夢(mèng)婷 陶如意 李子杰 1∶68

TC復(fù)合彈對(duì)多層A3鋼靶穿甲效應(yīng)的試驗(yàn)與仿真

胡迪奇 王堅(jiān)茹 陳智剛,等 1∶73

周向約束對(duì)桿式射流成型規(guī)律的仿真研究

王維占 趙太勇 陳智剛,等 1∶79

細(xì)晶銅材料力學(xué)性能及藥型罩領(lǐng)域應(yīng)用研究

閆 超 黃正祥 祖旭東,等 1∶85

基于自適應(yīng)回歸算法的導(dǎo)彈表面溫度預(yù)測(cè)

劉姝含 朱戰(zhàn)霞 1∶93

2017年第2期(總第112期)

多UCAV超視距協(xié)同空戰(zhàn)中的交接制導(dǎo)方法

周德云 楊 振 張 堃 2∶1

基于UKF彈體滾轉(zhuǎn)姿態(tài)測(cè)量方法研究

袁丹丹 易文俊 管 軍,等 2∶8

約束混凝土靶的準(zhǔn)靜態(tài)柱形空腔膨脹理論

詹昊雯 曹揚(yáng)悅也 蔣志剛,等 2∶13

考慮侵蝕效應(yīng)的卵形彈丸侵徹混凝土介質(zhì)模型研究

劉志林 王曉鳴 李文彬,等 2∶19

離散元模擬鋼筋混凝土靶板貫穿響應(yīng)研究

馮 君 孫巍巍 張武滿(mǎn),等 2∶26

新型雙層反應(yīng)裝甲金屬板運(yùn)動(dòng)分析與研究

侯 輝 姚文進(jìn) 李文彬,等 2∶34

基于二維分岔的超空泡航行體非線(xiàn)性動(dòng)力學(xué)特性分析

呂一品 熊天紅 易文俊,等 2∶39

細(xì)長(zhǎng)體射彈高速水平入水研究

王瑞琦 黃振貴 郭則慶,等 2∶47

可燃藥筒材料高壓燃燒性能的測(cè)量與計(jì)算

劉 靜 余永剛 嚴(yán)小林 2∶54

單組元粉末發(fā)動(dòng)機(jī)內(nèi)流場(chǎng)數(shù)值模擬研究

冷林濤 翁春生 白橋棟,等 2∶58

基于VOF模型的凝膠推進(jìn)劑的偽流動(dòng)研究

曹欽柳 封 鋒 鄧寒玉 2∶65

首發(fā)浮動(dòng)的高初速榴彈機(jī)槍發(fā)射性能研究

宋 杰 邱 明 廖振強(qiáng),等 2∶70

火炮后坐阻力的區(qū)間不確定性?xún)?yōu)化研究

李 榮 楊國(guó)來(lái) 孫全兆,等 2∶78

基于聲學(xué)傳感網(wǎng)絡(luò)的彈著點(diǎn)定位系統(tǒng)

劉德耀 陳志菲 郭心偉,等 2∶85

分階段對(duì)地打擊武器-目標(biāo)分配建模與決策

楊奇松 王順宏 王然輝,等 2∶90

2017年第3期(總第113期)

推力調(diào)節(jié)飛行距離最優(yōu)自適應(yīng)滑?？刂?/p>

劉家祺 謝曉方 王誠(chéng)成,等 3∶1

遠(yuǎn)程彈道式飛行器機(jī)動(dòng)制導(dǎo)方法

王 濤 張洪波 王 征,等 3∶7

比例導(dǎo)引法中剩余飛行時(shí)間的計(jì)算方法

陳升富 常思江 3∶14

基于終端滑模面的導(dǎo)彈滑?？刂破髟O(shè)計(jì)

華思雨 王旭剛 3∶20

THAAD攔截彈螺旋彈道仿真分析

何陽(yáng)光 李小兵 陳 峰,等 3∶27

翼形參數(shù)對(duì)某彈道修正迫彈氣動(dòng)特性的影響

沈皓敏 楊新民 3∶32

磁阻傳感器的地磁信號(hào)干擾研究和修正

張俊生 馮 波 王志興,等 3∶38

分布式雷達(dá)對(duì)非合作目標(biāo)彈道測(cè)量精度分析

宮志華 劉 洋 陳春江 3∶43

多點(diǎn)起爆方式對(duì)EFP侵徹能力增益的研究

沈慧銘 李偉兵 王曉鳴,等 3∶49

大質(zhì)量鎢破片沖擊多層間隙蓋板炸藥數(shù)值模擬與試驗(yàn)研究

梁 斌 馮高鵬 周婕群,等 3∶56

PELE侵徹10 mm厚均質(zhì)裝甲鋼的極限穿透速度和后效研究

何 俊 程 春 鄭紹君,等 3∶63

液體發(fā)射藥迫擊炮內(nèi)彈道建模及性能分析

陸 林 劉 寧 張相炎 3∶68

旋轉(zhuǎn)爆震發(fā)動(dòng)機(jī)工作特性試驗(yàn)研究

徐 燦 馬 虎 嚴(yán) 宇,等 3∶74

流量可調(diào)燃?xì)獍l(fā)生器壓強(qiáng)控制仿真

余業(yè)輝 陳 雄 鄭 健,等 3∶82

不同優(yōu)化算法在輪式自行火炮動(dòng)力學(xué)優(yōu)化中的應(yīng)用

曹巖楓 牛福強(qiáng) 洪亞軍,等 3∶87

一種單兵電磁武器發(fā)射過(guò)程仿真研究

徐 麟 張 軍 董健年 3∶92

2017年第4期(總第114期)

一種同時(shí)具有攻擊時(shí)間和攻擊角度約束的協(xié)同制導(dǎo)律

王曉芳 王紫揚(yáng) 林 海 4∶1

飛行器可達(dá)性問(wèn)題的統(tǒng)一求解方法研究

喬 浩 李曾浩 李新國(guó),等 4∶9

一種基于速度方向修正的旋轉(zhuǎn)穩(wěn)定彈彈道跟蹤制導(dǎo)方法研究

鐘揚(yáng)威 王良明 張立研,等 4∶15

基于迭代凸優(yōu)化的導(dǎo)彈探測(cè)時(shí)間估算方法

葛瑞星 周青松 張劍云,等 4∶22

SR-CDKF在組合導(dǎo)航直接法濾波中的應(yīng)用

逯 嶠 馬國(guó)梁 張 平,等 4∶29

基于零效脫靶量的制導(dǎo)估計(jì)一體化方法

李 炯 張 濤 張金鵬,等 4∶35

低速旋轉(zhuǎn)尾翼式彈箭氣動(dòng)特性數(shù)值研究

張 超 王學(xué)德 王 勇,等 4∶40

輕武器榴彈射擊密集度試驗(yàn)方法研究

蒲利森 徐酉亮 4∶48

破片式戰(zhàn)斗部對(duì)飛機(jī)類(lèi)目標(biāo)毀傷評(píng)估方法研究

司 凱 李向東 郭 超,等 4∶52

蜂窩鋁沖擊波形數(shù)值計(jì)算及分析

曹 杰 葛建立 王 浩,等 4∶58

正六邊形鋼管約束混凝土靶抗侵徹性能的數(shù)值模擬

蒙朝美 蔣志剛 蔡良才,等 4∶64

低侵徹陶瓷槍彈對(duì)航空有機(jī)玻璃的侵徹性能分析

李 波 王堅(jiān)茹 印立魁,等 4∶70

柔性噴管SRM三維兩相內(nèi)流場(chǎng)數(shù)值模擬

張 俊 田中旭 許 哲,等 4∶76

利用火焰彎曲理論預(yù)測(cè)復(fù)合推進(jìn)劑侵蝕函數(shù)的方法與應(yīng)用

陳 軍 4∶81

膛口制退器與緩沖器匹配對(duì)后坐力的影響

肖俊波 楊國(guó)來(lái) 李洪強(qiáng),等 4∶86

炮彈彈質(zhì)量分級(jí)現(xiàn)行標(biāo)準(zhǔn)對(duì)戰(zhàn)術(shù)使用影響分析

郭尚生 邢存震 黃福鋒,等 4∶93

JournalofBallistics

Vol. 29

Total Contents

No.1(2017),SumNo.111

Predictive Control Based on Characteristic Model for Reentry Hypersonic Vehicle With Multiple Constraints

ZHANGJun,LIYa-hui,ZHUSheng-zhen1∶1

Convex Optimization Method Used in the Landing-phase On-line Guidance of Rocket Vertical Recovery

ZHANGZhi-guo,MAYing,GENGGuang-you,etal1∶9

Modeling and Analysis of Controllable-rolling Actuactor System

LIUYuan-xiang,CUIYan,LIRui,etal1∶17

Method of Optimally Choosing Gross-error Detection Model

TUXian-qin,GUDe-feng,YIDong-yun,etal1∶22

Drag Coefficient Estimation for Projectiles Based on Improved Hybrid Extended Kalman Filter

YANGJing,CHANGSi-jiang,WANGZhong-yuan1∶28

Predictions and Analysis for Pitching Dynamic-derivatives of a Canard-configuration Missile

DENGWei,CHENShao-song1∶34

Dynamic Simulation of the Rope in Boost Phase of Throwing-line Rocket

LUMing,GUWen-bin,TUShan-chao,etal1∶39

Numerical Study of the Supercavitation Flow-field Around Underwater Vehicle With Different Surface-grooves

SHIHong-hui,SUNYa-ya,ZHOUYang-jie,etal1∶44

Study on the Trajectory of High-speed Projectile Exiting From Water

HOUJian,SHIHong-hui,SUNYa-ya,etal1∶51

Design on Die of One-hole Propellant Based on Its Expansion and Flow Uniformity

LVSheng-tao,JIDan-dan,LIAOXin,etal1∶57

Numerical Investigation of Supersonic and Hypersonic Combustion

LIEn-yi,LEGui-gao,MADa-wei,etal1∶62

Simulation of Two-phase Flow in the Constant Volume of Dispersal System Using Centralizing Blast-tube With Large

Length-Diameter Ratio

GUOMeng-ting,TAORu-yi,LIZi-jie1∶68

Simulation and Experimental Investigation on Armor-piecing Performance of TC Composite Projectile to Multilayer A3 Steel

Plates Targets

HUDi-qi,WANGJian-ru,CHENZhi-gang,etal1∶73

Effect of Circumferential Constraint on the Formation of Rod-type Jet

WANGWei-zhan,ZHAOTai-yong,CHENZhi-gang,etal1∶79

Mechanical Property of Ultra-fine Grained Copper Material and Study on Application of Liner Field

YANChao,HUANGZheng-xiang,ZUXu-dong,etal1∶85

Prediction on Surface Temperature of Missile Based on Adaptive Regression Algorithm

LIUShu-han,ZHUZhan-xia1∶93

No.2(2017),SumNo.112

Method of Guidance Handover in Beyond-visual-range Coordinated Air-combat for Multi-UCAVs

ZHOUDe-yun,YANGZhen,ZHANGKun2∶1

Study of Projectile Roll-attitude Measurement Method Based on Unscented Kalman Filter

YUANDan-dan,YIWen-jun,GUANJun,etal2∶8

Quasi-static Cylindrical Cavity-expansion Model for Confined-concrete Targets

ZHANHao-wen,CAOYang-yue-ye,JIANGZhi-gang,etal2∶13

Model of Ogive-nose Projectile Penetrating Concrete Target Considering Effect of Mass Loss and Nose Blunting

LIUZhi-lin,WANGXiao-ming,LIWen-bin,etal2∶19

Study on Perforation Responses of Reinforced Concrete Slab by Discrete Modeling

FENGJun,SUNWei-wei,ZHANGWu-man,etal2∶26

Analysis and Study on Plates Movement of New Double-layer Explosive Reactive Armor

HOUHui,YAOWen-jin,LIWen-bin,etal2∶34

Nonlinear Dynamic Characteristics of Supercavitating Vehicle Based on Two-dimensional Bifurcation

LVYi-pin,XIONGTian-hong,YIWen-jun,etal2∶39

Study on Horizontal Water-entry of Slender Projectile With High-speed

WANGRui-qi,HUANGZhen-gui,GUOZe-qing,etal2∶47

Measurement and Calculation of Combustion Performance of Combustible Cartridge Under High Pressure

LIUJing,YUYong-gang,YANXiao-lin2∶54

Numerical Simulation on Internal Flow-field of Monopropellant Powder Engine

LENGLin-tao,WENGChun-sheng,BAIQiao-dong,etal2∶58

Research on Spurious Currents of Gel Propellant Based on VOF Model

CAOQin-liu,FENGFeng,DENGHan-yu2∶65

Research on Launching Performance of GMG With High Muzzle-velocity Based on First-floating Technology

SONGJie,QIUMing,LIAOZhen-qiang,etal2∶70

Optimization on Interval Uncertainty of Artillery Recoil Resistance

LIRong,YANGGuo-lai,SUNQuan-zhao,etal2∶78

Measurement System for Projectile Impact-points Based on Acoustic Sensor Network

LIUDe-yao,CHENZhi-fei,GUOXin-wei,etal2∶85

Modeling and Decision-making of Ground Attack Weapon-Target Assignment

YANGQi-song,WANGShun-hong,WANGRan-hui,etal2∶90

No.3(2017),SumNo.113

Optimal Adaptive Sliding Mode Control of Flight Distance on Thrust Regulation

LIUJia-qi,XIEXiao-fang,WANGCheng-cheng,etal3∶1

Maneuver Strategy and Guidance Law of Large-range Ballistic Vehicle

WANGTao,ZHANGHong-bo,WANGZheng,etal3∶7

Study on Time-to-go Algorithm in Proportional Navigation Guidance

CHENSheng-fu,CHANGSi-jiang3∶14

Design on Sliding Mode Controller of Missile Based on Terminal Sliding Mode Surface

HUASi-yu,WANGXu-gang3∶20

Simulation and Analysis on Spiral Trajectory of THAAD Interceptor

HEYang-guang,LIXiao-bing,CHENFeng,etal3∶27

Effect of Airfoil Parameters on Aerodynamic Characteristics of Trajectory-correction Mortar Projectile

SHENHao-min,YANGXin-min3∶32

Research and Correction of Geomagnetic Signal Interference in Magnetoresistive Sensor

ZHANGJun-sheng,FENGBo,WANGZhi-xing,etal3∶38

Analysis on Precision of Distributed Radar Measuring Non-cooperative Target Trajectory

GONGZhi-hua,LIUYang,CHENChun-jiang3∶43

Study on the Penetration Ability of EFP by Annular Multi-point Initiation

SHENHui-ming,LIWei-bing,WANGXiao-ming,etal3∶49

Numerical Simulation and Experimental Study on the Explosive With Multi-layer Interval Targets Impacted

by Large-mass Tungsten Fragments

LIANGBin,FENGGao-peng,ZHOUJie-qun,etal3∶56

Critical Penetration Velocity and Aftereffect of PELE Penetrating RHA With 10 mm Thickness

HEJun,CHENGChun,ZHENGShao-jun,etal3∶63

Modeling and Performance Analysis for Ballistics of Mortar With Liquid Propellant

LULin,LIUNing,ZHANGXiang-yan3∶68

Experimental Study on Operating Characteristics of Rotating Detonation Engine

XUCan,MAHu,YANYu,etal3∶74

Simulation on Pressure Control of Adjustable-flow Gas Generator

YUYe-hui,CHENXiong,ZHENGJian,etal3∶82

Study on Different Optimization Algorithms for Optimization Design of Wheeled Self-propelled Gun Firing Dynamics

CAOYan-feng,NIUFu-qiang,HONGYa-jun,etal3∶87

Simulation on Launching Process of Individual Electromagnetic Weapon

XULin,ZHANGJun,DONGJian-nian3∶92

No.4(2017),SumNo.114

A Cooperative Guidance Law With Constraints of Impact Time and Impact Angle

WANGXiao-fang,WANGZi-yang,LINHai4∶1

A Unified Numerical Method for Aircraft Accessibility Problems

QIAOHao,LIZeng-hao,LIXin-guo,etal4∶9

Study on Trajectory Tracking Guidance Method for Spin Stabilized Projectile Based on Velocity Direction Correction

ZHONGYang-wei,WANGLiang-ming,ZHANGLi-yan,etal4∶15

Estimation Method of Missile Detection Time-window Based on Iterative Convex Optimization

GERui-xing,ZHOUQing-song,ZHANGJian-yun,etal4∶22

Application of SR-CDKF in Direct Filtering of Integrated Navigation

LUQiao,MAGuo-liang,ZHANGPing,etal4∶29

Unitization Method of Guidance and Estimation Based on Zero-Effort-Miss

LIJiong,ZHANGTao,ZHANGJin-peng,etal4∶35

Research on Aerodynamic Characteristics of Missile With Fins Under Low-speed Rotation

ZHANGChao,WANGXue-de,WANGYong,etal4∶40

Research on Test Method of Fire Concentration of Small Arms Grenade

PULi-sen,XUYou-liang4∶48

Research on Damage Assessment Method of Fragmentation Warhead Against Airplane Targets

SIKai,LIXiang-dong,GUOChao,etal4∶52

Numerical Simulation on Shock Waveform of Aluminum Honeycombs

CAOJie,GEJian-li,WANGHao,etal4∶58

Numerical Simulation of Anti-penetration Performance for Hexagonal Steel-tube-confined Concrete Target

MENGChao-mei,JIANGZhi-gang,CAILiang-cai,etal4∶64

Performance of Low-penetration Ceramic Bullet Penetrating Aviation Organic Glass

LIBo,WANGJian-ru,YINLi-kui,etal4∶70

Simulation on 3D Two-phase Inner Flow Field for Flexible-nozzle SRM

ZHANGJun,TIANZhong-xu,XUZhe,etal4∶76

Approach and Application of Predicting Erosive Ratio of Composite Propellant Based on Flame Bending Theory

CHENJun4∶81

Influences of Matching Muzzle Brake and Buffer on Weapon Recoil

XIAOJun-bo,YANGGuo-lai,LIHong-qiang,etal4∶86

Analysis of the Influence of Standard Mass Classification for Projectile on Tactical Operation

GUOShang-sheng,XINGCun-zhen,HUANGFu-feng,etal4∶93