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弹道学报第29卷总目次

2017-12-19

弹道学报 2017年4期
关键词:弹道制导数值

弹道学报第29卷总目次

2017年第1期(总第111期)

基于特征模型的高超声速飞行器再入多约束预测控制

张 军 李亚辉 朱晟桢 1∶1

火箭垂直回收着陆段在线制导凸优化方法

张志国 马 英 耿光有,等 1∶9

制导炮弹可控滚转执行机构模型分析

刘源翔 崔 岩 李 睿,等 1∶17

飞行器航迹测量数据的粗差探测模型优选方法

涂先勤 谷德峰 易东云,等 1∶22

基于改进混杂扩展卡尔曼滤波的炮弹阻力系数辨识

杨 靖 常思江 王中原 1∶28

某鸭式布局弹箭的俯仰动导数计算与分析

邓 维 陈少松 1∶34

抛索火箭系统主动段绳索动力学特性研究

陆 鸣 顾文彬 涂善超,等 1∶39

水下航行体表面凹槽数对超空泡流场影响的数值模拟

施红辉 孙亚亚 周杨洁,等 1∶44

高速射弹出水过程中水弹道问题研究

侯 健 施红辉 孙亚亚,等 1∶51

基于药料膨胀和流动均匀性的单孔药模具设计

吕胜涛 季丹丹 廖 昕,等 1∶57

超声速和高超声速燃烧的数值研究

李恩义 乐贵高 马大为,等 1∶62

大长径比中心炸管式抛撒定容阶段两相流模拟

郭梦婷 陶如意 李子杰 1∶68

TC复合弹对多层A3钢靶穿甲效应的试验与仿真

胡迪奇 王坚茹 陈智刚,等 1∶73

周向约束对杆式射流成型规律的仿真研究

王维占 赵太勇 陈智刚,等 1∶79

细晶铜材料力学性能及药型罩领域应用研究

闫 超 黄正祥 祖旭东,等 1∶85

基于自适应回归算法的导弹表面温度预测

刘姝含 朱战霞 1∶93

2017年第2期(总第112期)

多UCAV超视距协同空战中的交接制导方法

周德云 杨 振 张 堃 2∶1

基于UKF弹体滚转姿态测量方法研究

袁丹丹 易文俊 管 军,等 2∶8

约束混凝土靶的准静态柱形空腔膨胀理论

詹昊雯 曹扬悦也 蒋志刚,等 2∶13

考虑侵蚀效应的卵形弹丸侵彻混凝土介质模型研究

刘志林 王晓鸣 李文彬,等 2∶19

离散元模拟钢筋混凝土靶板贯穿响应研究

冯 君 孙巍巍 张武满,等 2∶26

新型双层反应装甲金属板运动分析与研究

侯 辉 姚文进 李文彬,等 2∶34

基于二维分岔的超空泡航行体非线性动力学特性分析

吕一品 熊天红 易文俊,等 2∶39

细长体射弹高速水平入水研究

王瑞琦 黄振贵 郭则庆,等 2∶47

可燃药筒材料高压燃烧性能的测量与计算

刘 静 余永刚 严小林 2∶54

单组元粉末发动机内流场数值模拟研究

冷林涛 翁春生 白桥栋,等 2∶58

基于VOF模型的凝胶推进剂的伪流动研究

曹钦柳 封 锋 邓寒玉 2∶65

首发浮动的高初速榴弹机枪发射性能研究

宋 杰 邱 明 廖振强,等 2∶70

火炮后坐阻力的区间不确定性优化研究

李 荣 杨国来 孙全兆,等 2∶78

基于声学传感网络的弹着点定位系统

刘德耀 陈志菲 郭心伟,等 2∶85

分阶段对地打击武器-目标分配建模与决策

杨奇松 王顺宏 王然辉,等 2∶90

2017年第3期(总第113期)

推力调节飞行距离最优自适应滑模控制

刘家祺 谢晓方 王诚成,等 3∶1

远程弹道式飞行器机动制导方法

王 涛 张洪波 王 征,等 3∶7

比例导引法中剩余飞行时间的计算方法

陈升富 常思江 3∶14

基于终端滑模面的导弹滑模控制器设计

华思雨 王旭刚 3∶20

THAAD拦截弹螺旋弹道仿真分析

何阳光 李小兵 陈 峰,等 3∶27

翼形参数对某弹道修正迫弹气动特性的影响

沈皓敏 杨新民 3∶32

磁阻传感器的地磁信号干扰研究和修正

张俊生 冯 波 王志兴,等 3∶38

分布式雷达对非合作目标弹道测量精度分析

宫志华 刘 洋 陈春江 3∶43

多点起爆方式对EFP侵彻能力增益的研究

沈慧铭 李伟兵 王晓鸣,等 3∶49

大质量钨破片冲击多层间隙盖板炸药数值模拟与试验研究

梁 斌 冯高鹏 周婕群,等 3∶56

PELE侵彻10 mm厚均质装甲钢的极限穿透速度和后效研究

何 俊 程 春 郑绍君,等 3∶63

液体发射药迫击炮内弹道建模及性能分析

陆 林 刘 宁 张相炎 3∶68

旋转爆震发动机工作特性试验研究

徐 灿 马 虎 严 宇,等 3∶74

流量可调燃气发生器压强控制仿真

余业辉 陈 雄 郑 健,等 3∶82

不同优化算法在轮式自行火炮动力学优化中的应用

曹岩枫 牛福强 洪亚军,等 3∶87

一种单兵电磁武器发射过程仿真研究

徐 麟 张 军 董健年 3∶92

2017年第4期(总第114期)

一种同时具有攻击时间和攻击角度约束的协同制导律

王晓芳 王紫扬 林 海 4∶1

飞行器可达性问题的统一求解方法研究

乔 浩 李曾浩 李新国,等 4∶9

一种基于速度方向修正的旋转稳定弹弹道跟踪制导方法研究

钟扬威 王良明 张立研,等 4∶15

基于迭代凸优化的导弹探测时间估算方法

葛瑞星 周青松 张剑云,等 4∶22

SR-CDKF在组合导航直接法滤波中的应用

逯 峤 马国梁 张 平,等 4∶29

基于零效脱靶量的制导估计一体化方法

李 炯 张 涛 张金鹏,等 4∶35

低速旋转尾翼式弹箭气动特性数值研究

张 超 王学德 王 勇,等 4∶40

轻武器榴弹射击密集度试验方法研究

蒲利森 徐酉亮 4∶48

破片式战斗部对飞机类目标毁伤评估方法研究

司 凯 李向东 郭 超,等 4∶52

蜂窝铝冲击波形数值计算及分析

曹 杰 葛建立 王 浩,等 4∶58

正六边形钢管约束混凝土靶抗侵彻性能的数值模拟

蒙朝美 蒋志刚 蔡良才,等 4∶64

低侵彻陶瓷枪弹对航空有机玻璃的侵彻性能分析

李 波 王坚茹 印立魁,等 4∶70

柔性喷管SRM三维两相内流场数值模拟

张 俊 田中旭 许 哲,等 4∶76

利用火焰弯曲理论预测复合推进剂侵蚀函数的方法与应用

陈 军 4∶81

膛口制退器与缓冲器匹配对后坐力的影响

肖俊波 杨国来 李洪强,等 4∶86

炮弹弹质量分级现行标准对战术使用影响分析

郭尚生 邢存震 黄福锋,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

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