子母弹打击机场跑道散布规律与毁伤效果研究
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摘要
在现代战争远距离精确打击的背景下,提高武器精度和弹药能量的利用率成为武器发展的两大趋势。在这种背景和趋势下,子母弹应运而生,它是提高常规战斗部有效利用率和毁伤效果的重要途径,是未来高技术局部战争中必不可少的一种作战武器。子弹落点散布是火力运用的基础,本文主要内容是研究子母弹的散布特性,为子母弹设计和火力运用提供辅助决策信息,以提高武器作战效能。
以分析子弹落点散布特性为目的,本文展开了一系列研究工作。首先,针对子弹为刚性尾翼无控子弹、采用侧向抛撒方式的子母弹,建立了在发射坐标系下的子母弹飞行动力学模型,给出了一种求解同射程条件下具有不同特性弹道的方法,并计算了三条具有不同特性的母弹弹道,为子弹落点散布分析提供了基础;针对散布形状为椭圆环的情况,提出了完整的散布特性参数,给出了散布特征范围的具体计算方法及均匀性评定方法,为子弹落点散布分析提供了依据。然后,利用标准弹道仿真产生子弹落点的方法对单层子弹落点散布进行了分析,利用基于侧向抛撒方式的子弹落点抽样方法对子弹落点散布均匀性进行了分析。最后,介绍了一种稳健设计方法――Taguchi方法,并针对跑道目标,利用该方法对影响毁伤效果指标的因素进行参数优化与分析,得到了有益的结论。
论文对子弹落点散布特性进行了比较全面深入的研究,论文所做工作对于提高子母弹的作战效能具有很好的参考价值和应用价值。
On the background of long distance precious attack in the modern war today, it has become two directions for development of weapon that improving precision and making better use of ammo energy. Cluster warhead emerges as the times require. Using cluster warhead is an important way to make good use of general combat warhead and improve destroy efficiency, so it is the absolutely necessary combat weapon in the future high technology local war. As cluster warhead submunition dispersion is the basis of using weapon, the main content of this paper is to study the distribute characteristic of cluster warhead, and it can provide some assistant information for designing and using cluster warhead to improve fighting efficiency.
This paper carries out a series of work aiming at analyzing the distribute characteristic of cluster warhead impact point. It first establishes a flight dynamic model of cluster warhead in the launch coordinate system, develops a method of calculating different characteristic ballistic trajectory which has the same shot distance, and calculates three different characteristic ballistic trajectories, which provides the basis of analyzing the distribute characteristic of cluster warhead impact point; presents a group of dispersion parameter when the shape of submunition dispersion is a elliptic circle, develops a evaluation method of calculating dispersion range and submunition uniformity for cluster warhead submunition, which provides the basis of analyzing the distribute characteristic of cluster warhead impact point. Then, this paper analyzes the dispersion characteristic of a single layer of submunition by the ballistic simulating calculation, and analyzes the submunition uniformity by using sample method to produce impact point of submunition. Last, this paper introduces a kind of robust design method—Taguchi method, by which to optimize and analyze the parameter which affect the destroy efficiency to airport runway, and gets some helpful conclusion.
This paper makes a relatively deeply study of cluster warhead submunition dispersion, and has a good reference and upper application value to improve the fighting efficiency.
以分析子弹落点散布特性为目的,本文展开了一系列研究工作。首先,针对子弹为刚性尾翼无控子弹、采用侧向抛撒方式的子母弹,建立了在发射坐标系下的子母弹飞行动力学模型,给出了一种求解同射程条件下具有不同特性弹道的方法,并计算了三条具有不同特性的母弹弹道,为子弹落点散布分析提供了基础;针对散布形状为椭圆环的情况,提出了完整的散布特性参数,给出了散布特征范围的具体计算方法及均匀性评定方法,为子弹落点散布分析提供了依据。然后,利用标准弹道仿真产生子弹落点的方法对单层子弹落点散布进行了分析,利用基于侧向抛撒方式的子弹落点抽样方法对子弹落点散布均匀性进行了分析。最后,介绍了一种稳健设计方法――Taguchi方法,并针对跑道目标,利用该方法对影响毁伤效果指标的因素进行参数优化与分析,得到了有益的结论。
论文对子弹落点散布特性进行了比较全面深入的研究,论文所做工作对于提高子母弹的作战效能具有很好的参考价值和应用价值。
On the background of long distance precious attack in the modern war today, it has become two directions for development of weapon that improving precision and making better use of ammo energy. Cluster warhead emerges as the times require. Using cluster warhead is an important way to make good use of general combat warhead and improve destroy efficiency, so it is the absolutely necessary combat weapon in the future high technology local war. As cluster warhead submunition dispersion is the basis of using weapon, the main content of this paper is to study the distribute characteristic of cluster warhead, and it can provide some assistant information for designing and using cluster warhead to improve fighting efficiency.
This paper carries out a series of work aiming at analyzing the distribute characteristic of cluster warhead impact point. It first establishes a flight dynamic model of cluster warhead in the launch coordinate system, develops a method of calculating different characteristic ballistic trajectory which has the same shot distance, and calculates three different characteristic ballistic trajectories, which provides the basis of analyzing the distribute characteristic of cluster warhead impact point; presents a group of dispersion parameter when the shape of submunition dispersion is a elliptic circle, develops a evaluation method of calculating dispersion range and submunition uniformity for cluster warhead submunition, which provides the basis of analyzing the distribute characteristic of cluster warhead impact point. Then, this paper analyzes the dispersion characteristic of a single layer of submunition by the ballistic simulating calculation, and analyzes the submunition uniformity by using sample method to produce impact point of submunition. Last, this paper introduces a kind of robust design method—Taguchi method, by which to optimize and analyze the parameter which affect the destroy efficiency to airport runway, and gets some helpful conclusion.
This paper makes a relatively deeply study of cluster warhead submunition dispersion, and has a good reference and upper application value to improve the fighting efficiency.
引文
1王荣,陆子辉.子母弹研究进展.国防科技大学学报, 2006, 18(8): 60~64
2 SACKS J, WELCH W J, MITCHELL T J, et al. Design and analysis of computer experiments [J]. Statistical Science, 2003, (4): 409~435
3 R.Sedney.“A model for bomblet ejection from missiles”. AD/A- 054641, Journal of Spaccraft and Rocket, 1998, (5): 7~8
4田口玄一.开发、设计阶段的质量工程学.兵器工业出版社, 1990: 67~79
5徐文旭,唐雪梅.子弹子弹抛撒弹道模型及数字仿真.宇航学报, 2001, 22(2): 71~78
6王家兵.子母弹落点散布研究.测控技术, 2002: 34~35
7林靖明.母弹激波对子弹气动特性及飞行姿态影响的研究.中国运载火箭技术研究院. 1998: 78~89
8陈冰,易东云,谢美华.地地战术子母弹抛射与散布建模仿真.飞行器测控学报, 2006, 25(4): 40~44
9张明宏,陈建新.提高子母弹子弹综合毁伤效能的方法.测控技术, 2005, 24(4): 55~57
10 BATES D M, WATTS D G. Nonlinear regression analysis and its applications [M]. New York: Inc John Wiley & Sons, 2005: 134~144
11 Edge HL, Jubaraj Sahu,Heavey KR.Computational Fluid Dynamics Modeling of Submuniti on Separation from Missile.American Institute of Aeronautics & Astronautics, 1999: 215~225
12蔡星会,王小龙,孙新利.子母弹内弹道理论计算模型.上海航天, 2000, (6): 5~8
13 Hadar O, Rotman SR,Kopeika NS.Thermal image target acquisition probabilities in the presence of vibrations[J]. In-frared Phys Technol., 1999, 36(3): 691~702
14吴雪松.远程子母弹囊式抛撒结构设计及计算机仿真技术.南京理工大学硕士学位论文,2001:67-69
15雷娟棉,吴甲生,肖雅彬.布撒器-子弹气动干扰风洞实验研究.兵工学报, 2005, 26(4): 535~538
16 Thomas PD Middleeoff JF. Directeontrol of theghd Point distribution inmeshes generated byelli Ptieequations.AIAA Joumal, Vol.18, 2004: 652~656
17赵子才.再入弹头动力学分析与理论研究.火力与指挥控制, 2001: 68~70
18 Norman,M, Wereley Feasibility Study of a Smart Submunition Deployment from a Conventional Weapon.Army Research Laboratory, 2001: 156~158
19徐望.子弹弹道测量方法的研究.国防科技大学学报, 2000: 45~47
20杜之明.发射试验结果分析与鉴定技术.国防工业出版社, 2006: 36~39
21唐雪梅,徐文旭.子母弹抛撒的均匀性指标的确定及评定方法.系统工程与电子技术, 1999, 21(1): 11~14
22 Lo5H.Anew Mesh Generation Scheme For Jbitrary Planar Domains. Intemational Joumal For Numerical Methods In Engineering, Vol.ZI, 2002: 1403~1426
23雷宁利,唐雪梅.侵彻子母弹对机场跑道的封锁概率计算研究.系统仿真学报, 2004, 16(9): 2030~2032
24 Harris, L, Edge Computational Fluid Dynamics Modeling of Submunition Separation from Missile.Army Research Laboratory,1999: 134~136
25 Baker TJ. Three dimension nalmesh generate on by triangulation of arbitrary Pointset. AIAAPaPer, 2006: 87~112
26舒建生,王运吉,朱昱.子母弹抛撒半径对机场毁伤效果影响分析.火力与指挥控制, 2001, (3): 49~50
27 G., Denian Anti -Torpedo Combat System for Surface Ships. UDT, 1993: 23~26
28王纳,万国龙.常规战术子母弹封锁机场跑道效率研究.战术子母弹技术, 2003, 5(3): 1~4
29宋光明.子母弹打击机场跑道的计算机模拟.火力与指挥控制, 2001, 26(4): 67~69
30 Louis, J, Rodrigues Brilliant Antiarmor Submunition Opportunity Exists to Conduct Critical Test Prior to Production Decision. 1997: 87~90
31陈立周.稳健设计.机械工业出版社, 2000: 135~140
32张明宏,陈建新.提高子母弹子弹综合毁伤效能方法探讨[J].理论与探索, 2004, (5): 19~20
33 Wu Jeff, C.F., Michael Hamada著,张润楚等译.试验理论与分析及参数优化.中国统计出版社, 2003: 78~87
34 CorderD A,EstB E. Prediction of Submunition Dispense Aerodynamics[C]. 33rd Aerospace Sciences Meeting and Exhibit, Reno, NV, 1995: 193~199
35 David, K, steensma Acquisition of the Wide Area Munition.Audit Report. 2001: 342~345
36 PERKINA S C Jr, DILLENIUS MF E and SIN J L. Supersonic submunition aerodynamics during dispense[R]. AIAA Paper 88-0335: 212~216
37杨启仁.尾翼稳定脱壳穿甲弹总体基本参数设计.华东工学院, 2005: 90~95
38彭程远.稳健设计方法及其在飞行器设计中的应用研究.西北工业大学硕士学位论文, 2004: 56~58
39 DavidA. Field.LaPlacian Smoothing Ad Delaunay Tria ngulations. Communi- eations In APPlied Numerical Methods. Vol. 4, 2003: 709~712
40 XIE M Y, FANG K T. Admissibility and minimaxity of the u-niform design measure in nonparametric regression model [J]. Journal of Statistical Planning and Inference, 2003, 83: 101~111
41 A. M. Law, W. D. Kelton. Simulation Modeling and Analysis (Third Edition).清华大学出版社, 2000: 178~180
42 SANTNER T J, WILLIAMS B J, NOTZ W I. The design and analysis of computer experiments [M]. New York:Springer, 2003: 123~134
43陈入领.稳健设计进程策略的研究及实践.浙江大学硕士学位论文, 2003: 35~37
44 Jubaraj, sahu Computational Modeling of Sense and Destroy Armor (SADARM) Submunition Separation Collision.Army Research Laboratory, 1997: 29~32
2 SACKS J, WELCH W J, MITCHELL T J, et al. Design and analysis of computer experiments [J]. Statistical Science, 2003, (4): 409~435
3 R.Sedney.“A model for bomblet ejection from missiles”. AD/A- 054641, Journal of Spaccraft and Rocket, 1998, (5): 7~8
4田口玄一.开发、设计阶段的质量工程学.兵器工业出版社, 1990: 67~79
5徐文旭,唐雪梅.子弹子弹抛撒弹道模型及数字仿真.宇航学报, 2001, 22(2): 71~78
6王家兵.子母弹落点散布研究.测控技术, 2002: 34~35
7林靖明.母弹激波对子弹气动特性及飞行姿态影响的研究.中国运载火箭技术研究院. 1998: 78~89
8陈冰,易东云,谢美华.地地战术子母弹抛射与散布建模仿真.飞行器测控学报, 2006, 25(4): 40~44
9张明宏,陈建新.提高子母弹子弹综合毁伤效能的方法.测控技术, 2005, 24(4): 55~57
10 BATES D M, WATTS D G. Nonlinear regression analysis and its applications [M]. New York: Inc John Wiley & Sons, 2005: 134~144
11 Edge HL, Jubaraj Sahu,Heavey KR.Computational Fluid Dynamics Modeling of Submuniti on Separation from Missile.American Institute of Aeronautics & Astronautics, 1999: 215~225
12蔡星会,王小龙,孙新利.子母弹内弹道理论计算模型.上海航天, 2000, (6): 5~8
13 Hadar O, Rotman SR,Kopeika NS.Thermal image target acquisition probabilities in the presence of vibrations[J]. In-frared Phys Technol., 1999, 36(3): 691~702
14吴雪松.远程子母弹囊式抛撒结构设计及计算机仿真技术.南京理工大学硕士学位论文,2001:67-69
15雷娟棉,吴甲生,肖雅彬.布撒器-子弹气动干扰风洞实验研究.兵工学报, 2005, 26(4): 535~538
16 Thomas PD Middleeoff JF. Directeontrol of theghd Point distribution inmeshes generated byelli Ptieequations.AIAA Joumal, Vol.18, 2004: 652~656
17赵子才.再入弹头动力学分析与理论研究.火力与指挥控制, 2001: 68~70
18 Norman,M, Wereley Feasibility Study of a Smart Submunition Deployment from a Conventional Weapon.Army Research Laboratory, 2001: 156~158
19徐望.子弹弹道测量方法的研究.国防科技大学学报, 2000: 45~47
20杜之明.发射试验结果分析与鉴定技术.国防工业出版社, 2006: 36~39
21唐雪梅,徐文旭.子母弹抛撒的均匀性指标的确定及评定方法.系统工程与电子技术, 1999, 21(1): 11~14
22 Lo5H.Anew Mesh Generation Scheme For Jbitrary Planar Domains. Intemational Joumal For Numerical Methods In Engineering, Vol.ZI, 2002: 1403~1426
23雷宁利,唐雪梅.侵彻子母弹对机场跑道的封锁概率计算研究.系统仿真学报, 2004, 16(9): 2030~2032
24 Harris, L, Edge Computational Fluid Dynamics Modeling of Submunition Separation from Missile.Army Research Laboratory,1999: 134~136
25 Baker TJ. Three dimension nalmesh generate on by triangulation of arbitrary Pointset. AIAAPaPer, 2006: 87~112
26舒建生,王运吉,朱昱.子母弹抛撒半径对机场毁伤效果影响分析.火力与指挥控制, 2001, (3): 49~50
27 G., Denian Anti -Torpedo Combat System for Surface Ships. UDT, 1993: 23~26
28王纳,万国龙.常规战术子母弹封锁机场跑道效率研究.战术子母弹技术, 2003, 5(3): 1~4
29宋光明.子母弹打击机场跑道的计算机模拟.火力与指挥控制, 2001, 26(4): 67~69
30 Louis, J, Rodrigues Brilliant Antiarmor Submunition Opportunity Exists to Conduct Critical Test Prior to Production Decision. 1997: 87~90
31陈立周.稳健设计.机械工业出版社, 2000: 135~140
32张明宏,陈建新.提高子母弹子弹综合毁伤效能方法探讨[J].理论与探索, 2004, (5): 19~20
33 Wu Jeff, C.F., Michael Hamada著,张润楚等译.试验理论与分析及参数优化.中国统计出版社, 2003: 78~87
34 CorderD A,EstB E. Prediction of Submunition Dispense Aerodynamics[C]. 33rd Aerospace Sciences Meeting and Exhibit, Reno, NV, 1995: 193~199
35 David, K, steensma Acquisition of the Wide Area Munition.Audit Report. 2001: 342~345
36 PERKINA S C Jr, DILLENIUS MF E and SIN J L. Supersonic submunition aerodynamics during dispense[R]. AIAA Paper 88-0335: 212~216
37杨启仁.尾翼稳定脱壳穿甲弹总体基本参数设计.华东工学院, 2005: 90~95
38彭程远.稳健设计方法及其在飞行器设计中的应用研究.西北工业大学硕士学位论文, 2004: 56~58
39 DavidA. Field.LaPlacian Smoothing Ad Delaunay Tria ngulations. Communi- eations In APPlied Numerical Methods. Vol. 4, 2003: 709~712
40 XIE M Y, FANG K T. Admissibility and minimaxity of the u-niform design measure in nonparametric regression model [J]. Journal of Statistical Planning and Inference, 2003, 83: 101~111
41 A. M. Law, W. D. Kelton. Simulation Modeling and Analysis (Third Edition).清华大学出版社, 2000: 178~180
42 SANTNER T J, WILLIAMS B J, NOTZ W I. The design and analysis of computer experiments [M]. New York:Springer, 2003: 123~134
43陈入领.稳健设计进程策略的研究及实践.浙江大学硕士学位论文, 2003: 35~37
44 Jubaraj, sahu Computational Modeling of Sense and Destroy Armor (SADARM) Submunition Separation Collision.Army Research Laboratory, 1997: 29~32