[an error occurred while processing this directive] [an error occurred while processing this directive] [an error occurred while processing this directive]
[an error occurred while processing this directive]

直升机载航空火箭弹仰射作战分析

  • 黄若超 ,
  • 高宏超 ,
  • 毛瑞 ,
  • 何庆华 ,
  • 汪恒
展开
  • 西安现代控制技术研究所, 陕西 西安 710065

黄若超(1991—), 女, 高级工程师, 硕士。E-mail:

收稿日期: 2024-06-20

  网络出版日期: 2025-05-15

Analysis of Elevated Firing Operations with Helicopter-mounted Aerial Rockets

  • HUANG Ruochao ,
  • GAO Hongchao ,
  • MAO Rui ,
  • HE Qinghua ,
  • WANG Heng
Expand
  • Xi'an Mordern Control Technology Research Institute, Xi'an 710065, Shaanxi, China

Received date: 2024-06-20

  Online published: 2025-05-15

摘要

针对直升机上仰发射航空火箭弹存在的落点精度差问题, 通过仰射作战机理分析提出了一种上仰发射改进方式, 基于国外公开的武装直升机及航空火箭弹参数建立了弹道与毁伤效能仿真模型, 选取上仰和平飞发射典型条件进行射程、散布、毁伤效能对比分析。仿真结果表明, 上仰发射改进后的航空火箭弹攻击距离可达到9 km, 同时纵向散布呈减小趋势, 组有效毁伤面积是平飞条件下的3倍。文中所提的改进仰射作战方式及火控、稳瞄优化建议对直升机仰射作战应用具有一定的指导意义。

本文引用格式

黄若超 , 高宏超 , 毛瑞 , 何庆华 , 汪恒 . 直升机载航空火箭弹仰射作战分析[J]. 弹箭与制导学报, 2025 , 45(2) : 260 -265 . DOI: 10.15892/j.cnki.djzdxb.2025.02.017

Abstract

To address the issue of poor impact accuracy in elevated firing operations of helicopter-mounted aerial rockets, an improved method for elevated firing has been proposed through analyzing the combat mechanisms involved. A simulation model for the ballistic trajectory and the damage effectiveness has been established based on the publicly available parameters of a certain armed helicopter and its aerial rockets from abroad. Typical conditions of elevated and level flight firings are selected for comparative analysis of range, dispersion, and damage effectiveness. The simulation results indicate that the improved aerial rockets, when fired in an elevated position, can achieve an attack distance of up to 9 km, while also exhibiting a trend of reduced longitudinal dispersion. The effective damage area of the rocket salvo is 3 times that under level flight conditions. The improved elevated firing method and the suggestions for the fire control and the aiming stabilization optimization mentioned in this paper have certain guiding significance for the application of helicopter elevated firing operations.

[an error occurred while processing this directive]
[1]
曹林平, 黄长强. 武装直升机机载火箭弹对地最佳攻击条件研究[J]. 弹箭与制导学报, 1999, 19(3):41-46.

CAO L P, HUANG C Q. Study of optimum attack condition for air-to-land firing airborne rockets launched by armed helicopter[J]. Journal of Projectiles, Rockets, Missiles and Guidance, 1999, 19(3):41-46.

[2]
王晓光, 何镜, 刘东兴, 等. 俄乌冲突中的航空弹药作战使用分析与启示[J]. 战术导弹技术, 2022 (4):23-29.

WANG X G, HE J, LIU D X, et al. Analysis and discussion on application of aviation munitions in the Russia-Ukraine conflict[J]. Tactical Missile Technology, 2022(4):23-29.

[3]
MACKINTOSH E. What does Putin want in Ukraine?The conflict explained[EB/OL].(2022-02-28)[2024-03-13]. https://edition.cnn.com/2022/02/24/europe/ukraine-russia-conflict-explainer-2-cmd-intl/index.html.

[4]
郭超. 破片式高炮弹药对武装直升机的毁伤评估研究[D]. 南京: 南京理工大学, 2017.

GUO C. A study to assess the damage of antiaircraft cartridge against the armed helicopter[D]. Nanjing: Nanjing University of Science and Technology, 2017.

[5]
洪大银, 夏成量. 破片式高炮弹药对武装直升机的毁伤评估研究[J]. 中国设备工程, 2020(4):221-222.

HONG D Y, XIA C L. Research on damage assessment of fragmentation-type anti-aircraft artillery ammunition against armed helicopters[J]. China Plant Engineering, 2020(4): 221-222.

[6]
何瑞恒. 军用直升机生存力标准研究[J]. 航空标准化与质量, 2014(5):10-12.

HE R H. Research on survivability standards for military helicopters[J]. Aeronautic Standardization & Quality, 2014(5): 10-12.

[7]
王岐朋, 李嘉诚, 王韩. 俄乌冲突中的便携式防空导弹[J]. 轻兵器, 2022(7):40-42.

WANG Q P, LI J C, Wang H. Portable air defense missiles in the Russia-Ukraine conflict[J]. Small Arms, 2022(7): 40-42.

[8]
何小盼, 罗冲凌, 刘杰. 俄乌冲突中防空反导作战分析[C]// 北京宇航学会.2022年俄乌冲突对未来作战及先进武器发展影响研究论文集. 贵阳: 贵阳出版社, 2022:23-26.

HE X P, LUO C L, LIU J. Analysis of air defense and anti-missile operations in the Russia-Ukraine conflict[C]// Beijing Institute of Aeronautics and Astronautics. Proceedings of the 2022 Research on the Impact of the Russia-Ukraine Conflict on Future Warfare and Advanced Weaponry Development. Guiyang: Guiyang Publishing House, 2022: 23-26.

[9]
于琦. 国外武装直升机型号发展与作战能力分析[J]. 科技导报, 2017, 35(15):28-33.

DOI

YU Q. Model development and combat ability analysis for foreign armed helicopters[J]. Science & Technology Review, 2017, 35(15): 28-33.

[10]
王从阳, 王东南, 王立文. 信息化条件下陆航作战运用与直升机的发展[J]. 国防科技, 2009, 30(2):50-51.

WANG C Y, WANG D N, WANG L W. The operational application of army aviation in situation of informatization and the developent of helicopters[J]. National Defense Science & Technology, 2009, 30(2): 50-51.

[11]
钱杏芳, 林瑞雄, 赵亚男. 导弹飞行力学[M]. 北京: 北京理工大学出版社, 2008.

QIAN X F, LIN R X, ZHAO Y N. Missile flight dynamics[M]. Beijing: Beijing Institute of Technology Press, 2008.

[12]
杨绍卿. 火箭外弹道偏差与修正理论[M]. 北京: 国防工业出版社, 2011:98-144.

YANG S Q. The trajectory error and correction theory of rockets[M]. Beijing: National Defense Industry Press, 2011: 98-144.

[13]
刁平, 葛银茂, 王超勇. 航空火箭弹对地攻击命中概率的计算与分析[J]. 实用测试技术, 2001(3):14-15.

DIAO P, GE Y M, WANG C Y. Calculation and analysis of hit probability for air-to-ground attacks with aerial rockets[J]. Practical Measurement Technology, 2001(3): 14-15.

[14]
张先锋, 李向东, 沈培辉, 等. 终点效应学[M]. 北京: 北京理工大学出版社, 2017:133-159.

ZHANG X F, LI X D, SHEN P H, et al. Terminal effects[M]. Beijing: Beijing Institute of Technology Press, 2017: 133-159.

[15]
王林, 李彤华, 李晓辉, 等. 人员目标特性的战斗部杀伤威力评价方法[J]. 四川兵工学报, 2011, 32(11):122-124.

WANG L, LI T H, LI X H, et al. Evaluation method for the lethal effectiveness of warheads based on personnel target characteristics[J]. Journal of Sichuan Ordnance, 2011, 32(11): 122-124.

文章导航

/

[an error occurred while processing this directive]