制导化改进的常规航空炸弹命中精度分析

doi:10.3969/j.issn.1001-506X.2020.09.24

摘要/Abstract

摘要：

针对常规航空炸弹制导化改进的作战需求,研究了制导控制系统采用稳定控制回路和弹体构成的闭环系统方案,提出了稳定控制回路的设计方法。首先，分析了影响制导化改进的常规航空炸弹命中精度的主要误差表现形式和分布规律模型。其次，给出了基于蒙特卡罗法的命中精度分析方法。最后，采用A、B两组试验仿真分析了落点分布规律对圆概率误差(circular error probability, CEP)值和命中精度的影响。结果表明，分析方法科学合理,控制系统的设计方案可行。

关键词: 常规航空炸弹, 制导化改进, 制导控制, 命中精度

Abstract:

To satisfy the operational requirement of guidance improvement for conventional aerial bombs, the scheme of a closed-loop system for the guidance and control system utilizing the stable control loop and projectile is studied, and the design idea of the stability control loop is put forward. Firstly, the representation of the main errors and the model of distribution are analyzed which impacts the hit accuracy of the guidance improved conventional bomb. Secondly, the analytical method of hit accuracy based on Monte Carlo is given. Finally, A and B two set of experiments are used to analyze the influence of the distribution rule of drop point on the circular error probability (CEP) and hit accuracy. The simulation results show that the analysis method is scientific and reasonable, and the design scheme of the control system is feasible.

Key words: conventional aerial bomb, guidance improvement, guidance and control, hit accuracy

中图分类号:

E927.5

刘泽乾, 纪义国, 杨林, 田春艳, 刘俊峰. 制导化改进的常规航空炸弹命中精度分析[J]. 系统工程与电子技术, 2020, 42(9): 2071-2076.

Zeqian LIU, Yiguo JI, Lin YANG, Chunyan TIAN, Junfeng LIU. Hit accuracy analysis of guidance improved conventional aerial bomb[J]. Systems Engineering and Electronics, 2020, 42(9): 2071-2076.

图/表 7

图1

图2

图3

图4

图5

图6

图7

参考文献 26

1	王琦, 穆希辉, 路桂娥. 美军制导弹药发展现状及趋势[J]. 飞航导弹, 2015, (8): 12- 17.
	WANG Q , MU X H , LU G E . Development status and trend of guided munitions in the US military[J]. Aerodynamic Missile Journal, 2015, (8): 12- 17.
2	刘林海, 陈军, 王广海. 从美国空军弹药研讨会看制导航空弹药发展[J]. 飞航导弹, 2015, (6): 63- 68.
	LIU L H , CHEN J , WANG G H . Development of guided aerial munitions from the US air force ammunition seminar[J]. Aerodynamic Missile Journal, 2015, (6): 63- 68.
3	唐奕, 王建博, 王燕. 国外模块化制导航空炸弹发展概述[J]. 飞航导弹, 2018, (1): 38- 42.
	TANG Y , WANG J B , WANG Y . Overview of the development of modular guided aerial bombs abroad[J]. Aerodynamic Missile Journal, 2018, (1): 38- 42.
4	刘旭, 李为. 美俄军事卫星系统发展现状与趋势[J]. 国防科技, 2015, 36 (2): 43- 48.
	LIU X , LI W . Development status and trends of military satellite systems in the United States and Russia[J]. National Defense Technology, 2015, 36 (2): 43- 48.
5	刘百奇, 吕艳, 尹世明, 等. 一种起竖过程中捷联惯导快速对准方法[J]. 兵器装备工程学报, 2018, 39 (3): 169- 173. doi: 10.11809/bqzbgcxb2018.03.035
	LIU B Q , LYU Y , YIN S M , et al. A rapid alignment method for strapdown inertial navigation system during vertical alignment[J]. Journal of Ordnance Equipment Engineering, 2018, 39 (3): 169- 173. doi: 10.11809/bqzbgcxb2018.03.035
6	付心如, 徐爱功, 孙伟. 抗差自适应UKF的INS/GNSS组合导航算法[J]. 导航定位学报, 2017, 5 (2): 111- 116. doi: 10.3969/j.issn.2095-4999.2017.02.020
	FU X R , XU A G , SUN W . INS/GNSS combined navigation algorithm based on robust and adaptive UKF[J]. Journal of Navigation and Positioning, 2017, 5 (2): 111- 116. doi: 10.3969/j.issn.2095-4999.2017.02.020
7	LIU M. Research on GPS/INS integrated navigation algorithm[C]//Proc.of the 2nd International Conference on Electrical, Automation and Mechanical Engineering, 2017: 282-285.
8	王彦朋, 靳晓栋, 滑海, 等. SINS/GPS组合导航技术研究与分析[J]. 电子世界, 2016, (22): 53- 54. doi: 10.3969/j.issn.1003-0522.2016.22.046
	WANG Y P , JIN X D , HUA H , et al. Research and analysis of SINS/GPS integrated navigation technology[J]. Electronics World, 2016, (22): 53- 54. doi: 10.3969/j.issn.1003-0522.2016.22.046
9	樊云鹏, 杨锁昌. GNSS/INS深组合导航关键技术研究[J]. 飞航导弹, 2017, (10): 22- 25, 48.
	FAN Y P , YANG S C . Research on key technologies of GNSS/INS deep integrated navigation[J]. Aerodynamic Missile Journal, 2017, (10): 22- 25, 48.
10	WEI F M , ZHANG J P , YANG J , et al. A novel gyrocompass alignment method under large azimuth misalignment angle[J]. Journal of Shanghai Jiaotong University (Science), 2015, 20 (5): 558- 564. doi: 10.1007/s12204-015-1617-8
11	SILVA F O , HEMERLY E M , FILHO W C L . On the error state selection for stationary SINS alignment and calibration Kalman filters—part Ⅰ: estimation algorithms[J]. Aerospace Science and Technology, 2017, 61, 45- 56. doi: 10.1016/j.ast.2016.11.019
12	LI Z K , WANG J , GAO J X . An enhanced GPS/INS integra-ted navigation system with GPS observation expansion[J]. Journal of Navigation, 2016, 69 (5): 1041- 1060. doi: 10.1017/S0373463315001083
13	WANG Z Q , LI L H , LIU X , et al. Transfer alignment of ship-borne aircraft with large misalignment based on rotation vector error model[J]. Journal of Chinese Inertial Technology, 2016, 24 (6): 723- 729.
14	陈勇.速度加姿态匹配传递对准技术研究[D].哈尔滨:哈尔滨工业大学, 2017.
	CHEN Y. Research on speed and attitude matching transfer alignment technology[D]. Harbin: Harbin Institute of Technology, 2017.
15	ZHAO H , XIONG Z , SHI L J , et al. A robust filtering algorithm for integrated navigation system of aerospace vehicle in launch inertial co-ordinate[J]. Aerospace Science and Techno-logy, 2016, 58, 629- 640. doi: 10.1016/j.ast.2016.09.023
16	梁卓, 薛晓中, 孙瑞胜. 基于优化理论的"惯性/卫星"制导炸弹纵向复合制导律[J]. 火力与指挥控制, 2010, 35 (8): 48- 51. doi: 10.3969/j.issn.1002-0640.2010.08.013
	LIANG Z , XUE X Z , SUN R S . Longitudinal compound gui-dance law of inertial/satellite guided bombs based on optimization theory[J]. Fire Control & Command Control, 2010, 35 (8): 48- 51. doi: 10.3969/j.issn.1002-0640.2010.08.013
17	梁卓. SINS/GPS制导炸弹变结构制导控制系统设计与研究[D].南京:南京理工大学, 2014.
	LIANG Z. Design and research of SINS/GPS guided bomb variable structure guidance control system[D]. Nanjing: Nanjing University of Science & Technology, 2014.
18	行健. 珠海航展中国机载制导炸弹[J]. 兵器知识, 2011, 6 (1): 32- 33.
	XING J . China airborne guided bomb at Zhuhai air show[J]. Ordnance Knowledge, 2011, 6 (1): 32- 33.
19	秦蓁. 珠海航展"雷石"6制导炸弹系列[J]. 兵器知识, 2011, (1): 85.
	QIN Z . Zhuhai air show "thunderstone" 6 guided bomb series[J]. Ordnance Knowledge, 2011, (1): 85.
20	贾秋锐, 孙媛媛, 肖树臣, 等. 航空制导炸弹发展趋势[J]. 制导与引信, 2014, 35 (1): 8- 11. doi: 10.3969/j.issn.1671-0576.2014.01.002
	JIA Q R , SUN Y Y , XIAO S C , et al. Development trend of the aerial guided bomb[J]. Guidance & Fuze, 2014, 35 (1): 8- 11. doi: 10.3969/j.issn.1671-0576.2014.01.002
21	张尧, 郭杰, 唐胜景. 导弹制导与控制一体化三通道解耦设计方法[J]. 航空学报, 2014, 35 (12): 3438- 3450.
	ZHANG Y , GUO J , TANG S J . Design method of integrated three-channel decoupling for missile guidance and control[J]. Acta Aeronautica et Astronautica Sinica, 2014, 35 (12): 3438- 3450.
22	高娟, 韩惠珍, 白军. SINS/GPS紧耦合与松耦合组合导航系统分析[J]. 四川兵工学报, 2011, 32 (10): 92- 96.
	GAO J , HAN H Z , BAI J . Analysis of SINS/GPS combined navigation system with tight coupling and loose coupling[J]. Journal of Sichuan Ordnance, 2011, 32 (10): 92- 96.
23	胡国欣, 李安, 覃方君. 基于伪距、伪距率的组合导航误差校正仿真[J]. 电子设计工程, 2018, 26 (6): 105- 108. doi: 10.3969/j.issn.1674-6236.2018.06.023
	HU G X , LI A , QIN F J . Simulation of combined navigation error correction based on pseudo-distance and pseudo-distance rate[J]. Electronic Design Engineering, 2018, 26 (6): 105- 108. doi: 10.3969/j.issn.1674-6236.2018.06.023
24	WANG Z , WANG J . Guided bomb release planning based on Monte Carlo in a distributed virtual environment[J]. The Aeronautical Journal, 2013, 117 (1192): 585- 602. doi: 10.1017/S0001924000008228
25	许建胜, 苏坡, 戎永杰. 基于蒙特卡罗法的末敏弹命中点散布研究[J]. 弹箭与制导学报, 2015, 35 (6): 29- 32.
	XU J S , SU P , RONG Y J . Monte Carlo method based on the impact point dispersion of terminal sensitive missile[J]. Journal of Projectiles, Rockets, Missiles and Guidance, 2015, 35 (6): 29- 32.
26	薛震.制导化改进的250 kg常规航空炸弹制导控制研究[D].长春:空军航空大学, 2016.
	XUE Z. Research on 250 kg conventional aerial bomb guidance control with guidance modification[D]. Changchun: Air Force Aviation University, 2016.

[1]	安通, 王鹏, 王建华, 汤国建, 潘玉龙, 陈海山. 弹性高超声速飞行器动态面制导控制一体化设计方法[J]. 系统工程与电子技术, 2022, 44(3): 956-966.
[2]	赵坤, 曹登庆, 黄文虎. 突防导弹机动、制导与控制一体化设计[J]. 系统工程与电子技术, 2018, 40(9): 2040-2047.
[3]	张登辉, 马萍, 晁涛, 王松艳. 高超声速飞行器制导控制系统性能评估[J]. 系统工程与电子技术, 2018, 40(8): 1811-1816.
[4]	夏川, 董朝阳, 王青, 程昊宇. 复合控制导弹反步滑模IGC自适应设计方法[J]. 系统工程与电子技术, 2018, 40(10): 2325-2333.
[5]	齐辉1, 张泽1, 韩鹏鑫2, 许江涛1, 张德伟1. 基于反演滑模控制的导弹制导控制一体化设计[J]. 系统工程与电子技术, 2016, 38(3): 618-623.
[6]	董朝阳, 程昊宇, 王青. 基于自抗扰的反步滑模制导控制一体化设计[J]. 系统工程与电子技术, 2015, 37(7): 1604-1610.
[7]	尹永鑫，石文，杨明. 基于动态逆和状态观测的制导控制一体化设计[J]. Journal of Systems Engineering and Electronics, 2011, 33(6): 1342-1345.
[8]	杨雪榕1，李晓冬2，梁加红1. 空空导弹高抛弹道复合制导律研究[J]. Journal of Systems Engineering and Electronics, 2009, 31(12): 2918-2923.