基于遗传算法的空地一体化攻击模糊比例导引律

doi:10.3969/j.issn.1000-1093.2017.10.010

兵工学报 ›› 2017, Vol. 38 ›› Issue (10): 1950-1956.doi: 10.3969/j.issn.1000-1093.2017.10.010

基于遗传算法的空地一体化攻击模糊比例导引律

李波，王元勋，高晓光，崔四杰

(西北工业大学电子信息学院，陕西西安 710100)

收稿日期:2017-03-24 修回日期:2017-03-24 上线日期:2017-11-22
作者简介:李波(1978—)，男，副教授，硕士生导师。 E-mail: libo803@nwpu.edu.cn
基金资助:
中央高校基本科研业务费专项项目(3102016CG002)

Research on Fuzzy Proportional Guidance Law of Air-to-ground Attack Based on Genetic Algorithm

LI Bo， WANG Yuan-xun， GAO Xiao-guang， CUI Si-jie

(School of Electronics and information, Northwestern Polytethnical University, Xi'an 710072, Shaanxi, China)

Received:2017-03-24 Revised:2017-03-24 Online:2017-11-22

摘要/Abstract

摘要： 针对空空导弹具有攻击空中目标和地面目标双任务的发展趋势，为满足导弹空地一体化综合作战模式需要，设计了一种适应双任务空空导弹作战需要的攻击导引律。在三维比例导引律的基础上，根据导弹和目标状态信息，利用遗传算法求解最优模糊控制规则；利用模糊控制来控制导引律在空间三轴的比例系数分量，从而建立了一种适应空地一体化攻击模式的导引律；通过仿真实验对空地一体化攻击导引律和传统三维比例导引律进行了对比。仿真结果表明：所设计的导引律能兼顾双任务攻击方式，且在对地面目标打击时具有更大的命中落角，更加适应空地一体化攻击作战模式。

关键词: 兵器科学与技术, 空地一体化, 遗传算法, 模糊控制, 导引律, 仿真

Abstract: At present, one of the development trends of air-to-air missiles is that the missile is used to attack both ground and air targets. On the basis of the three-dimensional proportional guidance law， the genetic algorithm is used to solve the optimal fuzzy control rules, and then the fuzzy control theory is used to control the proportional coefficient component of the three-axis in the proportional guidance law, thus establishing an integrated guidance law that enables the missiles to effectively attack the air and ground targets. The missile air-ground integrated attack guidance law is compared with the traditional three-dimensional proportional guidance law through the simulation experiment. The simulated results show that the proposed navigation law can be used for missile attacking the air-to-ground targets effectively and hasving a greater hit angle in the attack on ground target, so it is suitable for the air-to-ground integrated attack mode.Key

Key words: ordnancescienceandtechnology, air-to-groundintegration, geneticalgorithm, fuzzycontrol, guidancelaw, simulation

中图分类号:

TJ765.2⁺2

李波，王元勋，高晓光，崔四杰. 基于遗传算法的空地一体化攻击模糊比例导引律[J]. 兵工学报, 2017, 38(10): 1950-1956.

LI Bo， WANG Yuan-xun， GAO Xiao-guang， CUI Si-jie. Research on Fuzzy Proportional Guidance Law of Air-to-ground Attack Based on Genetic Algorithm[J]. Acta Armamentarii, 2017, 38(10): 1950-1956.

参考文献

［1］张同贺. 红外型空空导弹技术发展展望[J]. 红外技术, 2016, 38(10):813-819.
ZHANG Tong-he. A technical review of infrared air-to-air missiles [J]. Infrared Technology, 2016, 38(10):813-819. (in Chinese)
[2] Kane R W. Recent developments in air warfare including the atom bomb and missiles-war college series[M]. London, UK: War College Series, 2015:3-15.
[3] Stephen T. DARPA fires starting gun for new stealth missile[J]. Flight International, 2010, 11(3):9-15.
[4] 杨廷梧. 五维空间一体化试验体系的发展与思考[J]. 飞行力学,2016, 34(5):1-6.
YANG Ting-wu. Development and thinking of integrated test network architecture in 5-D space[J]. Flight Dynamics, 2016, 34(5): 1-6. (in Chinese)
[5] Daniel V. Information warfare[M]. Paris, France: Wiley ISTE, 2016:5-12.
[6] Rajasekhar V, Sreenatha A G. Fuzzy logic implementation of proportional navigation guidance[J]. Acta Astronautica, 2000, 46(1): 17-24.
[7] 邵节, 刘佳琪, 张超, 等. 基于模糊逻辑的导弹扩展比例导引律[J]. 导弹与航天运载技术, 2016(2):66-71.
SHAO Jie, LIU Jia-qi, ZHANG Chao,et al. Extended proportional guidance law of missile based on fuzzy logic[J]. Missile and Space Vehicles, 2016(2):66-71. (in Chinese)

[8] 熊俊辉, 唐胜景, 郭杰, 等. 基于模糊变系数策略的迎击拦截变结构制导律设计[J]. 兵工学报, 2014, 35(1): 134-139.
XIONG Jun-hui, TANG Sheng-jing, GUO Jie, et al. Design of variable structure guidance law for head-on interception based on variable coefficient strategy[J]. Acta Armamentarii, 2014, 35(1): 134-139.(in Chinese)
[9] 陈昌旭, 李洋, 祁琪, 等. 基于滑模变结构的导弹制导律设计[J]. 兵器装备工程学报, 2016, 37(12):56-59.
CHEN Chang-xu, LI Yang, QI Qi, et al. Missile guidance law design based on sliding mode[J].Journal of Ordnance Equipment Engineering, 2016, 37(12):56-59. (in Chinese)

[10] Stormy A. Matlab: a practical introduction to programming and problem solving[M]. 4th ed. MA, US: Stormy Attaway, 2016: 4-15.
[11] Jiau M K, Huang S C, Lin C H. Optimizing the carpool service problem with genetic algorithm in service-based computing[C]∥Proceedings of 2013 IEEE International Conference on Services Computing. Santa Clara, CA, US: IEEE, 2013:478-485.
[12] 孙增圻, 邓志东, 张再兴. 智能控制理论与技术[M]. 北京：清华大学出版社, 2011.
SUN Zeng-xi, DENG Zhi-dong，ZHANG Zai-xing. Intelligent control theory and technology [M]. Beijing: Tsinghua University Press, 2011. (in Chinese)

[13] Santos W. Fuzzy control systems: design, analysis & performance evaluation[M]. NY, US: Nova Science Publishers Inc,2017:108-127.
[14] 李波, 崔四杰, 高晓光. 空地一体化多任务导弹攻击模式研究[J]. 电光与控制, 2014,21(12):5-9,56.
LI Bo，CUI Si-jie，GAO Xiao-guang. Research on attack mode of air-ground integrated multi-tasking missile[J]. Electronics Optics & Control, 2014, 21(12):5-9, 56. (in Chinese)
[15] 苏锋. 模糊神经网络解耦[D]. 大连:大连理工大学, 2000.
SU Feng. Fuzzy neural network decoupling [D].Dalian:Dalian University of Technology, 2000. (in Chinese)

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基于遗传算法的空地一体化攻击模糊比例导引律

Research on Fuzzy Proportional Guidance Law of Air-to-ground Attack Based on Genetic Algorithm

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