Air-to-Air Missile Launch Envelope Computation Based on Neural Network

被引:0
|
作者
Fang, Feng [1 ,2 ]
Li, Qingwei [1 ]
He, Jiafan [1 ]
Mao, Yiming [1 ]
Ding, Feng [1 ]
Fei, Aiguo [1 ]
机构
[1] Sci & Technol Informat Syst Engn Lab, Nanjing, Peoples R China
[2] Hangzhou Dianzi Univ, Hangzhou, Peoples R China
关键词
Missile launch envelope; Neural network; Golden section; Pursuit-evasion engagement simulation;
D O I
10.1007/978-981-99-0479-2_355
中图分类号
TP [自动化技术、计算机技术];
学科分类号
0812 ;
摘要
A fast algorithm for computing air-to-air missile launch envelope based on neural network is proposed, which can be applied to an air combat scenario for choosing the optimal missile launch time. Firstly, the simplified six-degree-of-freedom motion models of missile and fighter are built. Secondly, the missile-fighter pursuit-evasion engagement is simulated, by designing the traditional guidance strategy of missile and the common evasion maneuver of fighter. After that, the golden section method is used to search the launch envelope, and the envelope database is generated by simulating various air combat scenarios. Based on the database, the neural network is trained, and its optimal structure is determined by comparing the network performance with different number of layers and nodes. Lastly, the simulation results show that the proposed algorithm has a smaller computation error, compared with the traditional method of interpolation method.
引用
收藏
页码:3844 / 3853
页数:10
相关论文
共 50 条
  • [41] AIR-TO-AIR MISSILE AIRFRAME CAPTIVE FLIGHT VIBROACOUSTIC ENVIRONMENT
    POYNOR, SP
    JOURNAL OF THE IES, 1990, 33 (04): : 44 - 52
  • [42] Agile Turn Control for Air-to-Air Missile Based on Reaction Jet Control System
    Ma, Yue Yue
    Tang, Sheng Jing
    MANUFACTURING ENGINEERING AND AUTOMATION II, PTS 1-3, 2012, 591-593 : 1285 - 1288
  • [43] Learning Based Edge Computing in Air-to-Air Communication Network
    Wang, Zhe
    Li, Hongxiang
    Knoblock, Eric J.
    Apaza, Rafael D.
    2021 ACM/IEEE 6TH SYMPOSIUM ON EDGE COMPUTING (SEC 2021), 2021, : 333 - 338
  • [44] Research on Fast Calculation Technology of Air-to-Air Missile Impact Area
    Zhang, Yijie
    Wu, Yong
    Zhang, Yi
    Yue, Longfei
    PROCEEDINGS OF THE IEEE 2019 9TH INTERNATIONAL CONFERENCE ON CYBERNETICS AND INTELLIGENT SYSTEMS (CIS) ROBOTICS, AUTOMATION AND MECHATRONICS (RAM) (CIS & RAM 2019), 2019, : 245 - 250
  • [45] Multidisciplinary integrated design optimization for an airbreathing air-to-air missile shape
    Wang R.
    Zhang H.
    Wang G.
    Chen G.
    Bai P.
    Zhang Z.
    Li X.
    Fu J.
    Hangkong Xuebao/Acta Aeronautica et Astronautica Sinica, 2016, 37 (01): : 207 - 215
  • [46] Research on the Algorithm of Initial Alignment for New Generation Air-to-air Missile
    Feng, Min
    Xu, Xinpeng
    Wang, Xin
    Yin, Wei
    Liu, Ying
    Zhang, Di
    PROCEEDINGS OF THE 32ND 2020 CHINESE CONTROL AND DECISION CONFERENCE (CCDC 2020), 2020, : 4378 - 4383
  • [47] Study on stability of air-to-air missile in firing-back attack
    Zhang, Huaming
    Jiang, Yuxian
    Beijing Hangkong Hangtian Daxue Xuebao/Journal of Beijing University of Aeronautics and Astronautics, 2004, 30 (06): : 572 - 576
  • [48] Dynamic consistency test method for air-to-air missile simulation results
    Chen, Jian-Wei
    Fu, Hui-Min
    Xitong Fangzhen Xuebao / Journal of System Simulation, 2008, 20 (19): : 5121 - 5124
  • [49] Europe and US missile makers in dogfight over air-to-air market
    Wall, R
    Fulghum, DA
    Barrie, D
    AVIATION WEEK & SPACE TECHNOLOGY, 2002, 157 (04): : 169 - 170
  • [50] Optimal midcourse guidance of an air-to-air missile via SVM and RVM
    Mohammad Reza Mortazavi
    Farshad Almasganj
    Soft Computing, 2019, 23 : 6603 - 6616