INTERACTIVE HYBRID AIR-TO-AIR MISSILE CONTOUR PROGRAM

被引：0
|
作者：
KATZ, S
NEUMANN, D
PELED, U
机构：
来源：
ISRAEL JOURNAL OF TECHNOLOGY | 1975年 / 13卷 / 1-2期
关键词：
D O I：
暂无
中图分类号：
T [工业技术];
学科分类号：
08 ;
摘要：
引用
收藏
页码：16 / 24
页数：9
相关论文
共 50 条
  • [31] The technique for air-to-air missile guidance superiority handover based on particle swarm auction hybrid algorithm
    Fei, A.-G. (feiaiguo@263.net), 1600, China Spaceflight Society (34):
  • [32] Analysis of errors sensitivity for air-to-air missile launch control parameters
    Hangkong Xuebao, 6 (702-706):
  • [33] 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
  • [34] 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
  • [35] 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
  • [36] 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
  • [37] 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
  • [38] 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
  • [39] Optimal midcourse guidance of an air-to-air missile via SVM and RVM
    Mohammad Reza Mortazavi
    Farshad Almasganj
    Soft Computing, 2019, 23 : 6603 - 6616
  • [40] Longitudinal robust autopilot design for air-to-air missile using μ synthesis
    College of Automation Engineering, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China
    Nanjing Li Gong Daxue Xuebao, 2009, 6 (766-769):
12345