Advanced Search
Volume 27 Issue 1
Jan.  2001
Turn off MathJax
Article Contents
Abstract
References
Journal of Beijing University of Aeronautics and Astronautics  > 2001  >  27(1): 40-43.
Wu Zhigang, Yang Chao. Volterra series based transonic unsteady aerodynamics modeling[J]. Journal of Beijing University of Aeronautics and Astronautics, 2006, 32(04): 373-376. (in Chinese)
Citation: PENG Ke-mao, SHEN Gong-zhang, WEN Chuan-yuanet al. Research on Tactic to Delivery Guided Bomb with Laser[J]. Journal of Beijing University of Aeronautics and Astronautics, 2001, 27(1): 40-43. (in Chinese)
shu

Research on Tactic to Delivery Guided Bomb with Laser

  • Beijing University of Aeronautics and Astronautics, Dept. of Automatic Control

  • Received Date: 15 Oct 1999
  • Publish Date: 31 Jan 2001
    Abstract
  • The tactic to delivery guided bomb with laser is researched, while the laser bundle is transmitted by the fighter itself, that is to delivery guided bomb with laser in non-wing-level and to egress in turning. The major is to egress in turning, which synthesizes tactical requirement to shoot the target with the laser bundle and motive to egress. It can efficiently improve survival ability of the fighter to delivery bombs in maneuvering motion and to egress in curve. The condition to satisfy the two requirements is proposed with a simplified particle point model of the fighter and through analysis on the process that the fighter egresses in turning while continuously shoot the target with laser bundle. Simulations on the mission process prove that the proposed condition can satisfy the tactical requirements to delivery guided bomb with laser and to egress in turning while the fighter transmits laser bundle to shoot the target itself.

     

    • FullText(HTML)
    • References(1)
  • [1] 陆 彦.航空火力控制原理[M]. 西安:西北工业大学出版社,1989. [2] 彭可茂.综合控制与自动机动攻击技术研究 .北京:北京航空航天大学自动控制系,1998. [3] Bennett W S, Ramage J R. AFTI/F-16 AMAS configuration development and integration . In:IEEE Aerospace and Electronic Systems Society,eds. Proceeding of the IEEE 1986 National Aerospace Electronics Conference . Vol 2. New York:Institute of Electrical and Electronic Engineers Inc, 1986.538~549. [4] Grisword M R. AFTI/F-16 AMAS guidance and control . In:IEEE Aerospace and Electronic Systems Society,eds. Proceeding of the IEEE 1986 National Aerospace Electronics Conference . Vol 2. New York:Institute of Electrical and Electronic Engineers Inc, 1986.560~566.
    • Relative Articles

  • Relative Articles

    [1]ZHOU Q Z，YANG Y X，SUN L B，et al. Aeroelastic optimization design of SpaRibs wing structure[J]. Journal of Beijing University of Aeronautics and Astronautics，2025，51（6）：2148-2156 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2023.0343.
    [2]CHEN Q，AN C，XIE C C，et al. Large deformation prediction and geometric nonlinear aeroelastic analysis based on machine learning algorithm[J]. Journal of Beijing University of Aeronautics and Astronautics，2025，51（3）：943-952 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2023.0111.
    [3]LI Z B，SUN W，ZHANG Y N，et al. Computation on aerodynamic and aeroacoustic characteristics of scissor tail-rotor under sideslip condition[J]. Journal of Beijing University of Aeronautics and Astronautics，2024，50（12）：3794-3805 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2023.0037.
    [4]MA C，SHU B W，HUANG J T，et al. Knowledge mining of aircraft configuration design for sonic boom/aerodynamics[J]. Journal of Beijing University of Aeronautics and Astronautics，2024，50（3）：975-984 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2022.0310.
    [5]LIU Shenshen, JIANG Bo, HAN Qinghua, YU Jing, YANG Xiaofeng, WEI Dong, ZHU Yandan, GUI Yewei. Study of cumulative thermal deformation characteristics and its impacts under long-endurance aerodynamic-thermal coupling effects[J]. Journal of Beijing University of Aeronautics and Astronautics. doi: 10.13700/j.bh.1001-5965.2023.0486
    [6]CAO Mengda, ZHENG Mengzong, SU Guanting, PAN Tianyu, LI Zhiping, LI Qiushi. Study on the Unsteady Aerodynamic Characteristics of a Flexible Flapping Plate at Low Reynolds Numbers[J]. Journal of Beijing University of Aeronautics and Astronautics. doi: 10.13700/j.bh.1001-5965.2024.0235
    [7]YUAN Kaihua, ZHANG Zhuoge, ZHA Jun, CHENG Meng, JI Hongli, LIU Kai, TIAN Haitao. WIND TUNNEL TEST FOR AEROELASTIC DYNAMIC RESPONSE SUPRESSION OF SUPERSONIC PANEL[J]. Journal of Beijing University of Aeronautics and Astronautics. doi: 10.13700/j.bh.1001-5965.2024.0602
    [8]LI Keyu, YANG Chao, WANG Xiaozhe, WAN Zhiqiang, LI Chang. Aeroelastic optimization of wing structure and material using multiple microstructures[J]. Journal of Beijing University of Aeronautics and Astronautics. doi: 10.13700/j.bh.1001-5965.2024.0178
    [9]LI Hao, ZHANG Xiao-rong, SUN Yan, DENG Yan-zeng, ZHU Zhi-mao. Automatic selection algorithm of interpolation points on aeroelastic coupling interface[J]. Journal of Beijing University of Aeronautics and Astronautics. doi: 10.13700/j.bh.1001-5965.2024.0079
    [10]CAO T T，YANG Y X，YU L F，et al. Whirl flutter on distributed electric propeller aircraft[J]. Journal of Beijing University of Aeronautics and Astronautics，2024，50（8）：2627-2635 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2022.0684.
    [11]XU H，HAN J L，XI Y，et al. Aeroelastic morphing flight simulation platform for a folding wing aircraft[J]. Journal of Beijing University of Aeronautics and Astronautics，2024，50（6）：1921-1930 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2022.0536.
    [12]LEI Chao-hui, YANG Chao, SONG Chen. Optimization design of active aeroelastic wing with variable camber[J]. Journal of Beijing University of Aeronautics and Astronautics. doi: 10.13700/j.bh.1001-5965.2023.0623
    [13]WU Y，XIE C C，YANG C. Optimal design of shape and motion parameters of a flapping wing[J]. Journal of Beijing University of Aeronautics and Astronautics，2023，49（12）：3311-3320 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2022.0146.
    [14]WEI R K，DAI Y T，YANG C，et al. Numerical study of wing gust response alleviation based on camber morphing trailing edge[J]. Journal of Beijing University of Aeronautics and Astronautics，2023，49（7）：1864-1874 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2021.0563.
    [15]SHI Y，WAN Z Q，WU Z G，et al. Aerodynamic order reduction method for elastic aircraft flight dynamics simulation[J]. Journal of Beijing University of Aeronautics and Astronautics，2023，49（7）：1689-1706 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2021.0510.
    [16]BAI L Y，WU Z G，YANG C. Nonlinear flutter modes and flutter suppression of an all-movable fin with freeplay[J]. Journal of Beijing University of Aeronautics and Astronautics，2023，49（9）：2361-2373 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2022.0162.
    [17]LI Z W，PENG M Y，GAO C Q，et al. Air combat maneuver trajectory prediction of target based on Volterra series optimized by SABA algorithm[J]. Journal of Beijing University of Aeronautics and Astronautics，2023，49（3）：503-513 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2021.0287.
    [18]LI X Y，WAN Z Q，WANG X Z，et al. Aeroelastic optimization for overall design of joined wing[J]. Journal of Beijing University of Aeronautics and Astronautics，2023，49（12）：3343-3354 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2022.0074.
    [19]WU Yue, XIE Changchuan, YANG Chao, An Chao. Optimal design of motion parameters of flapping wing[J]. Journal of Beijing University of Aeronautics and Astronautics, 2022, 48(7): 1324-1331. doi: 10.13700/j.bh.1001-5965.2021.0593
    [20]Yuan Kaihua, Qiu Zhiping. Flutter control of composite panels with embedded piezoelectric materials[J]. Journal of Beijing University of Aeronautics and Astronautics, 2009, 35(12): 1429-1433.
    • Supplements(0)
    • Cited By
  • 加载中

Catalog

    通讯作者: 陈斌, bchen63@163.com
    • 1. 

      沈阳化工大学材料科学与工程学院 沈阳 110142

    1. 本站搜索
    2. 百度学术搜索
    3. 万方数据库搜索
    4. CNKI搜索
    Get Citation
    PDF
    XML

    Article Metrics

    Article views(4314) PDF downloads(14) Cited by()
    Proportional views
    Related

    Copyright © Journal of Beijing University of Aeronautics and Astronautics

    Address: Editorial Department of Journal of Beijing University of Aeronautics and Astronautics, 37 Xueyuan Road, Haidian District, Beijing Post Code: 100191 Email: jbuaa@buaa.edu.cn

    Supported by: Beijing Renhe Information Technology Co., Ltd.    

    /

    DownLoad:  Full-Size Img  PowerPoint
    Return
    Return