Modelling the suitability of multiple launch rocket system in the war in Ukraine

被引:0
|
作者
Chow, T. Edwin [1 ]
Sanchez, Dustin Paul [1 ]
Amatya, Prawan [2 ]
Tanzir, Md Tousif [1 ]
机构
[1] Texas State Univ, Dept Geog & Environm Studies, San Marcos, TX 78666 USA
[2] GeoNadir Naxa Pvt Ltd, Do Cha Marg,Maharajgunj-3, Kathmandu, Nepal
关键词
FIRMS; Missile detection; Warfare geography; Geospatial intelligence; Google earth engine; Cloud computing; MODIS;
D O I
10.1016/j.apgeog.2024.103206
中图分类号
P9 [自然地理学]; K9 [地理];
学科分类号
0705 ; 070501 ;
摘要
Since the war started, both Russian and Ukraine forces have been using Multiple Launch Rocket System (MLRS). Theoretically, the heated particulate matter residuals from MLRS could be captured by satellite imageries, but this premise has never been tested. In this study, the Fire Information for Resource Management System (FIRMS) data were analyzed to identify anthropogenic thermal anomalies resulting from the war in Ukraine. The research team examined the frequency of Feb-June FIRMS in both long-term (2001-2021) and short-term trends (2022), as well as the recency of last FIRMS date. In addition, other crucial factors like site control and the proximity of nearby Russian troops are also considered in developing this suitability model. Human analysts with military knowledge, understanding of standard operating procedure and the strategic importance of a developing battlefield were deployed to identify potential tactical firing locations. The proposed model was developed on Google Earth Engine for ease of distribution and deployment. Four case studies are demonstrated to illustrate the implemented model, interpreted in the context of ongoing conflicts and verified by geospatial intelligence crowdsourced and/or reported by the public and social media. This study provides counter-MLRS geospatial intelligence from crowdsourced data and publicly available satellite imagery.
引用
收藏
页数:10
相关论文
共 50 条
  • [31] Progress and key points for guidance of multiple launch rocket systems
    Yang S.-X.
    2016, China Ordnance Industry Corporation (37): : 1299 - 1305
  • [32] A Novel Vibration Control System Applying Annularly Arranged Thrusters for Multiple Launch Rocket System in Launching Process
    Gu, Lilin
    Rui, Xiaoting
    Wang, Guoping
    Yang, Fufeng
    Wei, Min
    SHOCK AND VIBRATION, 2020, 2020 (2020)
  • [33] LAUNCH RESULTS OF GUIDANCE & CONTROL SYSTEM OF EPSILON ROCKET
    Ohtsuka, Hirohito
    Morita, Yasuhiro
    Tanaka, Kensaku
    Saiki, Takanao
    Yamamoto, Takayuki
    Yamaguchi, Hiroyuki
    Segawa, Yasunobu
    Gotoh, Hitomi
    ASTRODYNAMICS 2015, 2016, 156 : 2063 - 2073
  • [34] Fast fault diagnosis expert system for rocket launch
    Zhang, Qingzhen
    Wang, Wei
    Song, Lihui
    Ren, Zhang
    PROCEEDINGS OF THE INTERNATIONAL CONFERENCE ON INTELLIGENT SYSTEMS AND KNOWLEDGE ENGINEERING (ISKE 2007), 2007,
  • [35] Neural-network-predictor-based control for an uncertain multiple launch rocket system with actuator delay
    Li, Bo
    Rui, Xiaoting
    Tian, Wei
    Cui, Guangyu
    MECHANICAL SYSTEMS AND SIGNAL PROCESSING, 2020, 141
  • [36] Study on test dynamics method of non-full loading firing for multiple launch rocket system
    Miao, Yunfei
    Wang, Guoping
    Rui, Xiaoting
    Tu, Tianxiong
    MECHANICAL SYSTEMS AND SIGNAL PROCESSING, 2019, 122 : 463 - 479
  • [37] Vibration control of uncertain multiple launch rocket system using radial basis function neural network
    Li, Bo
    Rui, Xiaoting
    MECHANICAL SYSTEMS AND SIGNAL PROCESSING, 2018, 98 : 702 - 721
  • [38] Numerical simulation of multiple launch rocket whole transient heat characteristics
    Zhao, Ji-Yong
    Ma, Da-Wei
    Le, Gui-Gao
    Nanjing Li Gong Daxue Xuebao/Journal of Nanjing University of Science and Technology, 2010, 34 (01): : 66 - 70
  • [39] Analysis of sneak path of liquid launch rocket engine system
    Zhai Zhiheng
    SEVENTH ASIA PACIFIC CONFERENCE ON OPTICS MANUFACTURE (APCOM 2021), 2022, 12166
  • [40] MARKS SMALL AVIATION-ROCKET SPACE LAUNCH SYSTEM
    Smolyakov, A. V.
    Yanakaev, V. A.
    Kornev, A. V.
    Shevko, S. V.
    JOURNAL OF ENGINEERING SCIENCE AND TECHNOLOGY, 2018, 13 (05) : 1143 - 1152