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
  • [21] Dynamics design for multiple launch rocket system using transfer matrix method for multibody system
    Tang, Wenbing
    Rui, Xiaoting
    Wang, Guoping
    Rui, Xue
    Song, Zhendong
    Gu, Lilin
    PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART G-JOURNAL OF AEROSPACE ENGINEERING, 2016, 230 (14) : 2557 - 2568
  • [22] Study on simulation and experiment of control for multiple launch rocket system by computed torque method
    Li, Bo
    Rui, Xiaoting
    Zhou, Qinbo
    NONLINEAR DYNAMICS, 2018, 91 (03) : 1639 - 1652
  • [23] Vibration characteristics of airborne multiple launch rocket systems
    Institute of Launch Dynamics, Nanjing University of Science and Technology, Nanjing 210094, China
    Zhendong Gongcheng Xuebao, 2013, 1 (15-19):
  • [24] Study on simulation and experiment of control for multiple launch rocket system by computed torque method
    Bo Li
    Xiaoting Rui
    Qinbo Zhou
    Nonlinear Dynamics, 2018, 91 : 1639 - 1652
  • [25] Automatic Optical Tracking System for Rocket Launch
    Curetti, Maria
    Garcia Bravo, Santiago
    Mathe, Ladislao
    2014 IEEE BIENNIAL CONGRESS OF ARGENTINA (ARGENCON), 2014, : 304 - 309
  • [26] Trajectory Design of a Rocket-Scramjet-Rocket Multistage Launch System
    Forbes-Spyratos, Sholto O.
    Kearney, Michael P.
    Smart, Michael K.
    Jahn, Ingo H.
    JOURNAL OF SPACECRAFT AND ROCKETS, 2019, 56 (01) : 53 - 67
  • [27] DYNAMICS SIMULATION AND CONTROL DESIGN OF GUN ADJUSTMENT FOR NONLINEAR MULTIBODY SYSTEM OF MULTIPLE LAUNCH ROCKET SYSTEM
    Miao, Yunfei
    Wang, Guoping
    Rui, Xiaoting
    Tu, Tianxiong
    Gu, Lilin
    PROCEEDINGS OF THE ASME INTERNATIONAL DESIGN ENGINEERING TECHNICAL CONFERENCES AND COMPUTERS AND INFORMATION IN ENGINEERING CONFERENCE, 2019, VOL 6, 2020,
  • [28] A new method for evaluating the firing precision of multiple launch rocket system based on Bayesian theory
    Miao, Yunfei
    Wang, Guoping
    Tian, Wei
    DEFENCE TECHNOLOGY, 2024, 32 : 232 - 241
  • [29] A new method for evaluating the firing precision of multiple launch rocket system based on Bayesian theory
    Yunfei Miao
    Guoping Wang
    Wei Tian
    Defence Technology, 2024, 32 (02) : 232 - 241
  • [30] Optimization research of firing interval for Multiple Launch Rocket Systems
    Zhong Jian-lin
    Ma Da-wei
    Hu Jian-guo
    INFORMATION TECHNOLOGY APPLICATIONS IN INDUSTRY II, PTS 1-4, 2013, 411-414 : 3046 - 3051