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http://dx.doi.org/10.9766/KIMST.2018.21.4.551

Application and Determination of Defended Footprint Using a Simulation Model for Ballastic Missile Trajectory  

Hong, Dongwg (The 1st Research and Development Institute, Agency for Defense Development)
Yim, Dongsoon (Department of Industrial and Management Engineering, Hannam University)
Choi, Bongwhan (Department of Industrial and Management Engineering, Hannam University)
Publication Information
Journal of the Korea Institute of Military Science and Technology / v.21, no.4, 2018 , pp. 551-561 More about this Journal
Abstract
Footprint is defined as ground area that is projected from the outer edges of the battle space protected by a defence system. This concept can be effectively used for making decisions on site selection of anti missile systems to defend against enemy's ballistic missiles. In this paper, simulations of ballistic missile trajectories based on various launch conditions are performed first and then the footprint is derived with engagement zone set as a boundary condition. Results of the simulation with various relative positions between the defense system and defended asset are also presented. The proposed method, in which the trajectories are generated based on launch point of the ballistic missile, has an advantage of approximating the defended area close to reality. Two applications are introduced in the present paper to describe how the derivation of defended area could be utilized in deployment decision of defense systems.
Keywords
Ballistic Missile; Missile Defence; Defended Asset; Footprint;
Citations & Related Records
Times Cited By KSCI : 1  (Citation Analysis)
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1 Lu, Y, Miao W., Li, Ming, “The Air Defense Missile Optimum Target Assignemnt based on the Improved Genetic Algorithm,” Journal of Theoretical and Applied Information Technology, Vol. 48, No. 2, pp. 809-816, 2013.
2 Selvi, S. T. and Malmathanraj, R., “Missile Defence and Interceptor Allocation by LVQ-RBF Multi-agent Hybrid Architecture,” Defence Science Journal, Vol. 57, No. 2, pp. 173-183, 2007.   DOI
3 Mantle, Peter J., "The Missile Defence Equation : Factors for Decision Making," AIAA, pp. 109-110, 2004.
4 C. H. Jung, "An Optimal Missile Allocation Problem for Maximizing Kill Probability," Journal of the Korean Operations Research & Management Science Society Vol. 27, No. 1, 2006.
5 Jae-Kwon Kim, Hyeonju Seol, "The Optimal Deployment Problem of Air Defense Artillery for Missile Defense," Korea Ind. Syst. Eng., Vol. 39, No. 1, pp 98-104, 2016.
6 Forden, Geoffrey, "GUI Missile Flyout : A General Program for Simulating Ballastic Missiles, Science and Global Security," Vol. 15, pp. 133-146, 2007.
7 Heung Seob Kim, Ki Tae Kim, Geonwook Jeon, “A Requirement Assessment Algorithm for Anti-Ballistic Missile Considering Ballastic Missile’s Flight Characteristics,” Journal of the KIMST, Vol. 14, No. 6, pp. 1009-1017, 2011.
8 J. H. Kim, A Study on Requirements Derivation of rhe Lower Tier Defense Sensor Systems based TBM Flight Trajectory Characteristics Analysis, Korea National Defense University, pp. 44-45, 2010.
9 Harlin, W. J. and Cicci, D.A., Ballastic Missile Trajectory Prediction Using a State Transition Matrix, Applied Mathematics and Computation, Vol. 188, pp. 1832-1847, 2007.
10 Roger R. Bate, Fundamentals of Astrodynamics, Department of Astronautics & Computer Science United States Air Force Academy, p. 13, 1971.
11 Suk-Bon Choi, Yong Soo Kwon, Analysis of Flight Trajectory Characteristics of Ballastic Missiles, Journal of the KIMST, Vol. 32, No. 1, p. 176, 2006.
12 C. H. Jung, An Optimal Missile Allocation Problem for Maximizing Kill Probability, Journal of the Korean Operations Research & Management Science Society, Vol. 27, No. 1, 2006.