• Title/Summary/Keyword: Future Missile

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A Implementation of Command and Control Simulator System for Missile System (유도무기 사격지휘통제 시뮬레이터 시스템 구현)

  • Yi, Jeong-Hoon;Kim, Ki-Bum;Rhee, Chang-Lim;Jun, Jung-Hee;Koo, Bong-Joo
    • Journal of the Korea Institute of Military Science and Technology
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    • v.14 no.4
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    • pp.556-563
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    • 2011
  • Recently, the development of military system is focused on Network Centric Warfare. But, there is no deployed Command and Control System for Missile System in the country. Therefore, Command and Control System for Missile System was simulated to predict feasibility for the future development in this paper. The contents of the design and implementation for simulated system are described in details. Besides, a method for avoiding collisions in 1:N radio communication environment is proposed as the future work. The simulated system in this paper will be a help to developing Command and Control System for Missile System in the future.

Investigation of Missile Propulsion Technologies Necessary for Future Warfare Environment and The Role of Incorporations (미래전장환경에 필요한 유도무기 추진기술 고찰 및 산업체의 역할)

  • Moon, Soon-Il
    • Proceedings of the Korean Society of Propulsion Engineers Conference
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    • 2010.11a
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    • pp.515-518
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    • 2010
  • This technical paper presents future missile trends and propulsion technologies necessary for the missiles. The views are based on open literature briefings of the United States and internet informations. These informations let domestic incorporations prepare technologies for the future. Political and economical environment has been changing worldwidely. More extensive role is required for the incorporations to increase the economic growth of our country. The incorporations should establish the long term product development strategy of their own to compete with foreign countries.

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Development of Augmentation Method of Ballistic Missile Trajectory using Variational Autoencoder (변이형 오토인코더를 이용한 탄도미사일 궤적 증강기법 개발)

  • Dong Kyu Lee;Dong Wg Hong
    • Journal of the Korean Society of Systems Engineering
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    • v.19 no.2
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    • pp.145-156
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    • 2023
  • Trajectory of ballistic missile is defined by inherent flight dynamics, which decided range and maneuvering characteristics. It is crucial to predict range and maneuvering characteristics of ballistic missile in KAMD (Korea Air and Missile Defense) to minimize damage due to ballistic missile attacks, Nowadays, needs for applying AI(Artificial Intelligence) technologies are increasing due to rapid developments of DNN(Deep Neural Networks) technologies. To apply these DNN technologies amount of data are required for superviesed learning, but trajectory data of ballistic missiles is limited because of security issues. Trajectory data could be considered as multivariate time series including many variables. And augmentation in time series data is a developing area of research. In this paper, we tried to augment trajectory data of ballistic missiles using recently developed methods. We used TimeVAE(Time Variational AutoEncoder) method and TimeGAN(Time Generative Adversarial Networks) to synthesize missile trajectory data. We also compare the results of two methods and analyse for future works.

A Study of the Safety Assessment for Combustion Products in the Exposure Human Bodies Rounding Missile Ejection (유도탄 사출시 연소 생성물의 인체 안전성 평가에 관한 연구)

  • Song, Kee Hyeok;Chung, Sung-Hak
    • Journal of Korean Society of Industrial and Systems Engineering
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    • v.37 no.4
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    • pp.269-273
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    • 2014
  • The objective of this study is to safety assessment for human body on the guided missile combustion products. This study is to verify the safety assessment when operating the interior missile ejection take on verify the safety of the human body. During the missile ejection of combustion products, this study is analyzed combustion products. Result are accepted NIOSH and KOSHA of the safe guideline, and 6 exposure gas to the specified values 42% (CO), 22% ($CO_2$), not detected (others) are within minimal exposures criteria of the reference value respectively. Contribution of these results supported that interior missile ejection during combustion products may have been ensured human safely. Therefore, the future for improving the environmental safety of the shooting projectile steel plate round, dust collector, ventilation and other facilities is to improve environmental safety and efficient renovated design needed by target focused areas.

Threat Assessment of Anti-Ship Ballistic Missile (ASBM) of North Korea (북한 대함탄도미사일 위협 분석)

  • Park, Younghan;Oh, Kyungwon;Kim, Jiwon
    • Journal of Aerospace System Engineering
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    • v.10 no.3
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    • pp.1-8
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    • 2016
  • This paper provides an empirical assessment of the development of North Korea's Anti-Ship Ballistic Missile (ASBM), and its influence on South Korea's maritime strategy. While research studies on North Korea's ballistic-missile capabilities and South Korea's ballistic-missile defense systems are proliferating, less analytical attention has been given to the way that the strengthening of North Korea's ballistic-missile capacities presents a critical threat to the ROK's navy and lines of communication. The authors of this paper identify the continuing development of unique ASBM capabilities by China and Iran, and determine that such processes are mutually interactive and in accordance with threat perceptions; furthermore, North Korea can enact the same process by learning lessons from these nations. The findings of this paper provide an implication for the formulation of South Korea's maritime strategy and the related assets in consideration of the ASBM as a future threat.

The operational concept of the network based future airborne force power (네트워크 기반 미래 공중전력 운용개념)

  • Kim, Jong Yoel;Kwon, Yong Soo;Kim, Yun Kyu
    • Journal of the Korean Society of Systems Engineering
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    • v.4 no.2
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    • pp.45-54
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    • 2008
  • This paper describes an operational concept of the network based future airborne force power using a systems engineering approach. The battlefield is changing to new system of systems that command and control by the network based BM/C4ISR. Also, it is composed of various sensors and shooters in an single theater. Future threats may be characterized as unmanned moving bodies that the strategic effect is great such as UAVs, cruise missile and tactical ballistic missiles. New threats such as low altitude stealth cruise missile may also appear. The implementation of future airborne force power network systems against these future threats is required to complex and integrated approach based on systems engineering. This work developed the operational concepts of the future airborne network system, and then derived the requirements for performing missions effectively. In addition, the scheme of future airborne force power network systems is presented.

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A Case Study on Reliability Growth Analysis for a missile System composed of All-Up-Round Missile and Launcher (유도탄 및 발사체계로 구성된 유도무기체계의 신뢰도 성장 분석 사례 연구)

  • Jo, Boram
    • Journal of the Korea Academia-Industrial cooperation Society
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    • v.20 no.2
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    • pp.329-335
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    • 2019
  • Reliability growth analysis was conducted for a guided weapons system. In the development phase, reliability management activities were continuously carried out by identifying failure modes and causes and analyzing faults found during the testing. The missile system consists of an all-up-round missile and a launcher, and the analysis was carried out according to the test results of each system. The test results for the all-up-round missile were obtained with discrete data, which were success and failure as a one-shot-device. The test results for the launcher were obtained with continuous data by operating the equipment continuously in the test. For each test result, the reliability growth model was applied to the Standard Gompertz model and the Crow-Extended model. The models were used to identify the growth analysis results of the test so far. It was also possible to predict the reliability growth results by assuming the future test results. The study results could be useful in achieving the desired reliability goal and in determining the number of tests. Then, the planned test will be confirmed and the growth analysis of the missile system will continuously be conducted.

IP를 이용한 패트리어트 미사일 최적배치모형

  • Lee, Jae-Yeong;Jeong, Chi-Yeong
    • Proceedings of the Korean Operations and Management Science Society Conference
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    • 2005.10a
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    • pp.38-50
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    • 2005
  • The current Air defense missile, Nike, will be replaced by the Patriot missile in the near future. In this paper, we developed an optimal allocation model for the Patriot missile. In order to formulate the model, we applied a set covering and If model. This model considers not only weapon's characteristics and performances but also the threat of enemy aircrafts and SCUD missiles. When we apply this model, we can find the optimal location of Patriot batteries which maximizes the kill probability of enemy aircrafts and SCUD missiles attacking vital area of our forces. This model can directly be used to the decision making for the optimal military facility allocation.

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Concept and Employment Status of EPAA(European Phased Adaptive Approach) (EPAA(European Phased Adaptive Approach) 개념과 구축 현황)

  • Moon, Suk-hyun;Kim, Young-deuk;Park, Tae-yong
    • Proceedings of the Korean Institute of Information and Commucation Sciences Conference
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    • 2015.10a
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    • pp.586-588
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    • 2015
  • U.S. is constructing EPAA(European Phased Adaptive Approach) as a part of BMDS(Ballistic Missile System). The purpose of EPAA is to protect European NATO territory from Iranian ballistic missile threats. EPAA project consists of three phase, $1^{st}$ phase is completed as deploying transportable forces such as aegis BMD ships at the mediterranean, and $2^{nd}$ phase is on going. In this paper, the concept, characteristics, current status and future works of EPAA are surveyed and described.

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Study on Methods in Test & Evaluation of the Guided Rocket Munition (유도형 로켓탄의 시험평가 방법에 관한 연구)

  • Ahn, Mahn-Ki;Kwon, Tag-Mahn;Hwang, Un-Hee;Hwang, Woo-Yull
    • Journal of the Korea Institute of Military Science and Technology
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    • v.13 no.6
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    • pp.1019-1025
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    • 2010
  • This paper describes on methods in test and evaluation of the guided rocket munitions of the domestic new generation multiple launcher rocket system. We modified and refer to the present model of air-to-air missile(AAM) and surface-to-air missile(SAM). Also we suggested a method of surface-to-surface missile(SSM) based on the characteristics of the guided rocket in test and evaluation(T&E). According to this study, the suggested activity of T&E should be observed methods compatible with each item on the established model. Therefore, we expect that the proposed research material will be a good guide to the study of a surface-to-surface missile(SSM) installed GPS/INS integration navigation guidance & control systems in the future.