• 제목/요약/키워드: missile defense

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A Study on the Militarization of Artificial Intelligence Technology in North Korea and the Development Direction of Corresponding Weapon System in South Korea (북한 인공지능 기술의 군사화와 우리 군의 대응 무기체계 발전방향 연구)

  • Kim, Min-Hyuk
    • Journal of Information Technology Services
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    • v.20 no.1
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    • pp.29-40
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    • 2021
  • North Korea's science and technology policies are being pursued under strong leadership and control by the central government. In particular, a large part of the research and development of science and technology related to the Fourth Industrial Revolution in North Korea is controlled and absorbed by the defense organizations under the national defense-oriented policy framework, among which North Korea is making national efforts to develop advanced technologies in artificial intelligence and actively utilize them in the military affairs. The future weapon system based on AI will have superior performance and destructive power that is different from modern weapons systems, which is likely to change the paradigm of the future battlefield, so a thorough analysis and prediction of the level of AI militarization technology, the direction of development, and AI-based weapons system in North Korea is needed. In addition, research and development of South Korea's corresponding weapon systems and military science and technology are strongly required as soon as possible. Therefore, in this paper, we will analyze the level of AI technology, the direction of AI militarization, and the AI-based weapons system in North Korea, and discuss the AI military technology and corresponding weapon systems that South Korea military must research and develop to counter the North Korea's. The next study will discuss the analysis of AI militarization technologies not only in North Korea but also in neighboring countries in Northeast Asia such as China and Russia, as well as AI weapon systems by battlefield function, detailed core technologies, and research and development measures.

Cumulative control output compensation technique for voice coil actuator used in small guided missiles (소형 유도무기용 보이스 코일 구동장치의 누적 제어 출력 보상 기법)

  • Wonsung Lee;Gwang Tae Kim;Choonghee Lee;Yongseon Lee;Seungho Jeong;Sungho Choi
    • Journal of Aerospace System Engineering
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    • v.18 no.4
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    • pp.1-9
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    • 2024
  • In this study, we researched control compensation techniques to enhance control robustness against external forces and responsiveness to output dead zones in direct-actuated voice coil actuators for small guided missiles. An aircraft's wings must optimally control the command angle while managing various nonlinear external forces such as drag, lift, and thrust during flight. The small direct -drive voice coil actuator, when applied, benefits from small current requirements in no-load situations but suffers from diminished control robustness due to rapid increases in control current during external force applications. To address this issue, we designed and implemented a system that compensates for errors by accumulating additional output, thus improving the actuator's responsiveness in control scenarios with external forces. This was verified through experimental results.

A Study on the Effect of Design Reliability and Periodic Inspection Cycle on Storage Reliability : Focusing on One-shot Logistic Equipment System (설계신뢰도 및 정기검사주기가 저장신뢰도에 미치는 영향에 관한 연구 : 일회성 군수장비 시스템을 대상으로)

  • Chu, Yeon-Won
    • Journal of the Korea Convergence Society
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    • v.9 no.7
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    • pp.223-230
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    • 2018
  • In the case of a one-shot logistic equipment system that has been stored for a long time, reliability changes with the passage of time. Therefore, when the time comes to use, the storage reliability of the product is an important quality characteristic, and the existing studies have focused on the research for calculating the optimal period inspection cycle to improve the storage reliability. In this study, we analyzed the influence of the two factors on the storage reliability at the convergence point by analyzing the design reliability as well as the periodic inspection cycle. To do this, we applied the existing Martinez storage reliability model to the missile, a representative product of a one-shot system, and analyzed the quantitative effects of the design reliability and the periodic inspection cycle. From the results of the analysis, it was confirmed that the maintenance of the periodic inspection cycle is more important for the improvement of the storage reliability than the design reliability in the design reliability category of the current product.

Analysis of the Flight Trajectory Characteristics of North Korea SLBM (북한 SLBM의 비행특성 해석)

  • Lee, Kyoung-Haing;Seo, Hyeong-Pil;Kwon, Yong-Soo;Kim, Jiwon
    • Journal of the Korea Society for Simulation
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    • v.24 no.3
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    • pp.9-16
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    • 2015
  • This research focuses on analysis of the flight trajectory characteristics of SLBM (Submarine Launched Ballistic Missile) of North Korea. Recently, North Korea tested launching of SLBM which is threatening international security. Also it is known that North Korea had possessed the technologies about SLBM since they disassembled submarines out of commission of the former Soviet Union. If the development of the SLBM of North Korea is completed, it should be affected as asymmetric threat to South Korea. Therefore, for active respondence to these threat, it is essential to analyze the SLBM systematically. In this point of view, this work made a SLBM flight model and simulated. In addition, we controled flight trajectories according to adjusting loft angle and described their characteristics. The sea-based ballistic missile defense system is required for an effective response to the flight trajectory of the SLBM from mid-course to terminal phase.

Optimization of Voice Coil Motors for a Small Guided Missile Fin Actuator (소형 유도무기 날개 작동기용 보이스 코일 모터의 최적 설계)

  • Lee, Choong Hee;Kim, Gwang Tae;Lee, Byung Ho;Cho, Young Ki
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.47 no.1
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    • pp.59-65
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    • 2019
  • In this study, optimal design of direct-drive VCMs (Voice Coil Motor) for a missile fin actuator is carried out. The torque performance and the characteristics of the VCM are predicted by commercial electromagnetic analysis software, ANSYS Maxwell. The optimal design is obtained at the minimum and maximum actuating angles where the aerodynamic load acting on the fin is the largest in the operating range. The critical variables of the actuator is designed and the RSM (Response Surface Method) is used for the optimization. The response surface model consists of second-order functions and its experimental points are selected by a central composite design. This design is widely used for fitting a second-order response surface. The adjustment regression coefficients is computed for adequacy checking of the response surface model. Finally, the torque values obtained by the RSM and the ANSYS Maxwell are shown in good agreement.

Analysis of Aerodynamic Characteristics for Guided Gliding Type Ammunition Using Computational Analysis and Wind Tunnel Test (전산해석 및 풍동시험을 이용한 유도형 활공탄약의 공력해석)

  • Bang, Jae Won
    • Journal of the Korea Society for Simulation
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    • v.28 no.1
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    • pp.49-56
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    • 2019
  • In this study aerodynamic characteristics of guided gliding type ammunition were investigated by using a computational analysis and wind tunnel test. Missile DATCOM, a semi-empirical method, and a FLUENT, a computational fluid dynamics analysis program, were used for computational analysis. For a guided gliding type ammunition, aerodynamic characteristics were investigated by calculating lift force, drag force, pitching moment and etc. Aerodynamic characteristics of guided gliding type ammunition are completely different from those of conventional ammunition. The results obtained from the computer analysis are similar to those obtained from the wind tunnel test. Although the pitch moment values obtained by the semi-empirical method were slightly different from the wind tunnel test results, the overall computer analysis results showed trends and values similar to the test results. In this study, aerodynamic characteristics of guided gliding type ammunition were identified and it found that semi-empirical method can be applied to analyze the aerodynamic characteristic in the initial design of guided gliding ammunition.

A Study of Multi-to-Majority Response on Threat Assessment and Weapon Assignment Algorithm: by Adjusting Ballistic Missiles and Long-Range Artillery Threat (다대다 대응 위협평가 및 무기할당 알고리즘 연구: 탄도미사일 및 장사정포 위협을 중심으로)

  • Im, Jun Sung;Yoo, Byeong Chun;Kim, Ju Hyun;Choi, Bong Wan
    • Journal of Korean Society of Industrial and Systems Engineering
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    • v.44 no.4
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    • pp.43-52
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    • 2021
  • In weapon assignment studies to defend against threats such as ballistic missiles and long range artillery, threat assessment was partially lacking in analysis of various threat attributes, and considering the threat characteristics of warheads, which are difficult to judge in the early flight stages, it is very important to apply more reliable optimal solutions than approximate solution using LP model, Meta heuristics Genetic Algorithm, Tabu search and Particle swarm optimization etc. Our studies suggest Generic Rule based threat evaluation and weapon assignment algorithm in the basis of various attributes of threats. First job of studies analyzes information on Various attributes such as the type of target, Flight trajectory and flight time, range and intercept altitude of the intercept system, etc. Second job of studies propose Rule based threat evaluation and weapon assignment algorithm were applied to obtain a more reliable solution by reflection the importance of the interception system. It analyzes ballistic missiles and long-range artillery was assigned to multiple intercept system by real time threat assessment reflecting various threat information. The results of this study are provided reliable solution for Weapon Assignment problem as well as considered to be applicable to establishing a missile and long range artillery defense system.

Mark XIIA(Mode 5) IFF System Integration and Certification Test for Surface to Air Missile System (유도무기체계 모드 5 피아식별 체계통합 및 인증시험)

  • Kim, Woo-Hyun;Jung, Se-Young;Lee, Yun-Soo;Chang, Se-Myong
    • Journal of the Korea Institute of Military Science and Technology
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    • v.25 no.2
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    • pp.160-168
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    • 2022
  • The new IFF mode, Mode-5 replacing Mode-4, has already been established by the US DoD for its allies and NATO forces. A IFF retrofit program for replacing the Mark XII Mode-4 with Mark XIIA Mode-5 is in progress in order to overcome the security limitations of the former in R.O.K. IFF certification test for the new mode, Mode-5, has been performed on medium range surface to air missile platform of the Korean armed forces for the first time in R.O.K and this is regarded as a monumental event in Korean defense industry. The present paper is a discussion on the procedures applied to the IFF system retrofit and integration, lessons learned from AIMS test with the US AIMS PO as observer. The minimum modification from the existing Mark XII Mode-4 to Mark XIIA Mode-5 and evolutional adaption from previous design including interoperability are required for the system retrofit. Letter of Certification was received from the US AIMS PO after the tests. The authors propose that the lessons learned and know-how acquired during the tests are managed by the R.O.K Government as the standard structure of a database. It is expected that the use of the database will reduce the developmental difficulties and risk, also increase efficiency in future developments and other projects.

A Study on Inspecting Position Accuracy of DACS Pintle (위치자세제어장치의 핀틀 위치정확도 점검 방안 연구)

  • Tak, Jun Mo
    • Journal of Aerospace System Engineering
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    • v.15 no.3
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    • pp.57-64
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    • 2021
  • In the study, to minimize the error on guided control of the KV (Kill Vehicle) and to secure the hit-to-kill performance, a position accuracy inspection for the DACS (Divert and Attitude Control System) actuation system was proposed. The accuracy performance of the DACS actuation system is one of the most important factors in the interception of ballistic missiles. In order to validate actuation control accuracy of DACS system, an inspection item was set for position accuracy, and the inspection system was designed for DACS pintle. To measure the absolute position value of the DACS pintle, an external measurement system was developed using laser displacement sensors. The inspection system was designed so that it can be compared with the actuation command in real time. The proposed position accuracy inspection system can be inspected not only in a DACS system but also in missile system level. The position accuracy inspection was performed using the designed inspection system, and analysis of the inspection result.

Study on the Method to Improve a Maritime Safety by Analysing the Distribution Characteristics of the Ships on Marine Firing Range (해상사격장 선박분포 특성 분석을 통한 해상안전 개선방안에 대한 연구)

  • Baek, Sang Hwa;Lee, Ah Yoon;Park, Ho Jun;Lee, Woo Sung;Choi, Kye Soog
    • Journal of the Korean Society of Safety
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    • v.35 no.3
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    • pp.79-85
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    • 2020
  • Ahn-heung Proving Ground(APG) of Agency for Defense Development(ADD) is the only weapon test site which has been performing firing tests for many kinds of missile, artillery and ammunition. APG has been performing the firing tests of so many times every year. The tests related to missiles, artillery and ammunitions cover 80% among the quantity of annual test events. The target area of many kinds of missile, artillery and ammunition is on the sea. Therefore, APG has its marine firing ranges which were approved by the ministry of Defense. Both weapons and ships can run into each other on the sea. APG has to monitor and detect the positions of the ships in the specific dangerous zone on the sea. The positions of the ships are detected by Scanter 2001 radar and GPS100 detection radar. Evading the time period when the ships appear very often on the sea may be a good solution to keep the maritime safety. And evading the place where the ships appear very often on the sea may be a good solution as well. This paper is to analyze the ships' distribution characteristics of marine firing range, which are to raise the efficiency of many kinds firing tests which have been performed in APG of ADD. Ship distribution data from February 2014 to December 2016 were used in this paper. Ship distribution was analyzed with monthly data, seasonal data and etc. The number of the ships in approved sea area is higher in the morning than in the afternoon, and in fall than other seasons, and from August to November, and below 0.5 m in the hight of wave. Using the these conditions, we can raise the test efficiency of many kinds firing tests and guarantee maritime safety. The number of the ships in approved sea area is entirely unrelated to visibility of the sea. The time period when the number of the ships are high on the sea is morning. The season when the number of the ships are comparatively high on the sea is fall. APG of ADD could raise the efficiency of the firing tests and improve the maritime safety, using the analysis results of the characteristics on the ship distribution.