• Title/Summary/Keyword: Guided Weapons

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Inspection of guided missiles applied with parallel processing algorithm (병렬처리 알고리즘 적용 유도탄 점검)

  • Jung, Eui-Jae;Koh, Sang-Hoon;Lee, You-Sang;Kim, Young-Sung
    • Journal of Advanced Navigation Technology
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    • v.25 no.4
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    • pp.293-298
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    • 2021
  • In general, the guided weapon seeker and the guided control device process the target, search, recognition, and capture information to indicate the state of the guided missile, and play a role in controlling the operation and control of the guided weapon. The signals required for guided weapons are gaze change rate, visual signal, and end-stage fuselage orientation signal. In order to process the complex and difficult-to-process missile signals of recent missiles in real time, it is necessary to increase the data processing speed of the missiles. This study showed the processing speed after applying the stop and go and inverse enumeration algorithm among the parallel algorithm methods of PINQ and comparing the processing speed of the signal data required for the guided missile in real time using the guided missile inspection program. Based on the derived data processing results, we propose an effective method for processing missile data when applying a parallel processing algorithm by comparing the processing speed of the multi-core processing method and the single-core processing method, and the CPU core utilization rate.

A Study of Separation Mechanism in Ball Type Separated Bolt (볼타입 분리볼트의 분리현상 연구)

  • Lee, Yeung-Jo;Koo, Song-Hoe;Jang, Hong-Bin;Lee, Bang-Eop
    • Journal of the Korean Society of Propulsion Engineers
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    • v.15 no.2
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    • pp.62-67
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    • 2011
  • Launching tube is a kind of case to protect the guided weapons from external environments and conducted as a guide when they are fired. The guided weapons have been firmly kept at the launching tube and transferred, and would be separated at the required time when they are fired To meet the aim, it has been used explosive bolts which are reliable and efficient mechanical fastening devices having the special feature of a built-in release. The disadvantage of explosive bolt lies in that it is based on the high explosive effect of a pyrotechnic charge. When the explosive bolt is ignited, there are some bad effects; a flame, fragments and pyro-shock. Because of these bad effects there are many restriction to use bolt as joining devices to precision guided weapons. To solve these problems, the aim of the present work is to invent the ball-type separation bolt which is a pyrotechnically releasable mechanical linking device for two mechanical elements that does not suffer from such drawbacks. A standard pressure cartridge can moreover be easily integrated inside the device according to the present work and this with no modification to its structure. The present work was represented quantitatively the margin of separation safety and analysed separation mechanism in ball type separating bolt to perform the dynamic separation test.

A study on the Diminishing Manufacturing Source and Material Shortages Management and Cost Analysis based on Pilot Application of the Guided Weapons (부품단종관리 방안 및 유도무기 시범적용을 통한 비용분석)

  • Park, Kwang-Hyo;Shim, Bo-Hyun
    • Journal of the Korea Academia-Industrial cooperation Society
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    • v.21 no.3
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    • pp.390-398
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    • 2020
  • To solve the problem of frequent component failure in guided weapons, a process of component failure in developed countries was investigated and analyzed. The suitability of component control, including risk assessment, analysis of operational impact, and the establishment of response measures, was also demonstrated. In addition, the economic effects of component control were presented by estimating the costs incurred if component control is performed in advance, after-sales, and non-management. DMSMS problems refer to losses or impending losses of an item, raw material, or software manufacturer or supplier. A problem with the discontinuation of parts occurs when the manufacturer or supplier ceases to produce and support the necessary parts, materials, or software, or when the supply of raw materials is no longer possible. Hence, it is important to recognize that failure to all parts of the system can occur.

Transient heat transfer analysis of inertial measurement devices by outside frictional heat (외부 마찰열에 의한 내부 관성측정장치의 과도 열전달 해석)

  • Tak, Seungmin;Park, Jiwon;Kang, Minkyu;Park, Dongjin;Lee, Jongsu;Lee, Seoksoon
    • Journal of Aerospace System Engineering
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    • v.4 no.1
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    • pp.32-37
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    • 2010
  • Guided weapon is very excellent strategy system than conventional weapons. Recently, several devices and a technology developed much developing more, inertia measuring device is one example. Inertia measuring device is device that is used to improe more accuracy of guided weapon, this device is operated by sensors of inside. Sensors of inside are parts that is very sensitive about impact or shock, heat that interact when shoot, it is main purpose that verify durability of sensor by heat delivered from outside in this study.

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Analysis of Anti-jamming for GPS Guided Missile by GPS Reception Azimuth Control (GPS 수신 방위각 제어를 통한 GPS 유도무기 재밍대응 분석)

  • Choi, Chang-Mook
    • Journal of the Korea Institute of Information and Communication Engineering
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    • v.20 no.3
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    • pp.677-682
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    • 2016
  • Recently, because Global Positioning System (GPS) achieves accuracy for engagement of enemy targets, GPS guided weapons have a wide range of applications from land through sea to air. Especially, when GPS guided weapon is then launched, it reads current position and searches a course to the target. As we all know, because GPS signals are weak, these signals can be affected by interference. If jamming signal is strong enough, it can jam the receiver of GPS guided weapon. Therefore, anti-jamming technique is an important thing under these conditions. In this paper, the controlling azimuth angle was used to improve navigation performance of precision guided missile under jamming conditions. First of all, precision missiles by GPS positioning such as SLAM-ER and JDAM were investigated. Also, the azimuth cutoff angle of satellites for usable navigation under jamming signals was analyzed by experimental tests. As a result, we found that azimuth cutoff angle under 140 degree can help ensure continuous GPS reception under the missile guidance.

Study on the Performance Evaluation of the Explosive Bolt that has been Natural Aging (자연 노화된 폭발볼트의 성능 평가에 관한 연구)

  • Kim, Dongjin;Jeong, Donghee;Lee, Yeungjo;Lee, Youngwoo
    • Journal of the Korean Society of Propulsion Engineers
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    • v.21 no.3
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    • pp.84-90
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    • 2017
  • Explosive bolt is coupled in a variety of guided weapons and space projectiles, to perform the separation function. Thus, the role of the explosive bolt in guided weapons systems is very important, as it can cause failure of the entire system in the case of mission failure. For this reason, the design life prediction for explosive bolt is highly and frequently required recently, but its accurate prediction method has not been presented. In order to apply the existing accelerated aging process, we should know the activation energy and the acceleration factor of the explosive bolt. Since the information required for accelerated aging is not presently secured, it is difficult to predict the design life of explosive. Thus, in the present study, we have evaluated the performance of actual explosive bolts in the condition of natural aging over 10 years in order to present a minimum design life.

Development and Evaluation of Large Scale Composite Lattice Structures (대형 복합재 격자구조체 개발 및 평가)

  • Kim, Donggeon;Doh, Youngdae;Kim, Gensang;Kim, Myungjoo;Lee, Sangwoo
    • Journal of the Korean Society of Propulsion Engineers
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    • v.25 no.6
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    • pp.74-86
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    • 2021
  • The composite lattice structure is a structure that supports the required load with the minimum weight and thickness. Composite lattice structure is manufactured by the filament winding process using impregnating high-strength carbon fiber with an epoxy resin. Filament winding process can laminate and manufacture only structurally necessary parts, composite lattice structure can be applied to aircraft fuselages, satellite and launch vehicles, and guided weapons to maximize weight reduction. In this paper, the development and evaluation of the composite lattice structure corresponding to the entire process from design, analysis, fabrication, and evaluation of large-scale cylindrical and conical composites lattice structure were performed. To be applicable to actual projectiles and guided weapons, we developed a cylindrical lattice structure with a diameter of 2,600 mm and a length of 2,000 mm, and a conical lattice structure with an upper diameter of 1,300 mm, a lower diameter of 2,500 mm, and a length of 900 mm. The performance of the developed composite lattice structure was evaluated through a load test.

Operational Reliability Analysis of Guided Weapon Systems (유도무기 시스템의 운용 신뢰도 분석)

  • Ha, Ju Seok;Kim, Kyung Mo
    • Convergence Security Journal
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    • v.17 no.3
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    • pp.95-101
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    • 2017
  • Reliability is the priority matter in guided weapon systems. The reliability prediction data is used during the devel opment stage as the manufacturing cost is very high and the production quantity if quite limited. At the same time it takes relatively a long period of time to acquire a reliable operation data set after deployment such that in order t o determine the operational reliability, weapons must be tested and analyzed in real operating environments. For the research, the life distributions were estimated by using actual operation data and the reliability was calculated by ap plying the method of least squares and maximum likelihood estimation. Also, the comparisons were made between pr edicted reliability and actual operational reliability. As a result, the actual reliability of each system was higher than predicted reliability and it was considered that such a difference was caused by the fact that the application of the l atest designing technology and improved parts to the guided weapon systems was not reflected on the estimation of predicted reliability. It was possible to confirm the actual operational reliability of domestic (ROK) guided weapon sy stems through this research and the methods used here will contribute to the reliability analyses for the future guide d weapon systems to be developed.

A Study on the Evaluatioin Methods for the Rear Safety Zone of Portable Guided Missile (휴대용 유도탄의 후방 안전영역 평가방법에 관한 연구)

  • Song, Kee-Hyeok;Kang, Woo-Ram;Park, Jong-Ho
    • Journal of the Korean Society of Safety
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    • v.30 no.2
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    • pp.63-69
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    • 2015
  • Recoilless weapons, which lead strong back blast and impulse noise more than 160 dB, have been used in compliance with the regulation of the safety zone for the safe operations. However, the safety zone regulations for the newly developed weapons should be prepared since the existing guidelines do not provide any information concerning the reason for the safety zone. In this study, the outdoor launch tests were performed to collect the data such as noise, pressure and temperature of the back blast. An assessment method using data obtained from launch tests has been proposed to determine the safety zone. The safety zone has been determined with consideration for the following criteria: Impulse noise, temperature and pressure of the back blast and blast angle. As a results, new safety zones for them have been established for the recoilless weapon developed by ADD (Agency for Defense Development). We expect that this research can be used as a guideline for establishing a new safety zone regulation of similar weapon to be developed.