• Title/Summary/Keyword: guided bomb

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A Study OR the Cost-Effectiveness Analysis of Special Bomb (특수폭탄의 비용대 효과분석에 관한 연구)

  • Lee, Ching-Hoon
    • Journal of the military operations research society of Korea
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    • v.3 no.2
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    • pp.119-134
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    • 1977
  • The goal of this study is to determine which is the better bomb; a general purpose bomb or a special bomb, from the point of view of cost-effectiveness of air munitions. What we call the special bomb is a laser guided bomb which adds a guidance control unit on the head of a general purpose bomb. Althrough their characteristics of explosion are the same, their effectivenesses are very defferent due to their probability of hitting the targets. Now, in order to measure their relative a effectiveness, we could select various enemy targets such as runway, radar, and then Ive could also calculate requirments of both bombs and firghter aircraft sorties according to the desired damage level of each target, Following above steps, we can derive the total costs and compare effectiveness. As a results of this study, when the attrition rate of aircraft is under $1.1\%$, the general purpose bomb is better than the laser guided bomb. Above $1.1\%$ attrition rate, we could say that luser guided bomb is the most economical bomb.

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Computation of Launch Acceptability Region of Air-to-Surface Guided Bomb for Moving Target (이동표적에 적용 가능한 공대지 유도폭탄의 투하 가능 영역)

  • Kang, Yejun
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.49 no.7
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    • pp.601-608
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    • 2021
  • Launch Acceptability Region of Air-to-Surface Guided Bomb is defined as the set of release points in order to reach a target successfully. LAR is consisted of fixed target area and moving target area whether the target maneuvers or not. In this paper, the computational algorithm of LAR is studied for fixed and moving target. First, multi-simulations are performed varying platform, target, and atmospheric environment to attain Min/Max DB. Second, the LAR functions are obtained using regression and classification algorithm. For operational suitability, the algorithm for display of LAR is studied to obtain appropriate LAR. In this progress, the results of LAR are suitable to apply air-to-ground guided bomb for moving target.

Development of Guidance Control Module for GPS Guided Bomb (GPS 유도 폭탄용 유도조종모듈 개발)

  • Lim, Heung-Sik;Yoon, Hyung-Sik
    • Journal of the Korea Institute of Military Science and Technology
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    • v.14 no.5
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    • pp.774-780
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    • 2011
  • The guidance control module is needed for control of a GPS guided bombs to improve the accuracy and availability of a conventional bomb. In this paper, we present the development of hardware design, software design and test environments of it. And we also show the process of the tests and the results verifying and proving for its required functions and performances through ground tests and flight tests.

Developing an Algorithm to Calculate Launch Acceptability Region of Air-to-Ground Guided Bomb (공대지 유도폭탄 투하 가능 영역 계산 알고리즘 개발)

  • Seo, Jeong Jae
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.45 no.6
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    • pp.517-522
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    • 2017
  • Launch Acceptability Region(LAR) is a region for an aircraft which carries air-to-ground guided bombs to enter such that it can successfully hit the target. LAR should consider the release condition of an aircraft, impact condition for targets, and environmental condition of atmosphere. In this paper, LAR algorithm was developed using the database of many simulations which were varied by inputs, such as the release, impact, and environmental conditions. The algorithm was tested through the direct simulation results, and found that it was suitable to apply as LAR for air-to-ground guided bomb.

On an Air-To-Sea Guided Bomb

  • Takano, Hiroyuki;Baba, Yoriaki;Takao, Kichiro
    • 제어로봇시스템학회:학술대회논문집
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    • 1993.10b
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    • pp.462-467
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    • 1993
  • Even nowadays ships on the sea are important strategic base for aircraft and missiles. Thus we have been studying an unmanned attack system against ships recently. We experienced severa problems when this system was simulated on the computer. In this paper, problems and solutions of an Air-To-Sea Guided Bomb for this system are presented.

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Computation for Launch Acceptability Region of Air-to-Surface Guided Bomb Using Artificial Neural Network (인공신경망을 이용한 공대지 유도폭탄의 투하가능영역 산출)

  • Kim, Seonggyun;Park, Jeongho;Park, Sanghyuk;Lee, Seoungpil;Kim, Kilhun
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.46 no.4
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    • pp.283-289
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    • 2018
  • Launch Acceptability Region(LAR) means an area for successfully hitting the target. And LAR should be calculated in real time on aircraft so that LAR can be seen by pilot. LAR can be changed by the launch condition of the bomb, the impact condition of the target, and the atmospheric condition at the time of flight of the bomb. In this paper, we propose the calculation method of LAR using Artificial Neural Network(ANN). The learning data was generated by changing each condition from existing LAR model, and LAR model was derived through ANN learning. We confirmed the accuracy of the new LAR model by comparing the difference between the result data of existing LAR model and the new LAR model. And we confirmed the possibility of real time calculation of the LAR model on the aircraft by comparing the calculation time.

Van Test for GAK NM (GPS Adapter Kit Navigation Module) Using High Performance INS (고정밀 INS를 이용한 GAK(GPS Adapter Kit) 항법 모듈의 차량 시험)

  • Oh, Sang-Heon;Son, Seok-Bo;Kwon, Seung-Bok;Shin, Don-Ho;Lee, Sang-Jeong;Park, Chan-Sik;Hwang, Dong-Hwan
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.35 no.3
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    • pp.260-267
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    • 2007
  • GPS adapter kit (GAK) is a GPS/INS guided range extension system to improve the accuracy and availability of existing dumb bombs. In this paper, a van test result of GPS/INS navigation module (NM) for guided bomb with GAK has been presented. The NM consists of a commercial MEMS IMU, embedded GPS receiver and navigation computer unit (NCU). The GPS receiver of NM was designed to use multiple antennas for satellite visibility and GPS attitude determination. The real-time navigation software was designed by modularized structure to guarantee the maintainability and extensibility. In order to evaluate the performance of the NM, a van test was preformed by using a high performance INS - Honeywell H-726 MAPS(Modular Azimuth Position System).The van test results show that the GAK NM with GPS attitude measurement gives better navigation performance than a conventional GPS/INS integration and good coasting capabilities under jamming environment.

Hit Rate Prediction Algorithm for Laser Guided Bombs Using Image Processing (영상처리 기술을 활용한 레이저 유도폭탄 명중률 예측 알고리즘)

  • Ahn, Younghwan;Lee, Sanghoon
    • KIISE Transactions on Computing Practices
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    • v.21 no.3
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    • pp.247-256
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    • 2015
  • Since the Gulf War, air power has played a key role. However, the effect of high-tech weapons, such as laser-guided bombs and electronic optical equipment, drops significantly if they do not match the weather conditions. So, aircraft that are assigned to carry laser-guided bombs must replace these munitions during bad weather conditions. But, there are no objective criteria for when weapons should be replaced. Therefore, in this paper, we propose an algorithm to predict the hit rate of laser-guided bombs using cloud image processing. In order to verify the accuracy of the algorithm, we applied the weather conditions that may affect laser-guided bombs to simulated flight equipment and executed simulated weapon release, then collected and analyzed data. Cloud images appropriate to the weather conditions were developed, and applied to the algorithm. We confirmed that the algorithm can accurately predict the hit rate of laser-guided bombs in most weather conditions.

Development of MEMS-IMU/GPS Integrated Navigation System

  • Kim, Jeong Won;Nam, Chang Woo;Lee, Jae-Cheul;Yoon, Sung Jin;Rhim, Jaewook
    • Journal of Positioning, Navigation, and Timing
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    • v.3 no.2
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    • pp.53-62
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    • 2014
  • In the guided missile and unmanned vehicle system, the navigation system is one of the most important components. Recently, low-cost effective smart projectiles and guided bomb are being developed using MEMS based navigation system which has high-G, low-cost and small size. In this paper, locally developed MEMS based GPS/INS integrated navigation system will be introduced in comparison with the state of the art of MEMS based navigation system. And technical design and development method is described to satisfy the required performance of GPS receiver, MEMS inertial sensor assembly, navigation computer and software.

GPS 유도 폭탄용 복합 항법 모듈의 비행 시험

  • O, Sang-Heon;Son, Seok-Bo;Gwon, Seung-Bok;Sin, Dong-Ho
    • Proceedings of the Korean Institute of Navigation and Port Research Conference
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    • v.2
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    • pp.447-450
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    • 2006
  • 최근 국내외에서 재래식 폭탄의 정확도와 사거리를 향상시킨 정밀 유도 무기에 관한 연구가 활발하게 진행 중에 있다. 국내에서는 국방과학연구소의 주도로 재래식 폭탄에 GAK(GPS Adapter Kit)를 장착하는 연구가 진행 중이다. GAK는 GPS/INS 복합 항법 모듈을 내장한 사거리 연장 유도 키트의 일종으로 폭탄이 투하되면 접혀 있던 날개가 전개되고 이후 날개의 플래퍼론을 구동하여 유도 조종을 수행한다. 복합 항법 모듈은 상용의 MEMS IMU, 내장형 GPS 수신기 및 항법 컴퓨터와 실시간 운영 체제에서 구동되는 항법 소프트웨어로 구성된다. 본 논문에서는 복합 항법 모듈의 비행 시험 결과를 제시하였다. 시험 결과 항법 모듈이 실시간으로 정상적인 동작을 수행하였으며 GPS 유도 폭탄의 유도 조종에 적합한 항법 정보를 제공하였음을 확인하였다.

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