• Title/Summary/Keyword: 유도폭탄

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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.

Design of a Guidance Kit for Air-to-Surface Bomb (공대지 폭탄용 유도키트 설계)

  • Lee, Dae-Yeol;Lee, In-Won;Joe, Jae-Ho;Kim, Yong-Bin;Ju, Hyun-Jun;Jung, Na-Hyeon;Park, Jun-Sung
    • Journal of the Korea Institute of Military Science and Technology
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    • v.16 no.6
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    • pp.733-738
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    • 2013
  • A guidance kit transforming a general purpose bomb into an air-to-surface gliding bomb was developed. This guidance kit consists of a flight kit and a tail kit. Flight kit contains deployable wing, GPS/INS integrated navigation system, guidance and control system. Also this guidance kit was designed to use neither electrical nor mechanical interface with aircraft, and to increase dramatically the survivabilities of pilot and aircraft with the high accuracy and the mid-range non-powered gliding capability.

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.

A Study on HILS for Performance Analysis of Airborne EOTS for Aircraft (항공기용 EOTS 성능분석을 위한 HILS시스템 구축에 관한 연구)

  • Chun, Seungwoo;Baek, Woonhyuk;La, Jongpil
    • Journal of the Korea Society of Computer and Information
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    • v.18 no.12
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    • pp.55-64
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    • 2013
  • In this paper, the HILS (Hardware In-the-Loop Simulation) system to analyze and to verify the performance of the targeting pod is addressed. The main functions of the targeting pod is acquiring and tracking targets to guide a LGB (Laser Guided Bomb) to the targets. For the analysis of targeting pod, the real time simulate images generation of IR and daylight cameras, sever control technology, and the analysis of laser transfer characteristics are necessary. For the real time image generation and the laser transfer characteristics analysis, off-the-shelf SDK(Software Development Kit) OKTAL-SE is used. For the servo controller, well-proven mechanism in the previous program is applied to increase servo control accuracy. To analyze the performance of a targeting pod in a realistic environment, 1553B, ARINK818 interface and etc. which are actually implemented in real combat aircrafts are applied in the system. By using the developed HILS system, the performance of currently operating targeting pods in real combat aircrafts can be analyzed and predicted. Additionally, the relationship between overall system performance and each module performance can be analyzed, the currently developed HILS system is expected to be a very useful tool to generate system development requirements of targeting pods and to reduce any possible future development risks.

A Study on the Military Runway Protection Performance for the Multiple Warheads Attack (다탄두 공격에 대한 군 활주로 방호성능 평가)

  • Hwang, Injae;Han, Jaeduk;You, Seunghan;Kim, Sungkon
    • KSCE Journal of Civil and Environmental Engineering Research
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    • v.40 no.5
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    • pp.521-526
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    • 2020
  • Airfield pavements, such as runways and taxiways, are essential for smooth take-off and landing of fixed-wing aircraft and are the most important installation for the military to carry out air operations during wartime. Therefore, in wartime, it is necessary to reduce the damage to these installations and repair them in the shortest possible time. Recently, the pattern of attack is changing from the use of conventional high explosive which is to create large craters to the use of multiple warheads weapon system which is to effectively attack enemy's airfields but unrelated to accuracy. Hence in this study, through identifying the specification and composition of multiple warheads weapon system, we checked the protection performance and damage patterns of the pavement when explosion occurred on the installed military runway and taxiway by the multiple warheads weapon system. And The multiple warheads weapon systems is able to cause extensive damage but the destructive power of each warhead is not as great, so I would like to propose an airfield pavement design plan for minimal protection against such attacks.