• Title/Summary/Keyword: air defense

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The principles and Applications of Outdoor & Indoor GPS(Global Positioning System) (옥내 외 위치정보측정시스템의 원리와 응용)

  • Moon, Hank
    • Journal of the Korean Professional Engineers Association
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    • v.41 no.5
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    • pp.55-58
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    • 2008
  • GPS is the global Navigation Satellite System which is developed by the United States Department of Defense as an abbreviation of the Global Positioning System. The GPS uses a constellation of 24 Medium Earth Orbit satellites that transmit precise microwave signals, that enable GPS receivers to determine their location, speed, direction, and time. Following, the shooting down of Korean Air Lines Flight 007 in 1983. President Ronald Reagan issued a directive making the system available free for civilian use as a common good. Since then, GPS has become a widely used aid to navigation worldwide, and a useful tool for map-making, land surveying, commerce, scientific uses, and hobbies such as geocaching. GPS also provides a precise time reference used in many applications including scientific study of earthquakes, and synchronization of telecommunications networks.

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A Study on Dispersed Media Formation of Hydrocarbon Fuel by an Explosive Burster (화약 폭발에 의한 탄화수소계 연료의 분산매질 형성에 관한 연구)

  • Yoo, Jae Hun
    • Journal of the Korean Society of Safety
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    • v.31 no.2
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    • pp.33-40
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    • 2016
  • Liquid fuel can be easily exploded and release more energy of detonation than conventional explosives because it has different explosion mechanism. In order to analyze dispersion characteristics of liquid fuel for the safety purpose, two tests are conducted. First, pre-test, which is a computer simulation, is carried out by a software called ANSYS AUTODYN to eliminate the effect of a canister that usually causes irregular dispersion of the fuel. Second, field test is performed to find out the amount and density effect of bursting charge. High speed cameras are installed in front of the canister to visualize the mechanism. Velocity, area and radius of the dispersed cloud are measured by image processing software, these are shown that the amount of bursting charge affects cloud velocity and area but density is not a significant factor of cloud formation.

Heuristic Algorithm for the Single-machine Scheduling with Periodic Maintenance (주기정비를 고려한 단일기계 일정계획을 위한 휴리스틱 알고리즘 설계)

  • Lee, Sang-Heon;Lee, In-Gu
    • Journal of Korean Institute of Industrial Engineers
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    • v.34 no.3
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    • pp.318-327
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    • 2008
  • This paper considers a single-machine scheduling problem with availability constraints. In many realistic situations, machines may not be always available due to various reasons such as maintenance, breakdown and repair. However, most literature on scheduling assume that the machines are available at all times. This paper deals with a single-machine scheduling problem with periodic maintenance. If the maintenance decision is made jointly with the job scheduling, the system will be more effective. The objective is to minimize the total completion time of jobs. This problem is proved to be NP-hard in the strong sense. The proposed breaking heuristic(BH) algorithm rule is established by some theorems and conditions. Our computational results show that the BH algorithm is much more efficient than existing heuristic.

Improvement of Localization Accuracy with COAG Features and Candidate Selection based on Shape of Sensor Data (COAG 특징과 센서 데이터 형상 기반의 후보지 선정을 이용한 위치추정 정확도 향상)

  • Kim, Dong-Il;Song, Jae-Bok;Choi, Ji-Hoon
    • The Journal of Korea Robotics Society
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    • v.9 no.2
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    • pp.117-123
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    • 2014
  • Localization is one of the essential tasks necessary to achieve autonomous navigation of a mobile robot. One such localization technique, Monte Carlo Localization (MCL) is often applied to a digital surface model. However, there are differences between range data from laser rangefinders and the data predicted using a map. In this study, commonly observed from air and ground (COAG) features and candidate selection based on the shape of sensor data are incorporated to improve localization accuracy. COAG features are used to classify points consistent with both the range sensor data and the predicted data, and the sample candidates are classified according to their shape constructed from sensor data. Comparisons of local tracking and global localization accuracy show the improved accuracy of the proposed method over conventional methods.

Oxidative Stress Resulting from Environmental Pollutions and Defence Mechanisms in Plants (환경오염(環境汚染)에 의한 산화(酸化)스트레스와 식물체(植物體)의 방어기작(防禦機作))

  • Shim, Sang-In;Kang, Byeung-Hoa
    • Korean Journal of Environmental Agriculture
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    • v.12 no.3
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    • pp.264-280
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    • 1993
  • The environmental pollutions were a serious problem in Korea recently. So many researcher have studied the effect of environmental pollution on plants and agro-ecosystem, but the basic mechanisms of environmental stresses were various. One of the important mechanisms was oxidative stress caused by active toxic oxygen. The toxic oxygen was generated by several stresses, abnormal temperature, many xenobiotics, air pollutants, water stress, fugal toxin, etc. In the species of toxic oxygen which is primary inducer of oxidative stresses, superoxide, hydrogen peroxide, hydroxyl radical and singlet oxygen were representative species. The scavenging systems were divided into two groups. One was nonenzymatic system and the other enzymatic system. Antioxidants such as glutathione, ascorbic acid, and carotenoid, have the primary function in defense mechanisms. Enzymatic system divided into two groups; First, direct interaction with toxic oxygen(eg. superoxide dismutase). Second, participation in redox reaction to maintain the active antioxidant levels(eg. glutathione reductase, ascorbate peroxidase, etc.).

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A Reliability Optimization Problem of System with Mixed Redundancy Strategies (혼합 중복전략을 고려한 시스템 신뢰도 최적화 문제)

  • Kim, Heung-Seob;Jeon, Geon-Wook
    • IE interfaces
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    • v.25 no.2
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    • pp.153-162
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    • 2012
  • The reliability is defined as a probability that a system will operate properly for a specified period of time under the design operating conditions without failure and it has been considered as one of the major design parameters in the field of industries. Reliability-Redundancy Optimization Problem(RROP) involves selec tion of components with multiple choices and redundancy levels for maximizing system reliability with constraints such as cost, weight, etc. However, in practice both active and cold standby redundancies may be used within a particular system design. Therefore, a redundancy strategy(active, cold standby) for each subsystem in order to maximize system reliability is considered in this study. Due to the nature of RROP, i.e. NP-hard problem, A Parallel Particle Swarm Optimization(PPSO) algorithm is proposed to solve the mathematical programming model and it gives consistently better quality solutions than existing studies for benchmark problems.

Analysis of the Characteristics of an Aerospike Pintle Nozzle in terms of Stroke and Operating Pressure

  • Kim, Jeongjin
    • Journal of Aerospace System Engineering
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    • v.14 no.4
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    • pp.1-9
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    • 2020
  • The characteristics of an aerospike pintle nozzle system with excellent altitude compensation were analyzed using cold air testing. It was confirmed that reducing the stroke of the aerospike nozzle is effective in increasing the thrust. However, the results of additional numerical analysis indicated that the discharge coefficient factor was significantly lower at the maximum stroke. The Vena contracta due to the cowl reduction angle decreased the effective nozzle throat area at the maximum stroke and hindered expansion. Complementing the cowl design may thus increase the efficiency of a solid-propellant rocket engine that uses the aerospike pintle nozzle system.

Aircraft flight simulator development for ergonomics test (인간공학실험용 항공기 모의비행훈련장비 개발)

  • 오제상
    • Journal of the Ergonomics Society of Korea
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    • v.16 no.1
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    • pp.97-105
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    • 1997
  • An aircraft simulator for ergonomics testing and pilot training was developed from the joint work Agency for Defense Development(ADD) and Daewoo Heavy Industry, LTD, in Korea at first time. It is basically to satisfy the requirements established by FAA-AC-120-40C ( 1995-JAN-26). The aircraft simulator will be used mainly for ergonomics testing and pilot training for basic trainer on ADD and Korea Air Force in near futrue. This simulator reproduces faithfully the cockpit and flight characteristics of the KTX-1 aircraft. It is one of the latest full flight simulators that have the CGI(computer graphic image) visual system and six degree of freedom motions system. Development efforts focused on user-oriented design approach for ergonomics testing and flight training of pilots. Main characteristics of each subsystem are described such as cockpit, instruments, control loading system, motion system, visual system, aural system, instructor operation station and aircraft simulation softwear.

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DGPs System (DGPS 위성항법보정 SYSTEM)

  • 이용안
    • Journal of the Korean Professional Engineers Association
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    • v.37 no.2
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    • pp.47-53
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    • 2004
  • Space-based radio-positioning and time transfer system, Provide accurate position, velocity, and time(PVT) information \longleftarrowunlimited number of suitably equipped ground, sea, air and space users, by the U.S Department of Defense(DoD), Comprises major system segments\longrightarrowSpace, Control and User

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Accelerated Co-evolutionary Algorithms

  • Kim, Jong-Han;Tahk, Min-Jea
    • International Journal of Aeronautical and Space Sciences
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    • v.3 no.1
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    • pp.50-60
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    • 2002
  • A new co-evolutionary algorithm, of which the convergence speed is accelerated by neural networks, is proposed and verified in this paper. To reduce computational load required for co-evolutionary optimization processes, the cost function and constraint information is stored in the neural networks, and the extra offspring group, whose cost is computed by the neural networks, is generated. It increases the offspring population size without overloading computational effort; therefore, the convergence speed is accelerated. The proposed algorithm is applied to attitude control design of flexible satellites, and it is verified by computer simulations and experiments using a torque-free air bearing system.