• 제목/요약/키워드: Command Guidance

검색결과 74건 처리시간 0.023초

인질사건의 실태 및 대처방안 (A Study for Hostage Crisis and It's Effective Resolution)

  • 김상구
    • 시큐리티연구
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    • 제7호
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    • pp.29-59
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    • 2004
  • This is a study on hostage crisis and effective resolution of the crisis. First, we surveyed the theoretical guidance for our study: definition, patterns, of hostage crisis; psychology of hostage-takers. And we explores a great variety of hostage crisis cases to develop principles and methods for negotiation and subjugation. We suggest, throughout this study, some action program to be developed, as follow: First, we need to broaden and deepen the understanding on the issue of hostage-crisis by expanding educational opportunity on the issue, while raising hostage negotiators. Second, information sharing system among hostage management related offices, and complete training for SWAT team are required. Third, when a hostage-crisis is raised, police enforcement must corporate with mass-media in a way of close manner. Fourth, in a critical hostage crisis, the commander should appear on site for effective command. Lastly, the top-priority for the commander who is in charge of the crisis should be put on the security of hostage and hostage-taker, as well.

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유도무기체계의 성능분석기법 (A performance anaylsis technique for guided weapons)

  • 이연석;이장규;장상근
    • 제어로봇시스템학회:학술대회논문집
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    • 제어로봇시스템학회 1991년도 한국자동제어학술회의논문집(국내학술편); KOEX, Seoul; 22-24 Oct. 1991
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    • pp.274-279
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    • 1991
  • The development of a guided weapon system, such as a tactical missile, requires a performance analysis of a nonlinear system. Generally, the Monte Carlo analysis method is used for this purpose. The limitation of this method, a large number of simulations, for a nonlinear system performance analysis strongly motivated the development of a more efficient analytic technique. In this paper, the statisfical linearization methods is used for the performance analysis to the guided weapon system with the help of covariance analysis technique. Because the statistical linearization methods cannot be used to the look-up table nonlinear form such as aerodynamic coefficients, the second order polynomial representations is obtained from the table using the Lagrange interpolating polynomial and linearized statistically. Simple simulations about initial state conditions and random component in guidance command shows the results of this technique.

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관성항법장치가 포함된 비행체의 HWIL 시뮬레이션 시스템 개발 연구 (A Study on the HWIL Simulation System of the Flight Object including Inertial Navigation System)

  • 이아영
    • 한국군사과학기술학회지
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    • 제21권3호
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    • pp.349-360
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    • 2018
  • This paper proposes various methods for constructing a HWIL simulation system including Inertial Navigation System(INS) and Guidance Control Unit(GCU) under the assumption that the INS identifies the initial attitude of an aviation body through its own alignment and that it is a package consisting of an inertial sensor and a navigation computation module. This paper also presents a real-time computing technology and a way to calculate the command of the Flight Motion System(FMS) analogous to the acutal flight environment. The proposed HWIL simulation system is constructed by applying the above-mentioned methods and the results of running a series of simulations confirm high effectiveness and usefulness of the system. Finally, minor error factors that could be acquired only in HWIL simulation Environment are analyzed.

Alexa를 이용한 대학안내 시스템 (The University Gusdance System using the Alexa)

  • 김태진;김동현
    • 한국정보통신학회논문지
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    • 제21권11호
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    • pp.2061-2066
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    • 2017
  • 음성인식 기술은 사용자의 음성을 인식하여 명령을 실행하는 기술로 현재는 자연어 처리 기법과 접목되어 인공지능 음성인식 서비스로 제공되어 지고 있다. 이러한 인공지능 음성인식 서비스는 IoT기기를 제어하거나 뉴스 또는 날씨와 같은 정보 제공 분야에서 활용되고 있다. 정보 제공 분야의 하나인 대학 정보는 주로 웹을 통하여 제공되나 너무 많은 데이터를 제공하기 때문에 사용자가 신속하게 원하는 정보를 검색할 수 없는 문제가 있다. 이 논문에서는 사용자가 찾고자 하는 정보를 음성으로 인식하고 제공하기 위한 대학 안내 시스템을 설계하고 구현한다. 대학정보를 각 주제별로 분류하고 이를 제공하기 위한 람다 함수를 설계한다. 그리고 알렉사 스킬 키트를 이용하여 노드제이에스로 구현된 모듈을 아마존웹서비스에 업로드하여 음성인식을 이용하여 대학 정보를 제공한다.

스트랩다운 탐색기 기반 호밍루프 설계 (Homing Loop Design for Missiles with Strapdown Seeker)

  • 홍주현;유창경
    • 한국항공우주학회지
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    • 제42권4호
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    • pp.317-325
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    • 2014
  • 스트랩다운 탐색기를 장착한 유도탄의 경우 유도에 필요한 시선각속도 추출을 위해서는 탐색기 측정치인 관측각속도에서 동체각속도 성분을 보상해 주어야 한다. 관측각속도에 포함된 동체각속도와 동체각속도 성분의 보상에 사용되는 자이로 출력인 동체각속도의 신호 특성의 차이는 호밍루프의 불안정성을 야기한다. 본 논문에서는 자이로 출력에 탐색기 지연을 고려하여 보상신호의 특성을 일치시키고, 탐색기 지연에 오차가 있을 경우에도 전체 호밍루프의 안정화를 이루기 위해 유도명령 단에 PID제어기를 적용하는 호밍루프 설계방법을 제안하였다. 보상 전 후의 선형모델 대한 안정성해석을 수행하였고, 비선형 6자유도 시뮬레이션을 통해 설계된 호밍루프의 안정성과 성능을 검증하였다.

상법상 선장의 지위와 선박소유자의 대리권의 판례에 관한 연구 (A Study on legal status of shipmaster and precedent of his Authority)

  • 황석갑
    • 한국항해학회지
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    • 제17권3호
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    • pp.1-14
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    • 1993
  • The master of ship is always authorised to perform whatever acts are ordinarily necessary for the safe and proper prosecution of the voayge with regard to both ship and cargo. In other words, when a ship is away from her home port, where her business was managed, the master generally carried the owner's authority, and ordinarily he had power to enter into engagements, on their behalf, for carrying goods in the ship, or for letting her service, provided those engagements were consistent with the usual manner of employing her adopted by the owners. Accordingly he has always to decide onboard for an adequate applying of statutory law and cases whenever he acts. But the master would appear to have no such autho-rity where he can communicate with the owners without difficulty as, now-a-days, he nearly always can. This paper, therefore, intend to review some guidance of his authority in accordance with the Korean Code of Commerce as well as precedent based on it. The paper is also simply to place at the disposal of young shipmasters and those who aspire to command some legal information concerning limit of master's authority away from vessel's home port through legal commentation on the precedent, which may assist them to a better understanding of the many problems they may be faced with in the course of their ca-reers. In order to make an efficient study of legal structure concerned for shipmaster's authority, several up-to-date precedents are selected and described herein by writer's opinion for preventing unreasonable legal dispute in this field before courts in future.

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농용트랙터의 자동조향을 위한 퍼지제어와 적응제어의 비교 (Comparison between Fuzzy and Adaptive Controls for Automatic Steering of Agricultural Tractors)

  • 노광모
    • Journal of Biosystems Engineering
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    • 제21권3호
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    • pp.283-292
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    • 1996
  • Automatic guidance of farm tractors would improve productivity by reducing operator fatigue and increasing machine performance. To control tractors within $\pm$5cm of the desired path, fuzzy and adaptive steering controllers were developed to evaluate their characteristics and performance. Two input variables were position and yaw errors, and a steering command was fed to tractor model as controller output. Trapezoidal membership functions were used in the fuzzy controller, and a minimum-variance adaptive controller was implemented into the 2-DOF discrete-time input-output model. For unit-step and composite paths, a dynamic tractor simulator was used to test the controllers developed. The results showed that both controllers could control the tractor within $\pm$5cm error from the defined path and the position error of tractor by fuzzy controller was the bigger of the two. Through simulations, the output of self-tuning adaptive controller was relatively smooth, but the fuzzy controller was very sensitive by the change of gain and the shape of membership functions. Contrarily, modeling procedure of the fuzzy controller was simple, but the adaptive controller had very complex procedure of design and showed that control performance was affected greatly by the order of its model.

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소부대급 USN 기반 전장감시체계 적용 방안 (The Study Application of Identification Based on Small Units USN(Ubiquitous Sensor Network))

  • 김도헌;김도엽
    • 한국군사과학기술학회지
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    • 제13권2호
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    • pp.283-295
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    • 2010
  • Although some large units, upper than division, have a identification system, most of them depend on US military. Especially, the company unit can not but execute GOP(General OutPost) guidance and battles inefficiently because they apply the method of conventional identification system. urrently, North Korea causes the high tension of peninsular by experimenting nuclear weapons and launching ICBM(Intercontinental Ballistic Missile). In addition, ROK military will reduce the number of personnel and division through reorganizing the structure into NCW (Network Centric Warfare) until 2020. These unstable situation and future tendency require the high technical identification system based on USN(Ubiquitous Sensor Network) in company unit level. his study suggests the method that the company unit apply the identification system based on USN which distinguish between friend and foe in the warfare. The identification system concludes the results through experiment of military analysis model (AWAM; Army Weapon effectiveness Analysis Model). After analyzing the experiment results, it indicates the budget requirement and operational operability of identification system. This will be able to improves battle efficiency and to prevent damages of friendly forces.

햅틱 장치를 이용한 균형 훈련 시스템 및 효용성 검증 (A Balance Training System using a Haptic Device and Its Evaluations)

  • 윤정원;라힐 아프잘;표상훈;오민균
    • 제어로봇시스템학회논문지
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    • 제20권9호
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    • pp.971-976
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    • 2014
  • Haptic device can be a useful rehabilitation tool in balance training. The proposed system is composed of a body-wear smartphone, Phantom Omni(R) device, and its control PC system. Ten young healthy subjects performed balance tasks with different postures during 30 seconds with their eyes closed. An Android program on the smartphone transferred mediolateral (ML) and anteroposterior (AP) tilt angles to the PC system, which can generate haptic command through haptic device. Statistical data analysis was performed using MATLAB(R). COP (Center of Pressure) related indexes were measured to see reduction in body sway. ANOVA showed that haptic device significantly reduced body sway. Intuitive balance guidance could be generated using an economical and small-sized commercial haptic device, making the system efficient.

롤 보상알고리듬을 적용한 발사체 자세제어기 구조 설계 및 분석 (The Launch Vehicle Autopilot Structure Design and Analysis with Roll Compensation Algorithm)

  • 박용규;오충석;선병찬;노웅래
    • 항공우주기술
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    • 제10권1호
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    • pp.98-106
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    • 2011
  • 본 논문에서는 롤 자세운동이 발생하는 상황에서 안정적인 피치/요 자세제어를 위한 항법쿼터니언 기반 자세제어기 구조를 설계하고, 발사체 6자유도 시뮬레이션을 통해 설계된 제어기의 성능평가를 수행하였다. 항법쿼터니언 자세제어기는 기존 KSR-III, KSLV-I 상단부 자세제어기 설계 경험을 기반으로 고안되었고, 탑재소프트웨어 내에서 효율적인 자세제어 변수 사용 및 KSR-III, KSLV-I 상단부 제어기와 동일한 성능 확보 관점에서 설계되었다. 제안된 새로운 자세제어기 타당성 분석을 위하여 방위각 전환을 위한 롤 기동, 롤 자세제어가 수행되지 않는 두 비행조건에 대해 6자유도 시뮬레이션을 수행, 자세제어 성능을 평가하고 탑재 소프트웨어로서 적용 가능성을 확인하였다.