• 제목/요약/키워드: Mission Operations

검색결과 206건 처리시간 0.026초

최적화와 분할 방법을 이용한 항공기 표적 할당 연구 (A Study on Aircraft-Target Assignment Problem in Consideration of Deconfliction)

  • 이혁;이영훈;김선훈
    • 경영과학
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    • 제32권1호
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    • pp.49-63
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    • 2015
  • This paper investigates an aircraft-target assignment problem in consideration of deconfliction. The aircraft-target assignment problem is the problem to assign available aircrafts and weapons to targets that should be attacked, where the objective function is to minimize the total expected damage of aircrafts. Deconfliction is the way of dividing airspaces for aircraft flight to ensure the safety while performing the mission. In this paper, mixed integer programming model is suggested, where it considers deconfliction between aircrafts. However, the suggested MIP model is non-linear and limited to get solution for large size problem. The 2-phase decomposition model is suggested for efficiency and computation, where in the first phase target area is divided into sectors for deconfliction and in the second phase aircrafts and weapons are assigned to given targets for minimizing expected damage of aircraft. The proposed decomposition model shows outperforms the model developed for comparison in the computational experiment.

유무인 겸용 비행체의 자동비행조종시스템 개발 (Automatic Flight Control System Development for Optionally Piloted Vehicle)

  • 이상종;최형식;성기정
    • 한국항공우주학회지
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    • 제42권11호
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    • pp.968-973
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    • 2014
  • 유무인 겸용 비행체인 OPV는 무인기 개발방법 중의 하나로 기존 유인기 운용을 통해 검증된 유인 비행체와 엔진 및 각 계통을 유지하며, 무인기 운용을 위해 필요한 부가 시스템을 장착하고, 필요에 따라 기존시스템을 수정하여 개발비용과 시간을 줄일 수 있는 장점을 가지고 있다. 또한 임무 및 비행조건에 따라 유인기와 무인기로 겸용하여 운용할 수 있는 장점을 가지고 있으며, 퇴역하는 유인기를 재활용하는 측면에서도 국가의 중요재원을 효율적으로 활용할 수 있는 시스템이다. 본 논문에서는 국내 최초로 개발한 고정익 OPV 비행체의 자동비행조종시스템을 중심으로 초기 중요 개발개념과 기술적 고려사항 들을 정리하였다.

Feasibility study of corner reflector for radar countermeasures and deception for conventional forces

  • Kang, Hee-Jin;Yang, Hyang-Kweon;Jo, Min-Chul;Kim, Kook-Hyun
    • Journal of Advanced Marine Engineering and Technology
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    • 제41권2호
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    • pp.171-175
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    • 2017
  • The high-tech large warships are minimal and they are always monitored by opponents, and become primary targets when conflicts occur. The improvement in reducing susceptibility has significant importance because it is difficult for a ship to maintain mission capability and functionality once it is damaged. Ordinary decoys are effective only under the premise that the ship has already been exposed. Traditionally, for naval vessels, techniques related to the radar have been used in military stealth techniques to ensure confidentiality. The corner reflector, on the other hand, can produce rather large radar cross sections. Continued use of deceptive systems such as chaff during operations will help to improve survivability of naval ships. From this viewpoint, corner reflector was considered for making radar countermeasures and deception technology. This paper reviews the current status of corner reflector basis decoys and the technical feasibility of corner reflectors for developing structural decoys.

Launch and Early Orbit Phase Simulations by using the KOMPSAT Simulator

  • Lee, Sanguk;Park, Wan-Sik;Lee, Byoung-sun;Lee, Ho-Jin;Park, Hanjun
    • 제어로봇시스템학회:학술대회논문집
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    • 제어로봇시스템학회 1999년도 제14차 학술회의논문집
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    • pp.33-36
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    • 1999
  • The KOMPSAT, which is scheduled to be launched by Taurus launch vehicle in late November of 1999, will be in a sun-synchronous orbit with an altitude of 685km, eccentricity of 0.001, inclination of 98deg and local time of ascending node of 10:50 a.m. Electronics and Telecommunications Research Institute and Daewoo Heavy Industry had jointly developed a KOMPSAT Simulator as a component of the KOMPSAT Mission Control Element. The MCE had been delivered to Korea Aerospace Research Institute for the KOMPSAT ground operation. It is being used for training of KOMPSAT ground station personnel. Each of satellite subsystems and space environment were mathematically modeled in the simulator. To verify the overall function of KOMPSAT simulator, a Launch and Early Orbit Phase(LEOP) operation simulations have been performed. The simulator had been verified through various tests such as functional level test, subsystem test, interface test, system test, and acceptance test. In this paper, simulation results for LEOP operations to verify flight software adapted into simulator, satellite subsystem models and environment models are presented.

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3D Global Dynamic Window Approach for Navigation of Autonomous Underwater Vehicles

  • Tusseyeva, Inara;Kim, Seong-Gon;Kim, Yong-Gi
    • International Journal of Fuzzy Logic and Intelligent Systems
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    • 제13권2호
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    • pp.91-99
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    • 2013
  • An autonomous unmanned underwater vehicle is a type of marine self-propelled robot that executes some specific mission and returns to base on completion of the task. In order to successfully execute the requested operations, the vehicle must be guided by an effective navigation algorithm that enables it to avoid obstacles and follow the best path. Architectures and principles for intelligent dynamic systems are being developed, not only in the underwater arena but also in related areas where the work does not fully justify the name. The problem of increasing the capacity of systems management is highly relevant based on the development of new methods for dynamic analysis, pattern recognition, artificial intelligence, and adaptation. Among the large variety of navigation methods that presently exist, the dynamic window approach is worth noting. It was originally presented by Fox et al. and has been implemented in indoor office robots. In this paper, the dynamic window approach is applied to the marine world by developing and extending it to manipulate vehicles in 3D marine environments. This algorithm is provided to enable efficient avoidance of obstacles and attainment of targets. Experiments conducted using the algorithm in MATLAB indicate that it is an effective obstacle avoidance approach for marine vehicles.

GPS-Based Orbit Determination for KOMPSAT-5 Satellite

  • Hwang, Yoo-La;Lee, Byoung-Sun;Kim, Young-Rok;Roh, Kyoung-Min;Jung, Ok-Chul;Kim, Hae-Dong
    • ETRI Journal
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    • 제33권4호
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    • pp.487-496
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    • 2011
  • Korea Multi-Purpose Satellite-5 (KOMPSAT-5) is the first satellite in Korea that provides 1 m resolution synthetic aperture radar (SAR) images. Precise orbit determination (POD) using a dual-frequency IGOR receiver data is performed to conduct high-resolution SAR images. We suggest orbit determination strategies based on a differential GPS technique. Double-differenced phase observations are sampled every 30 seconds. A dynamic model approach using an estimation of general empirical acceleration every 6 minutes through a batch least-squares estimator is applied. The orbit accuracy is validated using real data from GRACE and KOMPSAT-2 as well as simulated KOMPSAT-5 data. The POD results using GRACE satellite are adjusted through satellite laser ranging data and compared with publicly available reference orbit data. Operational orbit determination satisfies 5 m root sum square (RSS) in one sigma, and POD meets the orbit accuracy requirements of less than 20 cm and 0.003 cm/s RSS in position and velocity, respectively.

평균 필드 게임 기반의 강화학습을 통한 무기-표적 할당 (Mean Field Game based Reinforcement Learning for Weapon-Target Assignment)

  • 신민규;박순서;이단일;최한림
    • 한국군사과학기술학회지
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    • 제23권4호
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    • pp.337-345
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    • 2020
  • The Weapon-Target Assignment(WTA) problem can be formulated as an optimization problem that minimize the threat of targets. Existing methods consider the trade-off between optimality and execution time to meet the various mission objectives. We propose a multi-agent reinforcement learning algorithm for WTA based on mean field game to solve the problem in real-time with nearly optimal accuracy. Mean field game is a recent method introduced to relieve the curse of dimensionality in multi-agent learning algorithm. In addition, previous reinforcement learning models for WTA generally do not consider weapon interference, which may be critical in real world operations. Therefore, we modify the reward function to discourage the crossing of weapon trajectories. The feasibility of the proposed method was verified through simulation of a WTA problem with multiple targets in realtime and the proposed algorithm can assign the weapons to all targets without crossing trajectories of weapons.

전문도서관 기준의 동향과 개정 방향 연구 (Trend Analysis and Revision of the Special Library Standard in Korea)

  • 김홍렬
    • 정보관리연구
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    • 제43권1호
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    • pp.1-22
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    • 2012
  • 도서관 기준은 도서관의 사명과 목적, 이용자서비스, 운영관리 등에 대한 기본 방향을 제공하고, 도서관이 수행하는 각종 서비스와 프로그램을 측정 평가할 수 있는 준거로 활용할 수 있다. 또한 도서관이 중장기 계획을 수립하고, 목표수준을 설정할 때, 근거자료가 될 수 있다. 국내에서도 관종별 도서관 기준이나 법적인 기준을 마련하여 이의 활동을 위한 도구로 활용하고 있다. 그러나 한국도서관기준은 오랜기간 동안 개정되지 못하여 현재의 도서관 환경을 반영하기 어려우며, 법적인 기준도 그 내용이 매우 미미하여 최소한의 기준으로도 작동하지 못하고 있는 실정이다. 이에 본 연구는 주요국가의 전문도서관 기준과 국내의 관련 기준들을 분석하여 현재의 도서관 환경을 반영할 수 있는 직원, 장서, 시설 기준의 개정방향을 제시하였다.

군사로봇의 감시제어에서 운용자 역량 평가 방법에 관한 연구 (Operator Capacity Assessment Method for the Supervisory Control of Unmanned Military Vehicle)

  • 최상영;양지현
    • 로봇학회논문지
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    • 제12권1호
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    • pp.94-106
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    • 2017
  • Unmanned military vehicles (UMVs) will be increasingly applied to the various military operations. These UMVs are most commonly characterized as dealing with "4D" task - dull, dirty, dangerous and difficult with automations. Although most of the UMVs are designed to a high degree of autonomy, the human operator will still intervene in the robots operation, and tele-operate them to achieve his or her mission. Thus, operator capacity, along with robot autonomy and user interface, is one of the important design factors in the research and development of the UMVs. In this paper, we propose the method to assess the operator capacity of the UMVs. The method is comprised of the 6 steps (problem, assumption, goal function identification, operator task analysis, task modeling & simulation, results and assessment), and herein colored Petri-nets are used for the modeling and simulation. Further, an illustrative example is described at the end of this paper.

NOTECHS이 안전운항(安全運航)에 미치는 영향(影響) (The Effect of the Non-Technical Skills on the Rotorcraft Flight Safety)

  • 이상민;김칠영;황사식
    • 한국항공운항학회지
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    • 제21권3호
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    • pp.27-40
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    • 2013
  • Rotorcraft operating in the domestic aviation safety techniques are applied CRM training is conducted but, aircraft accidents caused by human factors has not shown a declining trend. Thus, knowledge of aviation safety and human factors for the spread of awareness of improved rotorcraft flight operations department managers to understand the complexity of nature and culture, and to perform high-risk mission helicopter pilot study of local activation and enhance safety awareness research was conducted in order to. In this study, the development direction of CRM training studies in order to identify the leading NOTECHS (Non-Technical Skills; non-technical pilot skills) of the four categories as the independent variable and the dependent variable corresponding to the resulting effect on the key variables awareness of the differences were studied. In addition, the direction and strength of the relationship were analyzed to determine the relationship of each independent variable to assess the impact on the dependent variable regression analysis was performed. Pilot training and evaluation of non-technical skills related to the teaching reflected in the CRM training and assessment must be carried out with 5 star rating scale was preferred. Therefore, to meet our country rotorcraft operating environment 'NOTECHS' aviation safety by developing training programs reflected in the educational process, implementation, and periodic training and assessment is done in future research on this analysis and feedback is done to reflect the specific performance expect.