• Title/Summary/Keyword: 유인성능

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Development of the silver-white decoy for squid automatic jigging machine and fishing performance (오징어채낚기용 은백색 유인체 개발과 어획성능)

  • An, Young-Il;Jang, Ung-Jeong
    • Journal of the Korean Society of Fisheries and Ocean Technology
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    • v.49 no.3
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    • pp.208-217
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    • 2013
  • Decoys for automatic jigging machines, the body part of a squid hook, have been developed in small and existing sizes in consideration of squid food, color blindness, and retinomotor responses and in utilization of pearl pigment, PP of high transparency, and combined mixture. In comparison of the developed silver-white decoy and existing decoys, the optical characteristics were examined, and the fishing performance of small size silver-white squid hooks was assessed in application of 4 fishing boats with the squid automatic jigging machine and metal halide fishing lamp in July, 2012. The luminances of the three squid hook colors-green, dark green and silver-white-increased as the intensity of illumination increased. Among these, the increase of silver-white was particularly distinguished. As to the average contrast of squid hooks, that of silver-white was 10.33, which was the highest, and then green 1.86 and dark green -0.10 in the order. As to the fishing performance of the silver-white hook, that of the 202 Geumyeong-ho and 101Yongjin-ho which caught squids were similar to that of the existing green hook and was relatively low in the case of the Dongbu-ho. However, that of the Haengbok-ho which caught relatively small squids whose average length was 19.9cm and installed silver-white hook in all automatic jigging machines was significantly excellent. In order to enhance the fishing performance of small size silver-white hooks, therefore, it would be effective to install in every automatic jigging machines of fishing boat and to start fishing before July by which small squids are caught.

UAV Network Resource Allocation Algorithm according to the Network Environment and Data Requirement (네트워크 환경 및 데이터 요구사항에 따른 무인기 네트워크 자원할당 알고리즘)

  • Cheon, Hye-Rim;Hwang, Chan-Ho;Lee, Woosin;Yoo, Indeok;Kim, Jae-Hyun
    • Journal of the Institute of Electronics and Information Engineers
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    • v.54 no.7
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    • pp.3-11
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    • 2017
  • UAV system has the limitation to allocate enough spectrum bandwidth for the operation of multiple UAVs due to the market expansion. In addition, the communication environment of UAV network varies dynamically due to the UAV's mobility. Thus, to operate the stable UAV system and maximize the transmission data rate, it needs to allocate the resource effectively in the limited bandwidth considering the given network environment. In this paper, we propose the resource allocation algorithm which can maximize the network throughput as well as satisfy the minimum data requirement for the UAV system operation in the given network environment based on TDMA(Time Division Multiple Access). By performance analysis, we show that the proposed algorithm can allocate the resource to satisfy the high network throughput as well as the minimum data requirement in the given network environment.

Study on the Integrated UAV Simulation Environment for the Evaluation of the Midair Collision Alarm System (공중충돌경보시스템 평가를 위한 통합 무인기 시뮬레이션환경 연구)

  • Mun, Seong-yeop;Kim, Ju-young;Lee, Dong-woo;Baek, Gyeong Min;Kim, Jin Sil;Na, Jongwhoa
    • Journal of Advanced Navigation Technology
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    • v.19 no.4
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    • pp.288-298
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    • 2015
  • For the commercialization of unmanned aircraft, we must validate the safety of the air/ground collision alert systems (CAS). The validation procedure of CAS requires the flight test which is not only expensive but also dangerous. To alleviate this problem, we need the simulation based validation process for the CAS. We developed an integrated UAV simulation (IUS) environment which interconnect the flight simulator, the Matlab/Simulink, and a target avionics simulation model. We developed the collision warning module of the TCAS and tested using IUS and flight encounter models. Using IUS, we can evaluate the performance and reliability of a target avionic system at the preliminary design stage of a development life cycle.

A Study on Fingerprinting Robustness Indicators for Immersive 360-degree Video (실감형 360도 영상 특징점 기술 강인성 지표에 관한 연구)

  • Kim, Youngmo;Park, Byeongchan;Jang, Seyoung;Yoo, Injae;Lee, Jaechung;Kim, Seok-Yoon
    • Journal of IKEEE
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    • v.24 no.3
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    • pp.743-753
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    • 2020
  • In this paper, we propose a set of robustness indicators for immersive 360-degree video. With the full-fledged service of mobile carriers' 5G networks, it is possible to use large-capacity, immersive 360-degree videos at high speed anytime, anywhere. Since it can be illegally distributed in web-hard and torrents through DRM dismantling and various video modifications, however, evaluation indicators that can objectively evaluate the filtering performance for copyright protection are required. In this paper, a robustness indicators is proposed that applies the existing 2D Video robustness indicators and considers the projection method and reproduction method, which are the characteristics of Immersive 360-degree Video. The performance evaluation experiment has been carried out for a sample filtering system and it is verified that an excellent recognition rate of 95% or more has been achieved in about 3 second execution time.

Portable and Extensible ARINC 653 for Drones (드론을 위한 이식성과 확장성을 지원하는 ARINC 653)

  • Kim, Jooho;Jo, Hyun-Chul;Jin, Hyun-Wook;Lee, Sangil
    • The Journal of Korean Institute of Communications and Information Sciences
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    • v.41 no.12
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    • pp.1884-1891
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    • 2016
  • With the various usage of civil drones, such as hobby, filmmaking and surveillance, the need for technology that safely reconstructs software for target application domains has been increasingly rising. In order to support a reliable software integration of avionic systems, the ARINC 653 standard has been proposed and adapted mainly on manned aircrafts. Therefore, applying ARINC 653 on civil drones could be desirable. Though, various researches on implementing ARINC 653 has been conducted, there are still additional requirements to apply ARINC 653 to civil drones that use various platforms and have a wide range of use. In this paper, taking account of these requirements, we implement a portable and extensible ARINC 653 and analyze its performance. We offer the portability with the OS abstraction layer that reduces dependency on a specific operating system, and provide the design that can extend internal functions, such as partition scheduler and process scheduler.

Human-in-the-Loop Simulation Analysis of Conflict Resolution Maneuvers Using an Air Traffic Control Simulator (항공관제시뮬레이터를 이용한 항공기간 회피 기동의 위험도 분석)

  • Jeong, Se hun;Oh, Hyeju;Choi, Keeyoung;Lee, Hak-Tae
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.43 no.8
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    • pp.739-747
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    • 2015
  • With rapid growth in the technologies and demand of Remotely Piloted Aircraft Systems (RPASs), integration of such systems into the existing airspace system is becoming an issue in many countries. RPAS have different flight performances, communication characteristics, separation assurance mechanisms, and human machine interfaces from manned aircraft. To establish rules and regulations for RPAS integration, it is important to understand the impacts of RPASs on the airspace system. A simulation system that integrates manned aircraft, air traffic control, and RPASs is developed in Inha University to investigate these impacts through Human-in-The-Loop (HiTL) simulations. Three conflict resolution scenarios between a manned aircraft and a Remotely Piloted Aircraft (RPA) were constructed and tested. Human factors such as the response times of pilots and controllers were measured and analyzed as well as the risk of each maneuver.

Development of System Integration Laboratory for the Verification of UAV Avionics System Requirements (무인기 항공전자시스템 요구도 검증을 위한 통합시험환경 개발)

  • Jo, Young-Wo;Kim, Bong-Gyu;Park, Jae-Sung;Lee, Jae-Uk
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.40 no.5
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    • pp.446-453
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    • 2012
  • As part of the integration phases in developing a UAV, a System Integration Laboratory (SIL) has been developed to provide integrated test capability for the verification of avionics system requirements. The SIL has realized primary functions that are common in manned aircraft SIL's, and specialized laying stress on test data visualization and test automation under the closed-loop structure of the ground control simulation, aircraft simulation and flight simulation components. Those design results have led to easy and sure verification of lots of complex requirements of the UAV avionics system. The functions and performances of the SIL have been proved in four gradational test steps and checked to operate successfully in aircraft System Integration Test Environment for the integration of UAV ground station and aircraft.

Design of a Photovoltaic PCS with Compensation Control of Reactive Power and Unbalance Current in Three-phase systems (3상 시스템의 무효전력, 불평형 전류 보상 기능을 갖는 태양광 전력변환장치 설계)

  • Park, Sang-Min;Kim, Chang-Soon;Le, Dinh Vuong;Park, Minwon;Yu, In-Keun
    • Journal of Korea Society of Industrial Information Systems
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    • v.21 no.3
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    • pp.29-33
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    • 2016
  • Development of the distributed energy resources such as photovoltaic, wind, and fuel cell has increased rapidly due to the rising demand for clean energy utilization. On the other hand, the distribution system became complex and has problems such as degradation of power factor and current unbalance caused by power converters, reactive power and unbalanced loads. To solve these problems, this paper proposes a 3-phase 4-leg type power conditioning system with compensation control algorithm for the reactive power and unbalance current in distribution system using photovoltaic resource. It is simulated in PSCAD/EMTDC and the effectiveness is confirmed.

A Method on the Realization of QoS Guarantee in the Grid Network (그리드 네트워크에서의 QoS 보장방법 구현)

  • Kim, Jung-Yun;Na, Won-Shin;Ryoo, In-Tae
    • Journal of Digital Contents Society
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    • v.10 no.1
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    • pp.169-175
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    • 2009
  • Grid computing is an application to obtain the most efficient performance from computing resources in terms of cost and convenience. It is also considered as a good method to solve a problem that cannot be settled by conventional computing technologies such as clustering or is requiring supercomputing capability due to its complex and long-running task. In order to run grid computing effectively, it needs to connect high-performance computing resources in real-time which are distributed geographically. Answering to the needs of this grid application, researchers in several universities with Argonne National Laboratory in the USA (ANL) as the main axis have developed Globus. It is noticed, however, that the quality of service (QoS) is not guaranteed when certain jobs are exchanged through networks in the context of Globus. To tackle with this problem, the ANL has invented Globus Architecture for Reservation and Allocation (GARA). The researchers of this paper constructed a testbed for evaluating the ability to reserve resource in the GARA system and implemented the GARA code for it. We analyzed the applied results and discussed future research plans.

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An Experimental Study on the Effect of Swirler Mass Flowrate and Flare Exit Length on Flow Patterns inside a Model Combustor Chamber (스월러 플레어 출구길이가 모델 챔버내 유동에 미치는 영향에 대한 실험적 연구)

  • Ryu, Gyong Won;Jin, Yu In;Kim, Yeong Ryon;Kim, Hong Jip
    • Journal of the Korean Society of Propulsion Engineers
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    • v.20 no.6
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    • pp.70-75
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    • 2016
  • A swirler is a flame holding device generating recirculation regions in a gas turbine combustor, and the flow pattern due to a swirler has major effects on the flame distributions, combustion efficiency, and characteristics of exhaust gas. An experimental study for a counter-rotating swirler has been conducted to find out effects of the mass flow rate ratio of the inner/outer swirler flow area, the pressure difference between the swirler inlet and outlet, and the flare exit length ratio on the flow patterns in a model combustion chamber by using PIV(Particle Image Velocimetry) technique.