• Title/Summary/Keyword: unmaned

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Design and Performance Comparison of Synchronization Preambles for Device-to-Device Communications (단말 간 직접 통신을 위한 효율적인 동기 프리앰블 설계 및 성능비교)

  • Kim, Jong-Hoon;Sung, Ki-Young;Jung, Young-Ho
    • Journal of Satellite, Information and Communications
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    • v.12 no.1
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    • pp.125-131
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    • 2017
  • In this paper, an efficient structure of device-to-device (D2D) synchronization preamble is proposed to meet the enhanced time and frequency synchronization requirements for D2D communication. D2D communication can be applied not only for the cellular communications, but also unmaned aerial vehicle communications and vehicle-to vehicle communication. The proposed preamble structure is transmitting signals at every odd subcarriers, and empty the other subcarriers to minimize the effect of inter-carrier interference. According to the simulation results, the proposed preamble structure provides improved time offset estimation performance, without degrading frequency offset estimation performance compared to the current LTE D2D preamble.

Estimation of the Hydrodynamic Coefficients for the Deep-sea UUV "HEMIRE" (심해용 무인 잠수정의 동역학 계수의 추정에 관한 연구)

  • Baek, Hyuk;Kim, Ki-Hun;Jun, Bong-Huan;Lee, Pan-Mook;Lim, Yong-Kon
    • Journal of Ocean Engineering and Technology
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    • v.22 no.4
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    • pp.97-105
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    • 2008
  • This paper represents the experimental identification of a finite-dimensional dynamical plant model for the HEMIRE Remotely Operated Vehicle. The experiments were conducted during sea trials in the East Sea in October 2006 and peer testing by the South Sea Research Institute in January 2007. A least-squares method was employed to identify decoupled single degree-of-freedom plant dynamical models for the X, Y, Z and heading degree-of-freedom from experimental data. The performance of the identified plant dynamical model was evaluated by directly comparing simulations of the identified plant model to the experimentally observed motion data from the actual vehicle.

Design and Control of 6 D.O.F(Degrees of Freedom) Hovering AUV (6자유도 호버링 AUV의 설계 및 제어)

  • Jeong, Sang-Ki;Choi, Hyeung-Sik;Seo, Jung-Min;Tran, Ngoc Huy;Kim, Joon-Young
    • Journal of Institute of Control, Robotics and Systems
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    • v.19 no.9
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    • pp.797-804
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    • 2013
  • In this paper, a study of a new hovering six dof underwater robot with redundant horizontal thrusters, titled HAUV (hovering AUV), is presented. The results of study on the structure design, deployment of thrusters, and development of the developed control system of the AUV was presented. For the HAUV structure, a structure design and an analysis of the thrusting system was performed. For navigation, a sensor fusion board which can proceed various sensor signals to identify correct positions and speeds was developed and a total control system including EKF (Extended Kalman Filter) was designed. Rolling, pitching and depth control tests of the HAUV have been performed, and relatively small angle error and depth tracking error results were shown.

FLOW ANALYSIS AROUND THE ROTOR BLADE WITH TILT ANGLES (틸팅각에 따른 로터 블레이드 주위의 유동장 해석)

  • Yoo, Y.H.;Choi, J.W.;Kim, S.C.;Kim, J.S.
    • 한국전산유체공학회:학술대회논문집
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    • 2008.03a
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    • pp.166-170
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    • 2008
  • The changing process from hovering mode to transition one is of importance to determine a stability of tilt-rotor aircraft, which is utilized in UAV(Unmaned Aerial Vehicle). The analysis on fluid flows and aerodynamic characteristics according to variation of tilting angle of rotor is essential step in development of tilt-rotor. In the present study, the computation domain is divided into the rotating and stationary regions in order to consider the rotating blades. For the convenient realization of various tilting angle as well as application of boundary condition, the whole computation region is constructed into sphere domain. The near farfield boundary condition is adopted. The airfoil used in computation is NACA 0012. The computation results for the hovering mode are validated by comparing with previously conducted experimental results. From the results, the flow fields around rotor blade and the aerodynamic characteristics in transition mode are observed. The computational result will provide the basis for development and performance evaluation of tilt-type aircraft.

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Helicopter Landing Gear Ground Reaction Simulation (헬리콥터 강착장치 시뮬레이션)

  • 최형식;전향식;오경륜;배중원;남기욱
    • Proceedings of the Korea Society for Simulation Conference
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    • 2004.05a
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    • pp.131-135
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    • 2004
  • Landing gear force reaction module is important for aircraft take off and landing simulation. But usually this modulo is not accounted for control law design simulation. because it does not affect the flying quality of aircraft. Now a days, this module is getting more important according to the increase of needs for training purpose simulation and specific control law design such as unmaned aircraft landing on the moving platform. In this paper 1DOF mass spring simple force system per gear was accepted.

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Development of Effective Stiffness and Effective Strength for a Truss-Wall Rectangular model combined with Micro-Lattice Truss (트러스 벽면과 미세격자 트러스로 구성된 정육면체 단위모델의 강성 및 강도 개발)

  • Choi, Jeong-Ho
    • Journal of the Korean Society of Industry Convergence
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    • v.19 no.3
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    • pp.133-143
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    • 2016
  • The objective in here is to find the density, stiffness, and strength of truss-wall rectangular (TWR) model which is combined with lattice truss (MLT) inside space. The TWR unit-cell model is defined as a unit cell originated from a solid-wall rectangular (SWR) model and it has an empty space inside. Thus, the empty space inside of the TWR is filled with lattice truss model defined as TWR-MLT. The ideal solutions derived of TWR-MLT are based on TWR with MLT model and it has developed by Gibson-Ashby's theory. To validate the ideal solutions of the TWR-MLT, ABAQUS software is applied to predict the density, strength, and stiffness, and then each of them are compared with the Gibson-Ashby's ideal solution as a log-log scale. Applied material property is stainless steel 304 because of cost effectiveness and easy to get around. For the analysis, SWR and TWR-MLT models are 1mm, 2mm, and 3mm truss diameter separately within a fixed 20mm opening width. In conclusion, the relative Young's modulus and relative yield strength of the TWR-MLT unit model is reasonably matched to the ideal expectations of the Gibson-Ashby's theory. In nearby future, TWR-MLT model can be verified by advanced technologies such as 3D printing skills.t.

Accuracy Analysis of Farm Business Management Database Using Unmanned Aerial Vehicle and Field Survey (무인항공기 영상과 현장 조사를 통한 농업경영체 데이터베이스 정확도 분석)

  • Park, Jin-Ki;Park, Jong-Hwa
    • Journal of Korean Society of Rural Planning
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    • v.23 no.1
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    • pp.21-29
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    • 2017
  • The purpose of this study is to analyze the accuracy of cultivated crop database in agricultural farm business using UAV(Unmanned Aerial Vehicle) and field survey over Daesso-myeon, Umsung-gun, Chungbuk. When comparing with agricultural farm business and cadastral maps, Daeso-myeon crop field shows 29.8%(2,030 parcels out of 6,822 parcels) is either mismatched or missing. It covers almost 19.3%($3.4km^2$ of $17.6km^2$) of total farmland. In order to solve these problems, it is necessary to prepare a multifaceted plan including cadastral map. Comparative analysis of the cultivated crop registered in the agricultural farm business and the field survey agreed only in 3,622 parcels in total 6,822 parcels whereas 3200 parcels disagree. Among these disagreed parcels 2,030(29.8%) have been confirmed as unregistered farm business entity. Accuracy of cultivated crop registered in agricultural farm business agreed in 75.6% cases. Especially the paddy field registration is more accurate that other crops. These discrepancies can lead to false payment in agricultural farm business. For exploration and analysis of regional resources, UAV images can be used together with farm business management database and cadastral map to get a clearer grasp over on-site resources and conditions.

Unmaned Integration Control of Intelligent Robot with Automatic Teaching Function for Assembling Process Automation (조립공정 자동화를 위한 자동교시기능을 갖는 지능형 로봇 무인 통합제어)

  • 한성현
    • Journal of the Korean Society of Manufacturing Technology Engineers
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    • v.11 no.2
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    • pp.49-57
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    • 2002
  • 본 연구에서는 전자부품의 자동조립라인에서 매우 중요한 작업인 열코킹 검사, 납땜 및 납땜검사 작업공정을 보다 더 정밀하고 유연하게 수행할 수 있도록 오프라인 프로그램에의 자동교시기능을 갖는 지능형 로봇 제어 시스템 개발에 대한 연구를 수행하였다. 카메라 백 카바등의 전자부품의 자동조립라인은 작업의 난이도가 매우 높고, 고정밀도가 요구되고, 특히, 납펌 및 납땜 불량검사 작업의 셀은 전체 작업 셀 공정중에서 가장 불량률이 높다. 따라서 본 연구는 기존의 납땜 및 검사공정 셀의 구조를 개선하여 보다 더 높은 정밀도를 유지할 수 있고, 모델 변경에 대한 유연성 향상 및 불량율의 감소를 통한 시스템의 신뢰성을 증대시키기 위한 목적으로 수행된다. 이의 실현을 위한 세부내용으로는 셀의 구조개선, 로봇의 모델교체 및 성능향상, 고정도의 납땜 및 검사 기술, 오프라인 프로그래밍 (off-line programming, OLP)을 이용한 자동교시기법을 개발하여 지능형 시스템으로 새로운 셀을 구성하고, 이를 실제 카메라 백 카바등의 전자부품 조립 라인에 설치하여 실시간 구현을 실현하고자 한다.

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Red Tide Monitoring for Fish Farm Using Long-Endurance UAV (장기 체공형 무인기를 이용한 양식장에 대한 적조 모니터링)

  • Song, Moon-Soo;Yun, Hong-Sik;Kim, Gwang-Bae;Kim, Tae-Woo
    • Proceedings of the Korean Society of Disaster Information Conference
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    • 2016.11a
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    • pp.426-427
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    • 2016
  • 본 논문에서는 Unmaned Aerial Vehicle(UAV)를 이용하여 양식어장에 유입될 수 있는 적조 모니터링에 대한 연구를 실시하였다. 적조는 한반도 주변 해역을 포함한 전 세계 연안 지역에서 물고기의 집단 폐사, 해안구조물에 대한 물리적 손상등과 같이 사회 경제적인 피해를 야기 시켜왔고, 최근 해수면 온도상승과 같은 기후 변화에 의한 영향으로 증가되고 있는 실정이다. 특히 남해안과 같이 생활하수가 다량 유입되고 저층에 퇴적된 영양물질이 용출되는 곳에서 상습적으로 발생한다. 1995년에 발생한 코클로디니움에 의한 적조는 764억원의 기록적인 피해를 입히면서, 적조에 대한 신속한 대응과 효과적인 방제작업의 필요성이 대두되었다. 이렇게 양식어장 운영에 다양한 문제가 발생이 된 후 대응하는 것보다 모니터링을 통해 사전에 유입을 차단하고 대처하는 연구가 필요하고 판단된다. 원격탐사를 활용한 적조 탐지 및 모니터링 연구는 UAV에서 취득한 RGB color 영상을 통한 적조 추출 및 분석, 시계열 분석을 위한 영상자료 수집, 현장관측 자료와 위성영상에서 추출한 클로로필 농도 비료글 통해 이루어 졌다. 또한 매년 발생하는 적조생물에 관한 속성정보를 통해 적조발생지역에 대한 적조생물종과 국내 연안에서 발생한 적조의 발생 범위 등의 정보를 지리정보기반에 의한 공간분석을 실시하였다.

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On the Development of Modularized Structures for Safety-Critical Systems by Analyzing Components Failure (시스템 구성품의 위험 심각도를 반영한 안전중시 시스템의 설계 모듈화에 관한 연구)

  • Kim, Young Min;Lee, Jae-Chon
    • Journal of the Korea Safety Management & Science
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    • v.16 no.4
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    • pp.11-19
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    • 2014
  • Modern systems development becomes more and more complicated due to the need on the ever-increasing capability of the systems. In addition to the complexity issue, safety concern is also increasing since the malfunctions of the systems under development may result in the accidents in both the test and evaluation phase and the operation phase. Those accidents can cause disastrous damages if explosiveness gets involved therein such as in weapon systems development. The subject of this paper is on how to incorporate safety requirements in the design of safety-critical systems. As an approach, a useful system structure using the method of design structure matrix (DSM) is studied while reflecting the need on systems safety. Specifically, the effects of system components failure are analyzed and numerically modeled first. Also, the system components are identified and their interfaces are represented using a component DSM. Combining the results of the failure analysis and the component DSM leads to a modified DSM. By rearranging the resultant DSM, a modular structure is derived with safety requirements incorporated. As a case study, application of the approach is also discussed in the development of a military UAV plane.