• Title/Summary/Keyword: 테더

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Secure Tethering Method through Enhanced Authentication for Mobile Communication (향상된 인증기법을 통한 안전한 모바일 테더링 기법)

  • Park, Tae-Sung;Kim, Sung-Yoon;Jun, Moon-Seog
    • Proceedings of the Korean Information Science Society Conference
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    • 2010.06d
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    • pp.81-84
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    • 2010
  • 테더링 서비스(Tethering Service)는 인터넷에 연결된 모바일 장비가 스스로 중계기 역할을 하여 주변의 테더링을 사용하는 장비에 인터넷 접속을 가능케 하는 서비스이다. 즉, 별도의 모무선 모뎀 없이 이동전화를 PC나 휴대기기에 연결해 언제 어디서든 무선 인터넷을 이용할 수 있도록 하는 것이다. 이러한 테더링은 방식에 따라 블루투스, USB 케이블 연결, 무선랜 등이 사용되고 있으며, 이용자들은 스마트 단말기에 노트북 PC를 연결하여 인터넷 서비스를 이용한다. 테더링은 최근 OS3.0이 탑재되어 출시된 스마트 단말기에 테더링 기능이 지원되면서 관심이 급증하고 있다. 그러나 이러한 테더링의 확산은 유저들 사이에선 스마트 단말기 해킹 사이트를 통해 무료로 테더링 서비스를 이용할 수 있는 방법들이 유포되고 있으며, 부적절한 접속 방식으로 인해 사용자가 아닌 다른 유저한테 과금이 청구되는 사례도 있다. 테더링 통신 과정 중 거치는 장비들의 정보를 조작, 변조, 삭제 등이 가능하다. 따라서 본 논문에서는 무선 테더링에서의 상호인증을 통한 안전한 테더링 기법을 제안한다.

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Nonlinear Dynamic Analysis of a Satellite with Tether Conveying Fluid (유체가 이송하는 테더가 있는 인공위성의 동특성 분석)

  • Jung, Won-Young;Lee, Kyu-Ho;Chung, Jin-Tai
    • Transactions of the Korean Society for Noise and Vibration Engineering
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    • v.21 no.8
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    • pp.691-697
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    • 2011
  • The purpose of this study is to analyze nonlinear dynamics of a tethered satellite. The coupled non-linear equations of motion are derived by using the extended Hamilton's principle with the polar coordinate system. In order to analyze the response of tethered satellite, time responses are computed by the Newmark's time integration method. We also investigate the dynamic behavior of the system and the effects of length of tether, tip mass and conveyed fluid through the tether with time variation.

Nonlinear Dynamic Analysis of a Tethered Satellite (테더가 있는 인공위성의 비선형 동역학 해석)

  • Lee, Kyu-Ho;Jung, Won-Young;Chung, Jin-Tai
    • Transactions of the Korean Society for Noise and Vibration Engineering
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    • v.21 no.5
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    • pp.416-421
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    • 2011
  • The purpose of this study is to analyze nonlinear dynamics of a tethered satellite. The nonlinear equations of motion are derived by using Lagrange's equations with the polar coordinate system. In order to analyze the response of tethered satellite, time responses are computed by the Newmark's time integration method. This paper claims that the dynamic behavior of the system is changed by the effect of length of tether, mass ratio of satellites.

A Development of Active Vent Airbag for the Passenger New NCAP (동승석 최고 충돌성능 달성을 위한 액티브 벤트 에어백 기술 개발)

  • Yoo, Jaehaeng;Shin, Hyoseup;Kim, Taein;Bae, Hanil;Lee, Seungwoo
    • Journal of Auto-vehicle Safety Association
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    • v.5 no.1
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    • pp.31-36
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    • 2013
  • For the robust passenger NCAP 5star and the stable neck injury performance, a new concept of passenger airbag has been required strongly. Especially, the deployment stability and the vent hole control technology of the passenger airbag should be improved. According to these requirements, the deployment stability technique has been studied and the 'Active Vent' technology has been developed. As a result, these technologies have led to achieve the robust NCAP rating and are applied to the production vehicles.

A Dynamic Analysis of Tension-Legged Circular Cylinder in Irregular Waves (인장계류된 원통형 실린더의 동적 거동 해석)

  • Hwang, Jae-Hyuck;Jo, Hyo-Jae;Kwon, Kang-Il
    • Journal of the Korean Society of Fisheries and Ocean Technology
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    • v.38 no.4
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    • pp.259-264
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    • 2002
  • The technology development for ocean resources can be represented by the increase of water depth. TLP, Tension Leg Platform, is one of the most feasible systems for deep sea development. TLPs show a complex dynamic behavior resulting from the dynamic interactions among platform, tether system and riser system due to their hydrodynamic and structural dynamic characteristics in waves. This paper aims at the theoretical and experimental analysis on motion response of TLP in waves. It is composed of two parts as follows ;(1) wave and wave loadings (2) TLP motion.

A Design of the Multiple Moving Objects Tracking Technology using WiFi Technique (WiFi 기술을 활용한 이동 객체 위치 추적 기술 설계)

  • Lee, Hyoun-Sup;Kim, Jin-Deog
    • Proceedings of the Korean Institute of Information and Commucation Sciences Conference
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    • 2012.05a
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    • pp.104-106
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    • 2012
  • WPS(WiFi Positioning System)는 무선 AP의 정보를 통해 현재 이동 객체의 위치를 찾는 시스템이다. 일반적으로 WPS는 실내외에 존재하는 고정 AP 신호 세기 특징을 활용하여 무선 LAN을 보유한 이동 객체가 현재 자신의 위치를 판단할 때 사용된다. 그러나 지금까지 WPS 기술을 대량의 이동객체를 관리하기 위한 목적으로 활용한 연구는 거의 없다. 본 논문은 스마트폰 환경에서 WPS의 기능과 테더링을 응용하여 대량의 이동객체의 이탈을 판단하기 위한 기법과 이를 확장하여 위치까지 추적할 수 있는 시스템에 대하여 제안한다.

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A study on Development of 300m Class Underwater ROV (300m급 수중ROV 개발에 관한 연구)

  • 이종식;이판묵;홍석원
    • Journal of Ocean Engineering and Technology
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    • v.8 no.1
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    • pp.50-61
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    • 1994
  • A 300 meter class ROV(CROV300) is composed of three parts : a surface unit, a tether cable and an underwater vehicle. The vehicle controller is based on two processors : an Intel 8097-16-bit one chip micro-processor and a Texas Instruments TMS320E25 digital signal processor. In this paper, the surface controller, the vehicle controller and peripheral devices interfaced with the processors are described. These controllers transmit/receive measured status data and control commands through RS422 serial communication. Depth, heading, trimming, camera tilting, and leakage signals are acquired through the embedded AD converters of the 8097. On the other hand, altitude of ROV and lbstacle avoidance signals are processed by the DSP processor and periodically fetched by the 8097. The processor is interfaced with a 4-channel 12-bit D/A converter to generate control signals for DC motors an dseveral transistors to handle the relays for on/off switching of external devices.

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Analysis of 32m aerostat gust load using non-linear cable equation (비선형 테더 방정식을 이용한 에어로스탯 돌풍하중해석)

  • Kang, Wang-Gu;Lee, In;Kim, Dong-Min
    • Proceedings of the KSME Conference
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    • 2008.11a
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    • pp.757-761
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    • 2008
  • The aerostat dynamic equation of motion has been built including the tether cable dynamic effects. A numerical program to solve the derived equation of motion has been developed. The dynamic motion of the 32m aerostat has been analyzed under discrete gust and continuous turbulence. The aerostat behaviors under discrete gust which represents a deterministic approach for determining design loads for manned aircraft are solved to verify the effect of aerostat mechanical properties on the aerostat dynamic behavior. Continuous turbulences are simulated for each given altitude, translational mean wind velocity and gust intensity. Dynamic behaviors of the 32m aerostat are simulated for each continuous turbulence conditions. Translational and vertical velocity and pitching behavior and tether reaction force are monitored for each simulation.

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