• Title/Summary/Keyword: 탑재

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A Study on the Activity Recognition Touch Interface Using the EMG Sensing Wearable Device. (근전도 센서 탑재 웨어러블 디바이스를 활용한 행위 인지 터치 인터페이스에 대한 연구)

  • Moon, Ju-Hwan;Hong, Yeo-Jin;Song, Meoung-Jin;Yang, Dong-Ho;Kim, Keun-Hyung
    • Proceedings of the Korea Information Processing Society Conference
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    • 2015.04a
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    • pp.1061-1064
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    • 2015
  • 본 논문은 근전도 센서가 탑재된 손목착용형 웨어러블 디바이스를 통하여 스마트폰의 입력방식을 개선시켜 사용자와 스마트폰간의 인터렉션을 보다 발전시킨 시스템을 다룬다. 이 시스템은 사용자가 손목에 착용한 웨어러블 디바이스에 탑재된 근전도센서를 통하여 손의 고유근의 근전도를 측정함으로서 사용자의 엄지와 검지에 가해지는 힘을 탐지하고 이를 바탕으로 사용자가 스마트폰을 터치했을 경우 해당 터치행위가 사용자가 스마트폰을 의도적으로 힘을 가하여 누른 행위인지에 대한 여부를 판단할 수 있다. 결과적으로 본 논문은 스마트폰과 사용자와의 인터렉션에 있어 근전도 센서를 탑재한 웨어러블 디바이스를 활용하여 사용자의 의도를 보다 효과적으로 스마트폰 제어에 반영시킬 수 있는 행위 인지(Activity Recognition) 터치 인터페이스 시스템을 제안한다.

The Flight Test of the KSLV-I Electronic Systems Using a Light Airplane (경항공기를 이용한 KSLV-I 전자탑재장비 비행시험)

  • Ji, Ki-Man;Lee, Soo-Jin;Chung, Eui-Seung
    • Aerospace Engineering and Technology
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    • v.7 no.1
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    • pp.142-150
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    • 2008
  • In order to ensure the individual and mutual performances among the telemetry system, tracking system, flight termination system, GPS, and inertial navigation & guidance system which are installed in the KSLV-I 2nd stage and ground equipment of the Naro space center, flight test using a light airplane is required. Since the high degree of test efficiency is fulfilled through the minute plan and analysis about selection of the equipment which are applicable to the test, harness, operation strategy, and antenna installation. KSLV-I communication environment and flight profile should be precisely taken into account during the flight test. In this document, overall aspect of the KSLV-I 2nd stage equipment specification, a rack for the installation, harness, the airplane specification, and flight route which are required for the effective flight test are presented.

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Mechanical Interface Design of Optical Pay loads in a GEO Multi-Functional Satellite (정지궤도 복합위성의 광학탑재체 기계접속설계)

  • Park, Jong-Seok;Kim, Chang-Ho;Jeon, Hyung-Yoll;Kim, Sung-Hoon
    • Aerospace Engineering and Technology
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    • v.7 no.1
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    • pp.99-107
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    • 2008
  • The COMS is a kind of geostationary multi-functional satellites with three different mission objectives. Two of them aim at earth observation and the COMS has two optical payloads according to those missions. The payloads are composed of a meteo imager and an ocean color imager, and their inherent characteristics require optimal interface design for their performance to be concurrently achieved. Therefore, various kinds of constraints are considered in their component accommodation on the COMS platform. This paper shows a general overview of the optical payload accommodation design and describes the design consideration to achieve the optimized performance from thermal and mechanical point of view.

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Study on Polymer Electrolyte Membrane Fuel Cell for UAV Applications (고분자 전해질막 연료전지의 무인항공기 탑재화 연구)

  • Kim, Jin-Cheol;Kim, Sung-Uk;Kim, Dong-Min;Kim, Tae-Gyu
    • Proceedings of the Korean Society of Propulsion Engineers Conference
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    • 2012.05a
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    • pp.153-156
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    • 2012
  • The optimization and integration of a fuel cell were performed to improve the performance and reliability of the fuel cell in this paper. To improve the performance of the PEMFC, current and voltage of the fuel cell were measured using an electrical load, and the results was compared and analyzed with the data of a commercial fuel cell. Based on the above results, a controller for a fuel cell UAV applications was designed, and the fuel cell control algorithm was developed to optimize the performance of the fuel cell UAV.

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A Survey on the Software Technology of Health Management System for Aircraft Gas Turbine Engine (항공기용 가스터빈 엔진의 건전성 관리를 위한 소프트웨어 발전 동향)

  • Park, Iksoo;Ki, Taeseok;Kim, Junghoe;Min, Seongki
    • Journal of the Korean Society of Propulsion Engineers
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    • v.22 no.5
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    • pp.13-21
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    • 2018
  • Technology trends of onboard and ground health management system software for aircraft gas turbine engines are surveyed. The software has changed from ground based software for fault detection and identification to a model based health identification technology for onboard software. This advanced algorithm is currently under development in a technically advanced country while domestic research is on the birth stage. This paper suggested that the optimal development plan of the software considering current technology state.

Vulnerabilities Analysis of the OTP Implemented on a PC (PC에 탑재된 OTP의 취약점 분석)

  • Hong, Woo-Chan;Lee, Kwang-Woo;Kim, Seung-Joo;Won, Dong-Ho
    • The KIPS Transactions:PartC
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    • v.17C no.4
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    • pp.361-370
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    • 2010
  • OTP(One Time Password) is a user authentication using secure mechanism to authenticate each other in a way to generate a password, an attacker could intercept the password to masquerade as legitimate users is a way to prevent attacks. The OTP can be implemented as H/W or S/W. Token and card type OTP, implemented as H/W, is difficult to popularize because of having problem with deployment and usability. As a way to replace it implemented as S/W on Mobile or PC is introduced. However, S/W products can be target of malicious attacks if S/W products have vulnerability of implementation. In fact, FSA said the OTP implemented on a mobile have vulnerability of implementation. However, the OTP implemented on a PC have no case about analysis of vulnerability. So, in this paper derive security review and vulnerabilities analysis of implemented on a PC.

Development Trend of Geostationary Environment Monitoring Payloads (환경감시용 정지궤도위성 탑재센서 개발동향)

  • Lee, Seung-Hoon;Kim, Sung-Kyu;Yeon, Jeoung-Heum;Kim, Seong-Hui;Ko, Dai-Ho;Yong, Sang-Soon
    • Current Industrial and Technological Trends in Aerospace
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    • v.8 no.2
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    • pp.31-38
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    • 2010
  • Environment and climate changes affect all aspects of our society. The enhanced remote sensing technology made the satellite to be widely used in the environment monitoring applications. Geostationary environmental monitoring is also actively researched due to the increased needs for the monitoring of diurnal environmental changes, troposhperic pollution and its origin. In this paper, recent development trends of geostationary environment monitoring payloads are introduced. GEO-CAFE and GIFTS missions are researched by the leading of the NASA and Sentinel-4 by the ESA. Those missions are in the state of detailed conceptual design and hardware development preparing with the launch plan in the late 2010s. By considering these development trends, domestic environment monitoring payloads shall be developed with careful analysis on the mission and data application.

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Environment Simulation and Effect Estimation of Space Radiation for COMS Communication Payload (통신해양기상위성 통신 탑재체의 우주 방사선 환경 모사 및 영향 추정)

  • Kim, Seong-Jun;U, Hyeong-Je;Seon, Jong-Ho
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.34 no.11
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    • pp.76-83
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    • 2006
  • Space radiation environment for COMS is simulated by NASA AP8/AE8, JPL91 and NRL CREME models, respectively for trapped particle, solar proton and cosmic-ray. The radiation effects on electronic devices in communication payload are also estimated by using simulation results. Dose-depth curve and LET spectrum are calculated for estimating total ionizing dose(TID) effect and single event effect(SEE) respectively. Spherical sector method is applied to dose estimation at each position in the units of communication payload to consider shielding effect of platform and housing. Total ionizing dose at each position varies by 8 times through shielding effect under the same external space radiation environment.

Development of Single Board Computer (SBC) for Nano/Pico Small Satellites (초소형위성용 단일보드 탑재컴퓨터의 개발)

  • Kim, Young-Hyun;Moon, Byoung-Young;Lee, Bo-Ra;Chang, Young-Keun
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.32 no.4
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    • pp.101-110
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    • 2004
  • Flight and Qualification Models of Single Board Computer (SBC), called On-Board Computer (OBC), for HAUSAT-l picosatellite, which is scheduled to launch on September, 2004 by Russian "Dnepr" launch vehicle, have been developed. The OBC of HAUSAT-1 has been designed with some improved features compared to other picosatellites. A multifunctional controller and up-to-date SPI (Serial Peripheral Interface) and 1-Wire interface are implemented to simplify the harness routing and to minimize the mass and size of OBC. The improved fault-tolerant architecture design methodology is incorporated in the HAUSAT-1 OBC to protect against space radiation environment. The functions of the OBC were fully tested and verified by the Electrical Test Bed (ETB) model. This paper is also addressing the environmental test results, such as random vibration and thermal vacuum tests.

DEVELOPMENT OF THE SOLAR EUV TELESCOPE ENGINEERING MODEL FOR A SATELLITE (인공위성 탑재용 극자외선 태양망원경(EUVT) EM 개발)

  • 이선민;장민환;이은석
    • Journal of Astronomy and Space Sciences
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    • v.20 no.4
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    • pp.327-338
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    • 2003
  • The aim of this paper is to describe the results of the study on the extreme-ultra-violet (EUV) solar telescope, which is designed to. a possible satellite mission. Since the EUV band can not be observed on the ground, the observation in EUV should be performed in space using a satellite or a rocket. Design of the Extreme-Ultra-Violet solar Telescope (BUVT) in this study is based on "Designing a small-sized engineering model of solar EUV telescope for a Korean satellite" (Han et al. 2001). Our EUVT design is satisfied with the requirements for a satellite in size and input voltage. The major goal of the study is to confirm if we can detect the specific wavelength (58.4nm to 62.9nm) with the EUVT. We describe re-designing of the EUVT to decrease a shelter ratio. Also we describe the technics in the optic system and the detector, which were used to manufacture the EUVT. We explain the detective program, which is to calculate the amount of the solar radiation, and the image data processing system.ng system.