• 제목/요약/키워드: Team Mission Project

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주니어 공학 팀 미션 프로젝트 교육프로그램 및 교재 개발과 적용 효과 (A Study on Development and Application Effect of Junior Engineering Team Mission Project Education Program and Workbook)

  • 최유현;박기문;임윤진;임병웅
    • 공학교육연구
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    • 제14권3호
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    • pp.15-24
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    • 2011
  • The purpose of this study is to develop the 'Engineering Team Mission Project Education Program and Textbook', which is improved creativity and creative problem for Juniors(middle school students) that is in the growth stage to become the leading role in future society. This can be applied the creative experience activities time of revised curriculum in 2009 being implemented to secondary education by 2011. The results of this study are as follows. The formation of Team Mission Project Education Program is the big field 2 project, lower field 8 module and 38 total lessons. This education program has secured the validity of the SME(Subject Matter Expert) expert conference. Actually, by putting the education program and textbook to the invention talent class formed by middle school students and by normally analyzing, it has been analyzed as very satisfying result. Therefore, the "Engineering Team Mission Project Education Program and Textbook" can be provided as a practical education course of new talent training and engineering talent model of the nation's knowledge property education. And it can perform as an education program using usefully in the creative experience activity education course in middle class education stage. Also, it is concluded to become the basis of engineering design education's high grade education and department of engineering's creative engineering.

THE NEXT-GENERATION INFRARED SPACE MISSION SPICA: PROJECT UPDATES

  • Nakagawa, Takao;Shibai, Hiroshi;Kaneda, Hidehiro;Kohno, Kotaro;Matsuhara, Hideo;Ogawa, Hiroyuki;Onaka, Takashi;Roelfsema, Peter;Yamada, Toru;SPICA Team
    • 천문학논총
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    • 제32권1호
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    • pp.331-335
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    • 2017
  • We present project updates of the next-generation infrared space mission SPICA (Space Infrared Telescope for Cosmology and Astrophysics) as of November 2015. SPICA is optimized for mid- and far-infrared astronomy with unprecedented sensitivity, which will be achieved with a cryogenically cooled (below 8 K), large (2.5 m) telescope. SPICA is expected to address a number of key questions in various fields of astrophysics, ranging from studies of the star-formation history in the universe to the formation and evolution of planetary systems. The international collaboration framework of SPICA has been revisited. SPICA under the new framework passed the Mission Definition Review by JAXA in 2015. A proposal under the new framework to ESA is being prepared. The target launch year in the new framework is 2027/28.

SAT#1 (Preliminary Integration) Test Results of KASS System

  • Jeong, Hwanho;Jang, HyunJin;Kim, Koontack;Lee, Jaeeun;Lee, ByungSeok
    • Journal of Positioning, Navigation, and Timing
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    • 제10권2호
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    • pp.145-151
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    • 2021
  • According to the Korea Augmentation Satellite System (KASS) system milestone, Site Acceptance Test (SAT) has three steps test until the end of the project. SAT#1 is the first time of SAT steps and verify the KASS Reference Station (KRS) and Sub System (S/S) for the monitoring and controllable. After the equipment and software were installed at the Mission Control Center (MCC) with Central Monitoring and Control Simulator (CMS) for the SAT#1, the 1:1 test was progressed when the KRS and S/S are ready to test. SAT#1 has a 10 steps test case and it was progressed each KRS sites. The test was finished throughout the real-time monitoring and the data collection including the data analysis all of the 7 KRS sites. Finally SAT#1 was completed on December 2020 with successfully.

THE AKARI PROJECT: LEGACY AND DATA PROCESSING STATUS

  • NakagawaI, Takao;Yamamura, Issei
    • 천문학논총
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    • 제32권1호
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    • pp.5-9
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    • 2017
  • This paper provides an overview of the AKARI mission, which was the first Japanese satellite dedicated to infrared astronomy. The AKARI satellite was launched in 2006, and performed both an all-sky survey and pointed observations during its 550 days in the He-cooled mission phases (Phases 1 and 2). After the He ran out, we continued near-infrared observations with mechanical cryocoolers (Phase 3). Due to a failure of its power supply, AKARI was turned off in 2011. The AKARI data are unique in terms of the observed wavelengths as well as the sky coverage, and provide a unique legacy resource for many astronomical studies. Since April 2013, a dedicated new team has been working to refine the AKARI data processing. The goal of this activity is to provide processed datasets for most of the AKARI observations in a Science Ready form, so that more users can utilize the AKARI data in their astronomical research. The data to be released will include revised All-Sky Point Source Catalogues, All-Sky Image Maps, as well as high-sensitivity images and spectra obtained by pointed observations. We expect that the data will be made public by in the Spring of 2016.

A Conceptual Design of HAUSAT-1(CubeSat) Satellite

  • Kim, Joon-Tae;Kim, Young-Suk;Seo, Seung-Won;Kim, Young-Hyun;Chang, Young-Keun
    • International Journal of Aeronautical and Space Sciences
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    • 제3권1호
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    • pp.61-73
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    • 2002
  • This paper addresses the conceptual design results of the HAUSAT-1 (Hankuk Aviation University SATellite-1), developed by Space System Research Lab. of Hankuk Aviation Univ., which is a new generation picosatellite. This project has been funded by Korean Government for the purpose of developing the space core technology. This is the first attempt at the level of university in Korea to develop the satellite weighing less than 1kg and accelerates opportunities with low construction, low launch cost space experiment platforms. The purpose of the HAUSAT-1 project is to offer graduate and undergraduate students great opportunities to be able to understand the design process of satellite development as a team member. Its mission objectives are to track its position by the GPS receiver system, to deploy the thin film solar cell panel to generate extra power, and to measure plasma density and temperature with the plasma sensor. The HAUSAT-1 will orbit at the altitude of 650 km with 65 degree inclination angle with 12 months of design mission life. It is planned to be launched on November 2003 by Russian launch vehicle "Dnepr".

Status of KASI's Contribution to SPHEREx

  • Jeong, Woong-Seob;Yang, Yujin;Park, Sung-Joon;Pyo, Jeonghyun;Jo, Youngsoo;Kim, Il-Joong;Bang, Seungcheol;Lee, Bomee
    • 천문학회보
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    • 제46권2호
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    • pp.53.1-53.1
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    • 2021
  • The KASI team are participating in the NASA MIDEX mission (PI Institute: Caltech), the all-sky infrared spectro-photometric surveyor SPHEREx (Spectro-Photometer for the History of the Universe, Epoch of Reionization, and Ices Explorer). The SPHEREx will provide us the first all-sky infrared spectro-photometric data set to probe the origin of our Universe, to explore the origin and evolution of galaxies, and to explore whether planets around other stars could harbor life. After the project PDR (Preliminary Design Review) was successfully passed on the last September, the fabrication of flight hardware is in progress. As an international partner, KASI deeply involved in all fields of projects, i.e., the development of calibration facility, the construction of data reduction modules and the science studies for the SPHEREx. After finishing the fabrication and test of calibration facility for the SPHEREx in this year, it will be delivered to Caltech. Here, we report the status of the SPHEREx project and the progress in the Korean participation.

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DATA REDUCTION OF AKARI/IRC SPECTROSCOPIC OBSERVATIONS

  • Usui, Fumihiko;Onaka, Takashi;AKARI/IRC team
    • 천문학논총
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    • 제32권1호
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    • pp.41-43
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    • 2017
  • AKARI performed about 10,000 spectroscopic observations with the Infrared Camera (IRC) during its mission phase. These IRC observations provide unique spectroscopic data at near- and mid-infrared wavelengths for studies of the next few decades because of its high sensitivity and unique wavelength coverage. In this paper, we present the current status of the activity for improving the IRC spectroscopic data reduction process, including the toolkit and related data packages, and also discuss the goal of this project.

Case study on the Accuracy Assessment of the rainrate from the Precipitation Radar of TRMM Satellite over Korean Peninsula

  • Chung, Hyo-Sang;Park, Hye-Sook;Noh, Yoo-Jeong
    • 대한원격탐사학회:학술대회논문집
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    • 대한원격탐사학회 1999년도 Proceedings of International Symposium on Remote Sensing
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    • pp.103-106
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    • 1999
  • The Tropical Rainfall Measuring Mission(TRMM) is a United States-Japan project for rain measurement from space. The first spaceborne Precipitation Radar(PR) has been installed aboard the TRMM satellite. The ground based validation of the TRMM satellite observations was conducted by TRMM science team through a Global Validation Program(GVP) consisted of 10 or more ground validation sites throughout the tropics. However, TRMM radar should always be validated and assessed against reference data to be used in Korean Peninsula because the rainrates measured with satellite varies by time and space. We have analyzed errors in the comparison of rainrates measured with the TRMM/PR and the ground-based instrument i.e. Automatic Weather System(AWS) by means of statistical methods. Preliminary results show that the near surface rainrate of TRMM/PR are highly correlated with ground measurements especially for the very deep convective rain clouds, though the correlation is changed according to the type and amount of precipitating clouds. Results also show that TRMM/PR instrument is inclined to underestimate the rainrate on the whole over Korea than the AWS measurement for the cases of heavy rainfall.

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소나 센서를 이용한 소형 ROV의 위치제어시스템에 관한 연구 (A Study On the Position Control System of the Small ROV Using Sonar Sensors)

  • 최동현;임근남;김상현
    • 대한조선학회논문집
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    • 제45권6호
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    • pp.579-589
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    • 2008
  • In the past few years, there are many studies and researches of the underwater vehicles which are carried out its mission using sonar sensors. MSCL(Marine System Control Lab.) at Inha University developed test-bed small ROV, ISRO. ISRO is an open-frame type and has 4 thrusters. ISRO can control 4 motions i.e surge, sway, yaw and heave with sonar sensors. ISRO is developed for inspection of ship hull, marine structure, plant of lake or river and so on. When ROV ISRO inspects something, it is necessary to control the position of ROV ISRO's for the movement and anti-collision with structures in the underwater. In this paper, we deal with the development of a small ROV and verification of the position control system via simulation and experiment using sonar sensors.

태양위치추적 캔위성의 개발 (Design of Solar Tracking CanSat)

  • 정인지;문지환;김민수;임병덕
    • 한국항공우주학회지
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    • 제41권4호
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    • pp.327-334
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    • 2013
  • 2012년 8월, 교육과학기술부와 KAIST 인공위성 센터 주최로 국내 최초의 캔위성 경연대회가 열렸다. 본 논문은 대학부 최우수 수상팀의 캔위성의 설계에 대한 것으로, 개념설계 단계에서 부터 대회 결과에 이르기까지의 전반적인 내용을 다룬다. 캔위성의 임무는 GPS 정보, 자세정보, 지상 이미지 정보를 송신하는 필수임무와 낙하하는 동안 태양이 떠 있는 방향으로 캔위성의 센서부를 지향하는 창의적인 임무로 구분된다. 센서부가 안정적으로 태양의 위치를 추적할 수 있도록 IMU와 Servo motor를 이용하여 자세제어를 수행하도록 설계하였다. 약 150m 상공에서 캔위성을 낙하시켜 임무 수행을 한 결과, 자세제어와 태양 위치 추적 기능이 성공적으로 수행되었음을 알 수 있었다.