• Title/Summary/Keyword: JASS (Journal of Astronomy and Space Sciences)

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Study on an 8-Wheel Suspension to Enhance the Hill-Climbing Performance for a Planetary Exploration Rover

  • Eom, We-Sub;Lee, Joo-Hee;Gong, Hyun-Cheol;Choi, Gi-Hyuk
    • Journal of Astronomy and Space Sciences
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    • v.31 no.4
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    • pp.347-351
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    • 2014
  • Planetary exploration rovers are likely to make a trip on a winding and sloping road of irregular surfaces to the destination in order to accomplish scientific missions. One of the key technologies for rovers is a suspension for traveling and performing exploration missions; the suspension is an essential area of technology for a stable movement of a rover. In this study, an 8-wheel suspension is designed to enable efficient climbing of slopes on a passage to the destination. For the two front wheels among the eight wheels, the moment at the pivot connecting two wheels is derived when the distance between the wheels and the torque of wheels are same. A test experiment was performed to compare the magnitude of moment according to the change in tilt angle and the position of the pivot. Finally, a suspension design considering the position of the pivot was proposed to enhance the hill-climbing performance.

Computational Analysis of an LOx Supply Line System of an Liquid Rocket Engine (액체로켓엔진 산화제 배관 시스템 전산유동해석)

  • Moon, In-Sang;Moon, Il-Yoon;Lee, Soo-Yong
    • Journal of Astronomy and Space Sciences
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    • v.26 no.4
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    • pp.693-702
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    • 2009
  • A computational fluid analysis was performed on an LOx line system of a liquid rocket engine. The model was created with 3D CAD and imbedded to the 3D CFD program. Before the full scale analysis on the system was carried out, each components with simplified models was analyzed to save time and cost. As a result, the inlet pressure of the gas generator should be compensated with a certain device unless the inlet pressure of the line system is sufficiently high. The flow pattern of the exit of the system was dependant upon the location of the orifice as well as the size. As a whole the line system analyzed met the requirements, and will be tested and confirmed after being manufactured.

N III Bowen Lines and Fluorescence Mechanism in the Symbiotic Star AG Peg

  • Hyung, Siek;Lee, Seong-Jae;Lee, Kang Hwan
    • Journal of Astronomy and Space Sciences
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    • v.35 no.1
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    • pp.7-18
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    • 2018
  • We have investigated the intensities and full width at half maximum (FWHM) of the high dispersion spectroscopic N III emission lines of AG Peg, observed with the Hamilton Echelle Spectrograph (HES) in three different epochs at Mt. Hamilton's Lick Observatory. The earlier theoretical Bowen line study assumed the continuum fluorescence effect, presenting a large discrepancy with the present data. Hence, we analyzed the observed N III lines assuming line fluorescence as the only suitable source: (1) The O III and N III resonance line profiles near ${\lambda}$ 374 were decomposed, using the Gaussian function, and the contributions from various O III line components were determined. (2) Based on the theoretical resonant N III intensities, the expected N III Bowen intensities were obtained to fit the observed values. Our study shows that the incoming line photon number ratio must be considered to balance at each N III Bowen line level in the ultraviolet radiation according to the observed lines in the optical zone. We also found that the average FWHM of the N III Bowen lines was about $5km{\cdot}s^{-1}$ greater than that of the O III Bowen lines, perhaps due to the inherently different kinematic characteristics of their emission zones.

DEVELOPMENT OF MAGNETOMETER DIGITAL CIRCUIT FOR KSR-3 ROCKET AND ANALYTICAL STUDY ON CALIBRATION RESULT (KSR-3 과학 로켓용 자력계 디지털 회로 개발 및 검교정시험 결과 분석 연구)

  • 이은석;장민환;황승현;손대락;이동훈;김선미;이선민
    • Journal of Astronomy and Space Sciences
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    • v.19 no.4
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    • pp.293-304
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    • 2002
  • This paper describes the re-design and the calibration results of the MAG digital circuit onboard the KSR-3. We enhanced the sampling rate of magnetometer data. Also, we reduced noise and increased authoritativeness of data. We could confirm that AIM resolution was decreased less than InT of analog calibration by a digital calibration of magnetometer. Therefore, we used numerical-program to correct this problem. As a result, we could calculate correction and error of data. These corrections will be applied to magnetometer data after the launch of KSR-3.

METHODOLOGY TO ENHANCE THE PREDICTABILITY OF I/O DATA EXCHANGE BETWEEN DEVICE AND TASKS (장치와 태스크 간 입출력 데이터 교환의 예측성 향상 방안)

  • Koo, Cheol-Hea;Yang, Koon-Ho;Choi, Seong-Bong
    • Journal of Astronomy and Space Sciences
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    • v.24 no.4
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    • pp.451-456
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    • 2007
  • Data coming from devices shall be transported to a specific task to be used in a software with the most accurate time and data integrity. During this process, a potential cause for invoking structured hazard and performance degradation is dormant. In this paper, a method which can protect the data integrity from the possible data corruption when collision has happened during I/O data exchange between device and tasks is presented. Also, an example diagram of mechanism according to the method is shown and the effect, merits and demerits of the method is evaluated.

Orbit Prediction using Broadcast Ephemeris for GLONASS Satellite Visibility Analysis (GLONASS 위성 가시성 분석을 위한 방송궤도력 기반 궤도 예측)

  • Kim, Hye-In;Park, Kwan-Dong
    • Journal of Astronomy and Space Sciences
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    • v.26 no.2
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    • pp.199-210
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    • 2009
  • Even though there are several Global Navigation Satellite Systems under development, only GPS and GLONASS are currently available for satellite positioning. In this study, GLONASS orbits were predicted from broadcast ephemeris using the 4th-order Runge-Kutta numerical integration. For accuracy validation, predicted orbits were compared with precise ephemeris. The RMS(Root Mean Square) and maximum 3-D errors were 14.3 km and 17.4 km for one-day predictions. In case of 7-day predictions, the RMS and maximum 3-D errors were 15.7 and 40.1 km, respectively. Also, the GLONASS satellite visibility predictions were compared with real observations, and they agree perfectly except for several epochs when the satellite signal was blocked by nearby buildings.

Automatic Clock and Time Signal System of the Astronomical Agency in East Asia Area (동아시아 천문관서의 자동 시보와 타종장치 시스템의 고찰 - 수운의상대, 자격루, 옥루, 송이영 혼천시계 등을 중심으로 -)

  • Lee, Yong-Sam;Kim, Sang-Hyuk;Jeong, Jang-Hae
    • Journal of Astronomy and Space Sciences
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    • v.26 no.3
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    • pp.355-374
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    • 2009
  • We analysed the old automatic clock and time signal system that was used by the national astronomical agency in East Asian Area. Jagyeongnu is a kind of water clock that was operated by the flowing water in Joseon Dynasty. Seowoongwan managed the water clock so as to keep the standard time system in the dynasty from the 16th year (1434) of King Sejong's reign. In 1438 the Okru that was invented in the period. Such kind of clock system already was used in China, which was Shui $y\ddot{u}n$ i hsiang t'ai (水運儀象壹) in 1092. During the period Joseon Dynasty, China and Japan had been kept the time system that one day is divided into 12 shin (12辰) or 100 gak (刻). However detailed part of the system had a little difference among the three countries. Though the whole system of water clock in Joseon had manufactured on the basis of Chinese, it had been gradually developed by own method and idea. In this study we show the historical records of the standard time keeping system in East Asian history. And then we can inform materials on the structure and functional devises for the purpose of new restoration models about the automatic clock and time system.

MULTI-SENSOR DATA FUSION FOR FUTURE TELEMATICS APPLICATION

  • Kim, Seong-Baek;Lee, Seung-Yong;Choi, Ji-Hoon;Choi, Kyung-Ho;Jang, Byung-Tae
    • Journal of Astronomy and Space Sciences
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    • v.20 no.4
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    • pp.359-364
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    • 2003
  • In this paper, we present multi-sensor data fusion for telematics application. Successful telematics can be realized through the integration of navigation and spatial information. The well-determined acquisition of vehicle's position plays a vital role in application service. The development of GPS is used to provide the navigation data, but the performance is limited in areas where poor satellite visibility environment exists. Hence, multi-sensor fusion including IMU (Inertial Measurement Unit), GPS(Global Positioning System), and DMI (Distance Measurement Indicator) is required to provide the vehicle's position to service provider and driver behind the wheel. The multi-sensor fusion is implemented via algorithm based on Kalman filtering technique. Navigation accuracy can be enhanced using this filtering approach. For the verification of fusion approach, land vehicle test was performed and the results were discussed. Results showed that the horizontal position errors were suppressed around 1 meter level accuracy under simulated non-GPS availability environment. Under normal GPS environment, the horizontal position errors were under 40㎝ in curve trajectory and 27㎝ in linear trajectory, which are definitely depending on vehicular dynamics.

FIMS WAVELENGTH CALIBRATION VIA AIRGLOW LINE OBSERVATIONS (대기광 관측을 통한 과학기술위성 1호 원자외선분광기(FIMS)의 파장 보정)

  • Lee, Dae-Hee;Seon, Kwang-Il;Park, Jang-Hyun;Jin, Ho;Yuk, In-Soo;Nam, Uk-Won;Han, Won-Yong;Park, Jae-Woo;Lee, Ji-Na;Ryu, Kwang-Sun;Min, Kyoung-Wook
    • Journal of Astronomy and Space Sciences
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    • v.21 no.4
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    • pp.391-398
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    • 2004
  • Far-ultraviolet Imaging Spectrograph (FIMS) is the main payload of the Korea's first scientific micro satellite STSAT-1, which was launched at Sep. 27 2003 successfully. Major objective of FIMS is observing hot gas in the Galaxy in FUV bands to diagnose the energy flow models of the interstellar medium. Supernova remnants, molecular clouds, and Aurora emission in the geomagnetic pole regions are specific targets for pointing observation. Although the whole system was calibrated before launch, it is essential to perform on-orbit calibration for data analysis. For spectral calibration, we observed airglow lines in the atmosphere since they provide good spectral references. We identify and compare the observed airglow lines with model calculations, and correct the spectral distortion appeared in the detector system to improve the spectral resolution of the system.

A Case Study in the Mars Landing Site Selection for Science Objects

  • Seo, Haingja;Kim, Eojin;Kim, Joo Hyeon;Lee, Joo Hee;Choi, Gi-Hyuk;Sim, Eun-Sup
    • Journal of Astronomy and Space Sciences
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    • v.29 no.4
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    • pp.375-380
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    • 2012
  • It is a crucial matter to select a landing site for landers or rovers in planning the Mars exploration. The landing site must have not only a scientific value as a landing site, but also geographical features to lead a safe landing for Mars probes. In this regard, this study analyzed landing site of Mars probes and rovers in previous studies and discussed the adequacy of the landing site to scientific missions. Moreover, this study also examined domestic studies on the Mars. The frameworks of these studies will guide the selection of exploration sites and a landing site when sending Mars probe to the Mars through our own efforts. Additionally, this paper will be used as the preliminary data for selection of exploration site and a landing site.