• 항공우주산업기술동향
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• 제7권1호
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• pp.79-88
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• 2009

세계적인 관심이 고조되고 있는 환경 및 기후변화는 사회 전분야에 걸쳐 폭넓게 영향을 미치고 있다. 최근들어, 환경감시의 필요성과 이에 대한 관심의 고조와 더불어 원격탐사기술의 발전으로 인공위성을 이용한 환경감시가 본격화되고 있다. 본 논문에서는 환경감시 탑재체의 개발동향을 살펴본다. 지금까지 개발되었거나 개발되고 있는 환경탑재체들의 주요 규격 및 관측방식, 관측대상 등을 사례별로 조사하여 소개하였다. 하나의 위성으로 전지구 관측을 위하여 저궤도 탑재체를 중심으로 개발이 이루어졌으나, 최근들어 시간해상도의 중요성이 강조되면서 정지궤도 탑재체의 개발도 이루어지고 있다. 또한 관측대상에 따라 자외선, 가시광선, 적외선 등의 탐측대역을 달리한 탑재체가 개발되고 있다. 향후 국내 환경탑재체의 개발은 이러한 추세를 고려하여 명확한 임무분석과 함께 추진되어져야 할 것이다.

• 항공우주기술
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• 제6권2호
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• pp.87-95
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• 2007

통신해양기상위성에 탑재된 해양 및 기상탑재는 서로간의 기계적 섭동에 의한 영상품질 저하가 예상된다. 또한 위치유지 및 휠오프로딩을 위한 추력기 발사시 발생하는 섭등에 의해서도 성능저하가 일어난다. 이러한 간섭 문제를 최소화하기 위한 방편으로서 통신해양기상위성은 운용설계 관점에서 접근하고 있다. 본 논문은 이미지 품질의 저하를 최소화하기 위한 통신해양기상위성의 운용설계를 소개하였다. 통신해양기상위성은 기상 및 해양탑재체, 그리고 Housekeeping의 일정을 최적화하고 기상탑재체의 미러의 움직임을 제한하여 영상품질 저하를 최소화함으로써 사용자의 요구를 최대한 만족할 수 있도록 하였다. 또한 운용설계의 결과를 평가하기 위하여 시간여유분석을 소개하였다.

• KSII Transactions on Internet and Information Systems (TIIS)
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• 제15권10호
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• pp.3750-3770
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• 2021

This study investigates open-source dynamic XSS filters used as security devices in web applications to account for the effectiveness of filters in protecting against XSS attacks. The experiment involves twelve representative filters, which are examined individually by placing them into the final output function of a custom-built single-input-form web application. To assess the effectiveness of the filters in their tasks of sanitizing XSS payloads and in preserving benign payloads, a black-box testing method is applied using an automated XSS testing framework. The result in working with malicious and benign payloads shows an important trade-off in the filters' tasks. Because the filters that only check for dangerous or safe elements, they seem to neglect to validate their values. As some safe values are mistreated as dangerous elements, their benign payload function is lost in the way. For the filters to be more effective, it is suggested that they should be able to validate the respective values of malicious and benign payloads; thus, minimizing the trade-off. This particular assessment of XSS filters provides important insight regarding the filters that can be used to mitigate threats, including the possible configurations to improve them in handling both malicious and benign payloads.

• 한국소음진동공학회:학술대회논문집
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• 한국소음진동공학회 2002년도 추계학술대회논문초록집
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• pp.384.1-384
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• 2002

Rocket propulsion systems generate very high level noise (acoustic loads), which is due to supersonic jet of rocket propulsion system. In practice, the sound power level of rocket propulsion systems is over 180 ㏈. This high level noise excites rocket structures and payloads, so that it causes the structural failure and electronic malfunctioning of payloads. Prediction method of acoustic loads of rocket enables us to determine the safety of payloads. (omitted)

• 대한원격탐사학회:학술대회논문집
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• 대한원격탐사학회 2006년도 Proceedings of ISRS 2006 PORSEC Volume I
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• pp.290-293
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• 2006

COMS (Communication, Ocean and Meteorological Satellite) shall be operated with two remote sensing payloads, MI (Meteorological Imager) and GOCI (Geostationary Ocean Color Imager). Since both payloads have rotating mechanisms, the dynamic coupling between two payloads is very important considering the pointing stability during GOCI operation. In addition, COMS adopts a single solar wing to improve the image quality, which leads to the unbalanced solar pressure torque in COMS. As a result, the off-loading of the wheel momentum needs to be performed regularly (2 times per day). Since the frequent off-loading could affect MI/GOCI imaging performance, another suboptimal off-loading time needs to be considered to meet the AOCS design requirements of COMS while having margin enough in the number of thruster actuations. In this paper, preliminary analysis results on the pointing stability and the wheel off-loading time selection with respect to MI/GOCI operations are presented.

• 항공우주산업기술동향
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• 제6권1호
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• pp.74-81
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• 2008

본 논문에서는 최근 발사된 달 탐사 위성의 탑재체 종류와 임무를 분석하고 이를 통해 각국의 달 탐사선의 목적과 탑재체 개발동향을 알아보고자 하였다. 이를 위해, 90년대 이후 발사된 달 탐사 위성들에 실린 탑재체를 임무별로 분류한 후,각 위성 탑재체 별 성능을 분석하여 개발동향을 정리하였다.이러한 분석을 통해, 향후 국내 달 탐사 위성을 위한 임무와 활용 범위를 설정하거나 탑재체 선정 시 기초자료로 활용하고자 한다.

• 한국소음진동공학회:학술대회논문집
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• 한국소음진동공학회 2002년도 추계학술대회논문집
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• pp.853-856
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• 2002

Rocket propulsion systems generate very high-level noise (acoustic loads), which is due to supersonic jet emitted by rocket engine. In practice, the sound power level of rocket propulsion systems is over 180 dB. This high level noise excites rocket structures and payloads, so that it causes the structural failure and electronic malfunction of payloads. Prediction method of acoustic loads of rocket enables us to determine the safety of payloads. A popular prediction method is based on NASA SP-8072. This method was used to predict the acoustic loads of KSR-III rocket. Measurement of acoustic loads by KSR-III propulsion system was performed in the stage qualification test. The predicted results were compared with the measured ones.

• 한국우주과학회:학술대회논문집(한국우주과학회보)
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• 한국우주과학회 2008년도 한국우주과학회보 제17권2호
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• pp.35.1-35.1
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• 2008

The importance on the simulation of earth observation optical payloads has been recently emphasized in order to estimate on-orbit imaging performance of the payloads. The estimation should consider all aspects of payload development; design, manufacture, test, assembly, launch and space environment. Until recently several studies have been focused the evaluation of the individual factors rather than the integrated. This paper presents the development of an integrated payload simulator. The simulator analyzes the payload imaging performance based on MTF(Modulation Transfer Function) calculations of the major factors (Diffraction, Aberration, Detector integration, Image motion and etc.) and the simulator can generate realistic artificial earth images as taken by defined earth observation payloads. The simulator is developed for the use of evaluating pre- and post-launch imaging performance and assisting on-board calibration of COMPSAT-3.

• 대한원격탐사학회:학술대회논문집
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• 대한원격탐사학회 2007년도 Proceedings of ISRS 2007
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• pp.45-48
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• 2007

COMS satellite is a multipurpose satellite in the geostationary orbit, which accommodates multiple payloads of Meteorological Imager, Geostationary Ocean Color Imager and Ka band Satellite Communication Payload in a single spacecraft platform. In this paper, current status of Korea's first geostationary Communication, Ocean and Meteorological Satellte(COMS) program development is introduced. The satellite platform is based on the Astrium EUROSTAR 3000 communication satellite, but creatively combined with MARS Express satellite platform to accommodate three different payloads efficiently for COMS. The system design difficulties are in the different kinds of payload mission requirements of communication and remote sensing purposes and how to combine them into a single satellite to meet the overall satellite requirements. The COMS satellite critical design has been accomplished successfully to meet three different mission payloads. The platform is in Korea, KARI facility for the system integration and test. The expected launch target of COMS satellite is scheduled in June 2009.

• 전자통신동향분석
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• 제37권3호
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• pp.41-51
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• 2022

This article presents an overview of the key technologies in the communications payload of broadband LEO satellite communications systems. In recent years, new developments have been realized for LEO satellite communications. SpaceX's Starlink, a technology leader in this field, offers premium services with satellites carrying in-house developed communications payloads. OneWeb, Amazon, Telesat, and Boeing are also developing LEO satellite communications payloads. The communications payload consists of user link antennas, inter-satellite link communications equipment, feeder link antennas, and a digital processor. Highly sophisticated technologies of compact active phased array antennas for generating multiple hopping beams and light laser communication equipment for ultra-high-speed inter-satellite communication will be applied to next- generation payloads.