• 항공우주기술
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• 제6권2호
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• pp.40-44
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• 2007

대구경 탑재체는 광학설계형태에 따라 설계 및 조립/정렬의 특성이 다르며 각각의 장단점이 구분된다. 광학계 형태에 따른 특성분석을 수행하였고 이 결과를 바탕으로 광학계는 Korsch 타입의 4반 사식 카메라로 선정하였으며 각 미러조립체를 가지고 항우연에서 광구조체 및 광전자부의 조립, 정렬 및 성능시험을 수행하게 된다. 위성카메라의 최종광학성능은 여러 가지 요인에 의해 영향을 받지만 특히 핵심 하드웨어 부분인 광학부 및 광구조체의 광학성능에 크게 좌우된다. 본 논문에서는 광학계 형태에 따른 특성분석을 수행하였고 대구경 Korsch형 탑재체 광학계의 조립 및 정렬 방법에 대한 개념설계를 살펴보고자 한다.

• 대한원격탐사학회:학술대회논문집
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• 대한원격탐사학회 2005년도 Proceedings of ISRS 2005
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• pp.489-492
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• 2005

As a former level of MSC(Multi Spectral Camera) telescope of the KOMPSA T2satellite, the several performance tests of EOS(Electro Optical Subsystem) were performed in the EOS level. By these tests, not only the design requirement of payload can be verified but also the test result can be the important criterion to estimate the performance of payload in the launch and space orbit environment. The EOS Geometric Mapping test is to verify the accuracy of the alignment & assembly on the Subsystem of the MSC by measurement like these; LOS(Line of Sight), LOD(Line of Detector), Band to Band Registration, Optical Distortion and Reference Cube. This paper describes the test results and the analysis for the EOS Geometric Mapping.

• Journal of Astronomy and Space Sciences
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• 제20권3호
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• pp.217-226
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• 2003

MSC (Multi-Spectral Camera) is the payload of KOMPSAT-2, which is being developed for earth imaging in optical and near-infrared region. The design of the MSC is completed and its reliability has been assessed from part level to the MSC system level. The reliability was analyzed in worst case and the analysis results showed that the value complies the required value of 0.9. In this paper, a calculation method of reliability for the MSC system is described, and assessment result is presented and discussed.

• 융합보안논문지
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• 제2권2호
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• pp.1-8
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• 2002

멀티미디어 정보 전송을 위해 RTP(Real-Time Transport Protocol)을 사용하며, 멀티미디어 정보 보안을 위해서는 RPT의 페이로드를 암호화해야 한다. RPT페이로드의 암호화를 위해서 암호화/복호화로 인한 지연이 멀티미디어 정보의 실시간 제약에 미치는 영향을 최소로 하면서 네트워크의 트래픽과 부하에 적응하며 암호화 알고리즘을 변경하기 위한 방법이 필요하다. 또한 멀티미디어 서비스 진행 중 서비스 이용을 중지한 사용자는 RPT 페이로드의 암호화 키를 알고 있기 때문에 페이로드를 보호하기 위해서는 암호화 키를 변경하기 위한 방법이 필요하다. 따라서 본 논문에서는 RPT 페이로드의 암호화를 위해, 암호화 알고리즘과 암호화 키를 변경하기 위한 SCPR(Security Control Protocol for RTP)를 설계하고 구현하였다.

• 제어로봇시스템학회:학술대회논문집
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• 제어로봇시스템학회 2001년도 ICCAS
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• pp.92.6-92
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• 2001

MSC is being developed to be installed on KOMPSAT(Korea Multi-Purpose Satellite-II and to provide high resolution multi-spectral. MSC consists of three main subsystems. One is EOS(Electro-Optics Subsystem), another is PMU(Payload Management Unit) and the other is PDTS(Payload Data Transmission Subsystem). There is an SBC(Single Board Computer) in the PMU to control all MSC subsystems. SBC incorporates Intel 80486 as a main processor and VxWorks as a real-time operating system. SBC software consists of four main tasks and several modules to deal with all control information for imaging and all the state of health telemetrv data, and to perform interface with another MSC units. SBC software also has to handle a lot of commands in order for MSC to perform his mission. One mission command consists of a series of related commands, which are In be executed in the designated sequence, with a specified time ...

• 대한기계학회:학술대회논문집
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• 대한기계학회 2003년도 춘계학술대회
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• pp.462-467
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• 2003

For the Space-borne optical imaging payload system design, light weighting and moderate stiffness of mirror and/or mirror fixation device is very important aspects. The front surface of mirror is regulated by optical performance requirement, but the shape of backplate of mirror is to be optimised while satisfing the required stiffness and weight. According to the results, the best shape of backplate cell is triangular. And also related geometric dimensions and the optimised mounting point of MFD(Mirror Fixation Device) is presented. Finally, natural frequencies and shpaes of mirror structure are analysed.

• Journal of Mechanical Science and Technology
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• 제15권3호
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• pp.339-350
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• 2001

To overcome problems in tracking error related to the unmodeled dynamics in the high speed operation of industrial robots, many researchers have used sliding mode control, which is robust against parameter variations and payload changes. However, these algorithms cannot reduce the inherent chattering which is caused by excessive switching inputs around the sliding surface. This study proposes a fuzzy-sliding mode control algorithm to reduce the chattering of the sliding mode control by fuzzy rules within a pre-determined dead zone. Trajectory tracking simulations and experiments show that chattering can be reduced prominently by the fuzzy-sliding mode control algorithm compared to a sliding mode control with two dead zones, and the proposed control algorithm is robust to changes in payload. The proposed control algorithm is implemented to the SCARA (selected compliance articulated robot assembly) robot using a DSP (digital signal processor) for high speed calculations.

• 한국생산제조학회지
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• 제24권1호
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• pp.87-93
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• 2015

The dynamic responses of a telescope loaded on an STSAT-3 satellite were analyzed, and environmental tests were conducted to verify the reliability of the design. The space use telescope COMIS (compact imaging spectrometer) is a major payload of the STSAT-3 launched on November 21, 2013. Vibration responses such as the acceleration, displacement, and velocity with respect to random vibration and shock impulse inputs were obtained based on theoretical fundamentals in conjunction with finite element analysis. The main focus of this study was on developing technology for accurate and/or favorable modeling and analysis of the structure and fitting the results to that of experiments. Cutting-edge technology for manipulating the vibrations of a space use telescope is suggested.

• Journal of Astronomy and Space Sciences
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• 제17권2호
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• pp.309-316
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• 2000

KOMPSAT-2 will carry MSC(Multi-Spectral Camera) which provides 1m resolution panchromatic and 4m resolution multi-spectral images at the altitude of 685km sun-synchronous mission orbit. The mission operation of KOMSPAT-2 is to provide the earth observation using MSC with nadir pointing. KOMPSAT-2 will also have the capability of roll/pitch tilt maneuver using reaction wheel of satellite as required. In order to protect MSC from thermal distortion as well as direct sunlight, MSC shall be operated within the constraint of sun incidence angle. It is expected that the sunlight will not violate the constraint of sun incidence angle for normal mission operations without roll/pitch maneuver. However, during roll/pitch tilt operations, optical module of MSC may be damaged by the sunlight. This study analyzed sun incidence angle of payload using KOMPSAT-2 AOCS (Attitude and Orbit Control Subsystem) Design and Performance Analysis Soft ware for KOMPSAT-2 normal mission operations.

• 융합보안논문지
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• 제2권1호
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• pp.49-57
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• 2002

멀티미디어 정보 전송을 위해 RTP(Real-Time Transport Protocol)을 사용하며, 멀티미디어 정보 보안을 위해서는 RPT의 페이로드를 암호화해야 한다. RPT 페이로드의 암호화를 위해서 암호화/복호화로 인한 지연이 멀티미디어 정보의 실시간 제약에 미치는 영향을 최소로 하면서 네트워크의 트래픽과 부하에 적응하며 암호화 알고리즘을 변경하기 위한 방법이 필요하다. 또한 멀티미디어 서비스 진행 중 서비스 이용을 중지한 사용자는 RPT 페이로드의 암호화 키를 알고 있기 때문에 페이로드를 보호하기 위해서는 암호화 키를 변경하기 위한 방법이 필요하다. 따라서 본 논문에서는 RPT 페이로드의 암호화를 위해, 암호화 알고리즘과 암호화 키를 변경하기 위한 SCPR(Security Control Protocol for RTP)를 설계하고 구현하였다.