• 한국지리정보학회지
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• 제7권4호
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• pp.143-154
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• 2004

원격탐사는 각종 상업용 위성과 항공사진을 바탕으로 이루어진다. 그러나 이러한 자료는 연구자들이 원하는 시기와 장소에 따라 촬영되는데 자료 획득시, 기상조건 및 경제적 이유로 많은 어려움을 겪고 있다. 이러한 문제점을 해결하고자 본 연구에서는 소형비행기 및 초경량 비행기에 탈부착이 가능한 소형 다중분광 자동 항공촬영시스템(PKNU2)을 개발하였다. PKNU2호는 연구실 자체 보유한 고해상도 가시대역, 적외선대역 카메라를 이용하여 칼라영상 및 적외 영상을 획득하였다. 환경감시 등의 목적으로 칼라 적외 합성영상을 생성, 분석하였으나 그리 만족스러운 결과를 획득하지 못하였다. 또한 PKNU2호가 대용량 촬영은 가능하였지만 데이터 저장시간이 12초로 횡중복률 60%를 만족시키지 못하였다. 현재 우리는 PKNU2호의 단점을 극복하고자 가시대역과 적외선 대역의 자료를 한번에 획득할 수 있 칼라 적외선 분광카메라, 열적외 카메라, 그리고 영상의 실시간 저장이 가능한 MPEG board를 도입하여 헬리콥터에 탈부착이 가능한 소형 다중분광 자동 항공촬영시스템(PKNU3)을 개발하고 있다. 본 연구에서는 본격적인 촬영에 앞서 가치 있는 영상 획득을 위해 센서의 특성 평가를 실시, 센서의 분광 특성 보정 및 렌즈의 기하학적 왜곡 보정을 작업을 실시하였다.

• 한국멀티미디어학회논문지
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• 제4권1호
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• pp.37-45
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• 2001

다대역(multi-band) 카메라 시스템으로 물체의 분광 반사율을 추정하여 피사체의 고유한 색자극을 기록하기 위한 연구가 활발하다. 그러나 다대역 카메라 시스템은 대역 수에 따라 추가적인 색필터가 필요하며 중복촬영으로 인하여 시스템의 복잡성이 증가하는 단점이 있다. 따라서 본 논문에서는 기존의 3대역 RGB 카메라를 이용하여 분광 반사율의 추정 오차를 개선하는 방법을 제안한다. 제안된 방법에서는 화소 단위로 반사광의 모집단을 갱신하여 각 입력색에 대해 적응적인 주성분 벡터를 구하였으며 이를 이용하여 해당 화소의 분광반사율 추정시 오차를 줄였다. 제안된 반사율 추정 방법의 유용성을 평가하기 위하여 제안된 방법과 3대역 주성분 분석(principal component analysis) 방법 및 5대역 위너 추정(Wiener estimation) 방법에 대하여 각각 Macbeth ColorChecker에 대한 분광 반사율 추정 실험을 하였다. 결과, 제안한 방법은 색차 및 분광 반사율 평균자승오차가 기존의 3대역 주성분 분석 방법보다 적었으며 5대역 카메라를 이용한 분광 반사율 추정 방법과 근사하건, 개선되었음을 확인하였다.

• 대한원격탐사학회:학술대회논문집
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• 대한원격탐사학회 2003년도 Proceedings of ACRS 2003 ISRS
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• pp.642-644
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• 2003

SAC is a compact electro-optical camera for imaging in visible-NIR spectral ranges. SAC provides highresolution images over the wide geometric and spectral ranges: 10 m ground sample distance (GSD) and 50 km swath width in the spectral ranges of 520 ${\sim}$ 890 nm. SAC is designed to produce high quality images: modulation transfer function (MTF) of more than 15 %; signal-to-noise ratio (SNR) of more than 100. The missions of SAC incorporate various imaging operations: multi-spectral imaging; super swath-width imaging with cameras in parallel; along-track stereo imaging with slanted 2 cameras.

• 대한원격탐사학회:학술대회논문집
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• 대한원격탐사학회 2004년도 Proceedings of ISRS 2004
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• pp.601-603
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• 2004

Multi-Spectral Camera(MSC) is a payload on the KOMPSAT -2 satellite to perform the earth remote sensing. The instrument images the earth using a push-broom motion with a swath width of 15 km and a ground sample distance (GSD) of 1 m over the entire field of view (FOV) at altitude 685 Km. The instrument is designed to have an on-orbit operation duty cycle of $20\%$ over the mission lifetime of 3 years with the functions of programmable gain! offset and onboard image data compression/storage. MSC instrument has one(1) channel for panchromatic Imaging and four(4) channel for multi-spectral Imaging covering the spectral range from 450nm to 900nm using TDI CCD Focal Plane Array (FPA). In this paper, the configuration, the interface of MSC hardware and the MSC operation concept are described. And the method of the MSC calibration are described and the design of MSC calibration operation to measure the change of MSC after Launch & Early Operation(LEOP) and normal mission operations are discussed and analyzed.

• 대한원격탐사학회:학술대회논문집
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• 대한원격탐사학회 2003년도 Proceedings of ACRS 2003 ISRS
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• pp.825-827
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• 2003

Multi-Spectral Camera(MSC) is a payload on the KOMPSAT-2 satellite to perform the earth remote sensing. The instrument images the earth using a push-broom motion with a swath width of 15 km and a ground sample distance (GSD) of 1 m over the entire field of view (FOV) at altitude 685 Km. The instrument is designed to have an on-orbit operation duty cycle of 20% over the mission lifetime of 3 years with the functions of programmable gain/ offset and on-board image data compression/storage. The MSC instrument has one(1) channel for panchromatic imaging and four(4) channel for multi-spectral imaging covering the spectral range from 450nm to 900nm using TDI CCD Focal Plane Array (FPA). In this paper, the architecture and function of MSC hardware including electrical interface and the operation concept which have been established based on the mission requirements are described. And the design and the preparation of MSC system operation are analyzed and discussed.

• 제어로봇시스템학회논문지
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• 제19권12호
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• pp.1061-1066
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• 2013

In the steel industry, the detection of tiny defects including its 3D characteristics on steel surfaces is very important from the point of view of quality control. A multi-spectral photometric stereo method is an attractive scheme because the shape of the defect can be obtained based on the images which are acquired at the same time by using a multi-channel camera. Moreover, the calculation time required for this scheme can be greatly reduced for real-time application with the aid of a GPU (Graphic Processing Unit). Although a more reliable shape reconstruction of defects can be possible when the numbers of available images are increased, it is not an easy task to construct a camera system which has more than 3 channels in the visible light range. In this paper, a new 6-channel camera system, which can distinguish the vertical/horizontal linearly polarized lights of RGB light sources, was developed by adopting two 3-CCD cameras and two polarized lenses based on the fact that the polarized light is preserved on the steel surface. The photometric stereo scheme with 6 images was accelerated by using a GPU, and the performance of the proposed system was validated through experiments.

• 한국측량학회:학술대회논문집
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• 한국측량학회 2007년도 춘계학술발표회 논문집
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• pp.145-148
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• 2007

The Korea Multi-Purpose Satellite-2 (KOMPSAT-2) was launched in July 2006 and The main mission of the KOMPSAT-2 is a high resolution imaging for the cartography of Korea peninsula by utilizing Multi Spectral Camera (MSC) images. The camera resolutions are 1 m in panchromatic scene and 4 m in multi-spectral imaging. KOMPSAT-2 measure the position, velocity and attitude data of satellite using by star sensor, gyro sensor, and GPS sensor. This paper provides an initial geometric accuracy assessment of the KOMPSAT-2 high resolution image, both geometric Cal/Val overview.

• 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.

• 대한원격탐사학회:학술대회논문집
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• 대한원격탐사학회 2006년도 Proceedings of ISRS 2006 PORSEC Volume II
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• pp.780-783
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• 2006

The KOrea Multi-Purpose Satellite-2 (KOMPSAT-2) was launched in July 2006 and the main mission of the KOMPSAT-2 is a high resolution imaging for the cartography of Korea peninsula by utilizing Multi Spectral Camera (MSC) images. The camera resolutions are 1 m in panchromatic scene and 4 m in multi-spectral imaging. This paper provides an initial geometric accuracy assessment of the KOMPSAT-2 high resolution image without ground control points and briefly introduces the sensor model of KOMPSAT-2. Also investigated and evaluated the obtained 3-dimensional terrain information using the MSC pass image and scene images acquired from the KOMPSAT-2 satellite.

• 대한원격탐사학회:학술대회논문집
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• 대한원격탐사학회 2005년도 Proceedings of ISRS 2005
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• pp.478-481
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• 2005

The PMU (Payload Management Unit) is the main subsystem for the management, control and power supply of the MSC (Multi-Spectral Camera) Payload operation. It is the most important function for the electro-optical camera system that performs the Non-Uniformity Correction (NUC) function of the raw imagery data, rearranges the data from the CCD (Charge Coupled Device) detector and output it to the Data Compression and Storage Unit (DCSU). The NUC board in PMU performs it. In this paper, the NUC board system is described in terms of the configuration and the function, the efficiency for non-uniformity correction, and the influence of the data compression upon the peculiar feature of the CCD pixel. The NUC board is an image-processing unit within the PMU that receives video data from the CEV (Camera Electronic Unit) boards via a hotlinkand performs non-uniformity corrections upon the pixels according to commands received from the SBC (Single Board Computer) in the PMU. The lossy compression in DCSU needs the NUC in on-orbit condition.