• 제어로봇시스템학회:학술대회논문집
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• 제어로봇시스템학회 1993년도 한국자동제어학술회의논문집(국내학술편); Seoul National University, Seoul; 20-22 Oct. 1993
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• pp.799-804
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• 1993

In this paper, the scheme of combining the orbit correction and attitude control of a 3-axis stabilized satellite is suggested. Being coupled and complimentary, it is preferable to achieve the required orbit correction and the desired attitude control simultaneously. A solution of the probes simultaneous control of orbit correction and attitude of a satellite, is obtained by solving the two point boundary value problem numerically. The first-order gradient algorithm is used to solve the numerical problem. The simulation results show that the East-West station keeping process with the combined system of an orbit correction and an attitude control is satisfactory.

• 한국군사과학기술학회지
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• 제10권2호
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• pp.160-169
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• 2007

In this paper, we have described and simulated the effect analysis and correction of phase errors in the SAR rawdata induced by satellite attitude errors such as drift, jitter. This simulation is based on the FSA(Frequency Scaling Algorithm) for high resolution image formation of the Spotlight SAR. Phase errors produce the degradation of SAR image quality such as loss of resolution, geometric distortion, loss of contrast, spurious targets, and decrease in SNR. To resolve this problem, this paper presents method for correction of phase errors using the PGA(Phase Gradient Algorithm) in connection with the FSA. Several results of the phase errors correction are presented for Spotlight SAR rawdata.

• 대한원격탐사학회:학술대회논문집
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• 대한원격탐사학회 2002년도 Proceedings of International Symposium on Remote Sensing
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• pp.543-547
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• 2002

In this paper, we introduce a more improved camera modeling method for linear pushbroom images than the method proposed by Orun and Natarajan(ON). ON model shows an accuracy of within 1 pixel if more than 10 ground control points(GCPs) are provided. In general, there is high correlation between platform position and attitude parameters but ON model ignores attitude variation in order to overcome such correlation. We propose a new method that obtains an optimal solution set of parameters without ignoring the attitude variation. We first assume that attitude parameters are constant and estimate platform position's. Then we estimate platform attitude parameters using the values of estimated position parameters. As a result, we can set up an accurate camera model for a linear pushbroom satellite scene. In particular, we can apply the camera model to its surrounding scenes because our model provide sufficient information on satellite's position and attitude not only for a single scene but also for a whole imaging segment. We tested on two images: one with a pixel size 6.6m$\times$6.6m acquired from EOC(Electro Optical Camera), and the other with a pixel size 10m$\times$l0m acquired from SPOT. Our camera model procedures were applied to the images and gave satisfying results. We had obtained the root mean square errors of 0.5 pixel and 0.3 pixel with 25 GCPs and 23 GCPs, respectively.

• 한국정밀공학회:학술대회논문집
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• 한국정밀공학회 2006년도 추계학술대회 논문집
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• pp.85-86
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• 2006

• 문화기술의 융합
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• 제9권4호
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• pp.211-221
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• 2023

이 연구는 강의평가의 대상에 학업성취도를 추가하여 평가의 타당성을 높이고, 수업태도에 대한 통제정당성을 검증하고 수업태도 보정지수를 개발하여 평가의 신뢰성을 높이기 위한 목적으로 실시하였다. 연구의 결과는 다음과 같다. 첫째, 학생의 수업태도는 강의만족도에 유의미한 영향을 미치는 것으로 확인되었다. 수업태도가 긍정적일수록 강의만족도가 높아지고, 수업태도가 부정적일수록 강의만족도가 낮아지는 것으로 나타났다. 둘째, 학생의 수업태도는 학업성취도에 유의미한 영향을 미치는 것으로 확인되었다. 수업태도가 긍정적일수록 학업성취도가 높으며, 수업태도가 부정적일수록 학업성취도가 낮은 것으로 나타났다. 셋째, 강의만족도는 학업성취도에 유의미한 영향을 미치지 못하는 것으로 확인되었다. 강의만족도가 높다고 해서 강의품질이 높다고 할 수 없으며, 강의만족도가 낮다고 해서 강의품질이 낮다고 할 수 없다는 의미이다. 넷째, 수업태도로 인해 왜곡될 수 있는 강의만족도 결과를 보정하기 위한 강의만족도 보정지수를 개발하였다. 결론적으로 강의만족도외에 학업성취도를 평가대상으로 추가하여 강의평가의 타당성을 제고하고, 강의만족도 보정지수를 적용하여 강의평가의 신뢰성을 제고해야 한다.

• Journal of Astronomy and Space Sciences
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• 제21권4호
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• pp.399-416
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• 2004

국내 최초의 과학위성인 과학기술위성 1호(STSAT-1)의 주 탑재체 원자외선분광기(FIMS; Far-utraviolet IMaging Spectrograph)는 2003년 9월 발사된 이후로, 다양한 관측을 수행하고 있으나 위성체에서 제공하는 자세정보의 시각오차의 문제점이 발견되어 시각오차를 보정하기 위한 연구가 수행되었다. 시각오차의 보정 후에 잘 알려진 천체의 관측결과를 이용하여 FIMS와 위성체 좌표계 사이의 기계적인 정렬오차에 의해 발행하는 FIMS의 시선방향과 위성체에서 제공하는 자세의 차이를 단파장대와 장파장대에 대하여 각각 계산하였다. 또한, 자세정보의 월별 상태 및 정밀도를 조사하였다. FIMS의 관측방법의 특성상 FIMS로부터 얻어진 영상은 위치별로 서로 다른 노출시간을 갖는다. 이러한 노출시간을 보정하는 방법을 기술하였다. 이 연구의 결과는 FIMS 자료분석을 위해 반드시 필요한 내용이며 추후 좀 더 정밀한 자세정보 보정을 위한 참고 자료로 활용될 것이다.

• 천문학논총
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• 제20권1호
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• pp.135-141
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• 2005

The FIMS(Far-ultraviolet IMaging Spectrograph), the main payload onboard the first Korean Science Technology SATellite, STSAT-1, has performed various astronomical observations, including the Cygnus Loop, Vela supernova remnants, LMC(Large Magellanic Cloud), since its launch on September 2003. It has been found that the attitude information provided by spacecraft bus system has the errors of more than about 10-15 arcmins due to the time offset problem and errors in attitude knowledge. We develop an algorithm for correction of position errors in FIMS data. The aspect for the FIMS data is determined by comparing the positions of observed bright stars with the Tycho-II and TD-1 catalogs. The position errors of the bright stars along the scanning (${\gamma}$) and spatial (${\delta}$) directions were considered as functions of ${\delta}$, ignoring errors in position angle. The corrected positions of the bright stars coincided very well to their Tycho-II and TD-I positions. The correction algorithm is essential for the FIMS data analysis, and is being used for the FIMS data analysis.

• 대한공간정보학회지
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• 제10권5호
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• pp.67-74
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• 2002

The geometriccorrection of a satellite imagery is performed by making a systematic correction with satellite ephemerides and attitude angles followed by employing the Ground Control Points (GCSs) or Digital Elevation Models (DEMs). In a remote area or an inaccessible area, however, GCPs are unavailable to be surveyed and thus they can be obtained only by reading maps, which are not accurate in reality. In this study, we performed the systematic correction process to the inaccessible area and the precise geometric correction process to the adjacent accessible area by using GCPs. Then we analyzed the correlation between the two geo-referenced Korea Multiurpose Satellite (KOMPSAT-1 EOC) images. A new geometrical correction for the inaccessible area imagery is achieved by applying the correlation to the inaccessibleimagery. By employing this new method, the accuracy of the inaccessible area imagery is significantly improved absolutely and relatively.

• 대한원격탐사학회:학술대회논문집
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• 대한원격탐사학회 1998년도 Proceedings of International Symposium on Remote Sensing
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• pp.252-256
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• 1998

Accurate mapping of satellite images is one of the most important Parts in many remote sensing applications. Since the position and the attitude of a satellite during image acquisition cannot be determined accurately enough, it is normal to have several hundred meters' ground-mapping errors in the systematically corrected images. The users which require a pixel-level or a sub-pixel level mapping accuracy for high-resolution satellite images must use a number of Ground Control Points (GCPs). In this paper, the performance of two geometric correction algorithms is tested and compared. One is the polynomial warping algorithm which is simple and popular enough to be implemented in most of the commercial satellite image processing software. The other is full camera modelling algorithm using Physical orbit-sensor-Earth geometry which is used in satellite image data receiving, pre-processing and distribution stations. Several criteria were considered for the performance analysis : ultimate correction accuracy, GCP representatibility, number of GCPs required, convergence speed, sensitiveness to inaccurate GCPs, usefulness of the correction results. This paper focuses on the usefulness of the precision correction algorithm for regular image pre-processing operations. This means that not only final correction accuracy but also the number of GCPs and their spatial distribution required for an image correction are important factors. Both correction algorithms were implemented and will be used for the precision correction of KITSAT-3 images.

• 지질공학
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• 제24권2호
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• pp.171-178
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• 2014

In seismic reflection data processing, the crossdip correction effectively focuses the stacking energy near the sharp bends of a crooked survey line. Additionally, approximate 3-D information on the reflector (e.g., true crossdip angle and lateral continuity) are locally investigated as a by-product of the crossdip correction procedure. Improvement of the signal-to-noise ratio and estimation of reflector crossdip attitude are tested, in terms of both common midpoint bin direction and processing-line type, using synthetic seismic reflection data. To effectively image the reflection energy near bends in seismic survey lines, straight-line binning is preferred to slalom-line binning.