• 한국측량학회지
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• 제25권6_2호
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• pp.635-643
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• 2007

국내에 고해상도 지도제작용 항공디지털카메라 영상의 도입 및 공급이 현실화됨에 따라 항공디지털카메라 영상을 이용한 수치지도의 제작 및 갱신에 많은 관심이 모아지고 있다. 본 연구는 푸쉬부룸 항공디지털카메라 영상을 이용하여 기존의 1/1,000 수치지도의 갱신방법을 제시하고자 하였다. GPS측량성과를 이용하여 기하보정을 수행하고, 수치도화를 위해 수치사진측량시스템을 이용하였다. 수치도화는 건물 및 도로를 묘사하였고, GPS측량성과를 이용하여 절대위치정확도 평가와 해석도화에 의해 제작된 수치지도를 이용하여 상대위치정확도 평가를 수행하였다. 절대위치정확도 평가결과, RMSE가 X, Y축으로 각각 ${\pm}0.172m,\;{\pm}0.127m$, 평균거리오차는 0.208m, 상대위치정확도 평가결과, RMSE가 X, Y축으로 각각 ${\pm}0.238m,\;{\pm}0.281m$, 평균거리오차는 0.337m로 나타났다. 따라서, 본 연구에서 제시한 항공디지털카메라 영상을 이용한 수치지도 갱신방법은 국토지리정보원 규정의 허용오차 이내였으므로, 향후 국가기본도 제작은 물론 지자체의 GIS사업 및 다양한 분야에 활용할 수 있다.

• 한국측량학회지
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• 제28권4호
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• pp.449-454
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• 2010

최근 항공측량분야에서 항공디지털카메라 및 항공레이저측량시스템은 수치정사영상지도 및 수치표고모델제작 등의 지리정보 구축에 활용되고 있다. 본 연구에서는 항공레이저측량시스템인 ALS50-II에 구성된 중형CCD카메라 RCD105의 3차원 위치정확도를 디지털항공사진카메라인 DMC와 비교하였다. 이를 위해 연구지역을 선정하고 항공사진촬영을 실시하였으며, 축적 1:1,000 수치지형도에서 항공삼각측량에 사용할 지상기준점과 수치도화기를 이용해 평면 및 수준정확도 검증에 사용할 검사점을 선점하였다. RCD105와 DMC의 정확도는 항공삼각측량의 결과와 수치도화기를 이용해 검사점과 동일한 지점을 관측한 결과로 평가하였다. 항공삼각측량 결과 RCD105의 X, Y, Z RMSE (Root Mean Square Error)가 DMC보다 각각 2.1배, 2.2배, 1.3배 크게 나타났다. 또한 수치도화기를 이용해 검사점을 관측한 결과 RCD105의 평면 및 수직방향 RMSE가 DMC보다 각각 2.5배, 4.3배 크게 나타났다. RCD105의 정확도가 DMC보다는 떨어지지만, RCD105도 수치지형도 및 정사사진 제작에 활용이 가능할 것으로 사료된다.

• 한국지형공간정보학회:학술대회논문집
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• 한국지형공간정보학회 2004년도 추계학술발표대회 논문집
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• pp.123-128
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• 2004

최근 디지털 카메라(Digital camera), 다중/고분광 영상(Mumltispectral/Hyperspectral image), LiDAR(Light Detection and Ranging), InSAR(Interferometric SAR)와 같이 지상을 보다 상세하고 높은 정확도로 지상을 매핑할 수 있는 센서들이 출현하고 있다. 이러한 다양한 정보 취득 자료를 충분히 활용하여 통합하기 위해서는 영상에 대하여 정확한 기하보정 또는 정사영상의 제작과 LiDAR 자료와 같은 경우 평면위치의 오차를 조정하여 다중자료들 간의 정확한 지형보정(Coregistration)이 필요하다. 본 연구에서는 AIR-MS 자료를 이용하여 즉, 항공기로부터 취득한 LiDAR(Height와 강도(Intensity) 자료), digital camera을 통합하고, 기존의 컬러항공사진 및 1:1000 수치지도를 이용하여 3D GIS 자료의 생성을 시도하였다.

• Journal of the Optical Society of Korea
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• 제16권1호
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• pp.63-69
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• 2012

This paper presents a method to derive the theoretical requirements for the development of a 400 mm optical window that transmits dual-band wavelengths and had a stable structure. We also present design and fabrication results. Among the required specifications, the surface figure error was defined by the transmitted wavefront deformation (TWD), ${\lambda}$/15 rms at 632.8 nm. This value was derived by estimating the predicted performances with respect to five independent items that could cause system performance degradation and then calculating the required wavefront error (WFE) to satisfy the performance goals. We measured the image resolution at each performance level to trace and verify the requirements. The article also describes a design optimization process that could minimize the weight and volume of the optical window attached to the payload securing the FOV of the camera. In addition, we accurately measured the deformation that occurred in the series of fabrication steps including processing, coating, assembly, bonding and bolting, and investigated the effects by comparing them to the results of a simulation performed in advance to derive the predicted performance.

• Korean Journal of Geomatics
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• 제3권1호
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• pp.23-32
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• 2003

Rigorous sensor and dynamic modeling techniques are required if spatial information is to be accurately extracted from video imagery. First, a mathematical model for an uncalibrated video camera and a description of a bundle adjustment with added parameters, for purposes of general block triangulation, is presented. This is followed by the application of invariance-based techniques, with constraints, to derive initial approximations for the camera parameters. Finally, dynamic modeling using the Kalman Filter is discussed. The results of various experiments with real video imagery, which apply the developed techniques, are given.

• Journal of the Optical Society of Korea
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• 제15권2호
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• pp.174-181
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• 2011

An airborne sensor is developed for remote sensing on an aerial vehicle (UV). The sensor is an optical payload for an eletro-optical/infrared (EO/IR) dual band camera that combines visible and IR imaging capabilities in a compact and lightweight package. It adopts a Ritchey-Chr$\'{e}$tien telescope for the common front end optics with several relay optics that divide and deliver EO and IR bands to a charge-coupled-device (CCD) and an IR detector, respectively. The EO/IR camera for dual bands is mounted on a two-axis gimbal that provides stabilized imaging and precision pointing in both the along and cross-track directions. We first investigate the mechanical deformations, displacements and stress of the EO/IR camera through finite element analysis (FEA) for five cases: three gravitational effects and two thermal conditions. For investigating gravitational effects, one gravitational acceleration (1 g) is given along each of the +x, +y and +z directions. The two thermal conditions are the overall temperature change to $30^{\circ}C$ from $20^{\circ}C$ and the temperature gradient across the primary mirror pupil from $-5^{\circ}C$ to $+5^{\circ}C$. Optical performance, represented by the modulation transfer function (MTF), is then predicted by integrating the FEA results into optics design/analysis software. This analysis shows the IR channel can sustain imaging performance as good as designed, i.e., MTF 38% at 13 line-pairs-per-mm (lpm), with refocus capability. Similarly, the EO channel can keep the designed performance (MTF 73% at 27.3 lpm) except in the case of the overall temperature change, in which the EO channel experiences slight performance degradation (MTF 16% drop) for $20^{\circ}C$ overall temperate change.

• 대한원격탐사학회:학술대회논문집
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• 대한원격탐사학회 2008년도 International Symposium on Remote Sensing
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• pp.243-246
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• 2008

The Compact Airborne Imaging Spectrometer System (CAISS) was jointly designed and developed as the hyperspectral imaging system by Korea Aerospace Research Institute (KARI) and ELOP inc., Israel. The primary mission of the CAISS is to acquire and provide full contiguous spectral information with high quality spectral and high spatial resolution for advanced applications in the field of remote sensing. The CAISS consists of six physical units; the camera system, the gyro-stabilized mount, the jig, the GPS/INS, the power inverter and distributor, and the operating system. These subsystems shall be tested and verified in the laboratory before the flight. Especially the camera system of the CAISS shall be calibrated and validated with the calibration equipments such as the integrated sphere and spectral lamps. To improve data quality and availability, it is the most important to understand the mechanism of hyperspectral imaging system and the radiometric and spectral characteristics. This paper presents the major characteristics of camera system on the CAISS and summarizes the results of radiometric and spectral experiment during preliminary system verification.

• 환경영향평가
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• 제20권3호
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• pp.349-356
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• 2011

This research is aim to analyze of changing landscape and according to phenological cycle from image information of coastal environment obtained by multi-media were analyzed by camera and satellite image. The digital camera and satellite image were used for tidal flat vegetation monitoring during the construction of Sihwa lake. The vegetation type and phenological cycle of Sihwa tidal flat have been changed with the Sihwa lake ecosystem. The environment changes of Sihwa tidal flat area and ecological change were analyzed by field work digital camera images and satellite images. The airborne, UAV and satellite images were classified with the changed elements of coastal ecological environment and tidal flat vegetation monitoring carried out the changed area and shape of vegetation distribution with time series images.

• Current Optics and Photonics
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• 제7권4호
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• pp.354-361
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• 2023

We present the optical design and experimental verification of resolving performance of a 3× long wavelength infrared (LWIR) zoom camera for drones. The effective focal length of the system varies from 24.5 mm at the wide angle position to 75.1 mm at the telephoto position. The design specifications of the system were derived from ground resolved distance (GRD) to recognize 3 m × 6 m target at a distance of 1 km, at the telephoto position. To satisfy the system requirement, the aperture (f-number) of the system is taken as F/1.6 and the final modulation transfer function (MTF) should be higher than 0.1 (10%). The measured MTF in the laboratory was 0.127 (12.7%), exceeds the system requirement. Outdoor targets were used to verify the comprehensive performance of the system. The system resolved 4-bar targets corresponding to the spatial resolution at the distance of 1 km, 1.4 km and 2 km.

• 대한원격탐사학회:학술대회논문집
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• 대한원격탐사학회 2005년도 Proceedings of ISRS 2005
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• pp.201-204
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• 2005

Recently, the generation of panoramic images and high quality mosaic images from video sequences has been attempted by a variety of investigations. Among a matter of investigation, in this paper, left and right stereo mosaic image generation utilizing airborne-video sequence images is focused upon. The stereo mosaic image is generated by creating left and right mosaic image which is generated by front and rear slit having different viewing angle in consecutive video frame images. The generation of stereo mosaic image proposed in this paper consists of several processes: camera parameter estimation for each video frame image, rectification, slicing, motion parallax elimination and image mosaicking. However it is necessary to check the feasibility on generating stereo mosaic image as explained processes. Therefore, in this paper, we performed the feasibility test on generating stereo mosaic image using video frame images. In doing so, anaglyphic image for stereo mosaic images is generated and tested for feasibility check.