• Title/Summary/Keyword: Parallax correction

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PARALLAX THEORY ADOPTED IN THE JAMAL al-DIN ZIJ AND SHOUSHI-LI - ON THEIR SIMILARITY AND ORIGIN - (자말알딘 지즈와 수시력(授時曆)에 도입된 시차(視差) 이론 - 계산법의 유사성과 그 기원에 관하여 -)

  • EUN HEE LEE
    • Publications of The Korean Astronomical Society
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    • v.39 no.2
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    • pp.53-67
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    • 2024
  • Islamic Jamal al-Din zij and Chinese Shoushi-li(授時曆) are astronomical hand books compiled by Jamal al-Din(札馬魯丁) and Guo Shujing(郭守敬) of the Islamic and Chinese Astronomical Bureau in Yuan(元) China, respectively. Jamal al-Din zij is an Islamic zij based on the Almagest of Ptolemaios, while Shoushii-li is a calendrical treatise by the traditional Chinese calendar system. In case of the parallax correction method, however, both of them have a common origin from Indian astronomy in 6-7 Century. This paper examines and discusses the parallax theory and its origin adopted in Jamal al-Din zij and Shoushi-li as following: 1) Definitions of the parallax theory and parallax correction methods. 2) Similarities and origins of the parallax correction methods adopted in the Jamal al-Din zij and Shoushi-li. 3) Comparison of the parallax correction tables included in the Sanjufini zij of Tibet, the Huihui-lifa(回回曆法) of Ming(明) China and the Chiljeongsan-Oepyeon(七政算外篇) of Joseon(朝鮮) Korea. 4) Routes of the parallax theory transmitted from ancient Greece and India to Joseon via Islam world and China, respectively. 5) Astronomical exchanges and mutual influence between the East and the West.

The Parallax Correction to Improve Cloud Location Error of Geostationary Meteorological Satellite Data (정지궤도 기상위성자료의 구름위치오류 개선을 위한 시차보정)

  • Lee, Won-Seok;Kim, Young-Seup;Kim, Do-Hyeong;Chung, Chu-Yong
    • Korean Journal of Remote Sensing
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    • v.27 no.2
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    • pp.99-105
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    • 2011
  • This research presents the correction method to correct the location error of cloud caused by parallax error, and how the method can reduce the position error. The procedure has two steps: first step is to retrieve the corrected satellite zenith angle from the original satellite zenith angle. Second step is to adjust the location of the cloud with azimuth angle and the corrected satellite zenith angle retrieved from the first step. The position error due to parallax error can be as large as 60km in case of 70 degree of satellite zenith angle and 15 km of cloud height. The validation results by MODIS(Moderate-Resolution Imaging Spectrometer) show that the correction method in this study properly adjusts the original cloud position error and can increase the utilization of geostationary satellite data.

Implementation of Sonar Bearing Accuracy Measurement Equipment with Parallax Error and Time Delay Error Correction (관측위치오차와 시간지연오차를 보정하는 소나방위정확도 측정 장비 구현)

  • Kim, Sung-Duk;Kim, Do-Young;Park, Gyu-Tae;Shin, Kee-Cheol
    • Journal of the Institute of Convergence Signal Processing
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    • v.20 no.4
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    • pp.245-251
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    • 2019
  • Sonar bearing accuracy is the correspondence between the target orientation predicted by sonar and actual target orientation, and is obtained from measurements. However, when measuring sonar bearing accuracy, many errors are included in the results because they are made at sea, where complex and diverse environmental factors are applied. In particular, parallax error caused by the difference between the position of the GPS receiver and the sonar sensor, and the time delay error generated between the speed of underwater sound waves and the speed of electromagnetic waves in the air have a great influence on the accuracy. Correcting these parallax errors and time delay errors without an automated tool is a laborious task. Therefore, in this study, we propose a sonar bearing accuracy measurement equipment with parallax error and time delay error correction. The tests were carried out through simulation data and real data. As a result of the test it was confirmed that the parallax error and time delay error were systematically corrected so that 51.7% for simulation data and more than 18.5% for real data. The proposed method is expected to improve the efficiency and accuracy of sonar system detection performance verification in the future.

Parallax Distortion Detection and Correction Method for Video Stitching by using LDPM Image Assessment (LDPM 영상 평가를 활용한 동영상 스티칭의 시차 왜곡 검출 및 정정 방법)

  • Rhee, Seongbae;Kang, Jeonho;Kim, Kyuheon
    • Journal of Broadcast Engineering
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    • v.25 no.5
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    • pp.685-697
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    • 2020
  • Immersive media videos, such as panorama and 360-degree videos, must provide a sense of realism as if the user visited the space in the video, so they should be able to represent the reality of the real world. However, in panorama and 360-degree videos, objects appear to overlap or disappear due to parallax between cameras, and such parallax distortion may interfere with immersion of the user's content. Accordingly, although many video stitching algorithms have been proposed to overcome parallax distortion, parallax distortion still occurs due to the low performance of the Object detection module and limitations of the Seam generation method. Therefore, this paper analyzes the limitations of the existing video stitching technology and proposes a method for detecting and correcting parallax distortion of video stitching using the LDPM (Local Differential Pixel Mean) image evaluation method that overcomes the limitations of the video stitching technique.

The Suggestion of the Image Registration Using Terrain Relief Correction Based on RFM (유리함수모델 기반 표고시차보상기법을 사용한 Image Registration 방안 제안)

  • Kim, Hyun-Suk;Kim, Moon-Gyu;Seo, Doo-Chun
    • Journal of the Korean Society of Surveying, Geodesy, Photogrammetry and Cartography
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    • v.30 no.1
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    • pp.21-30
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    • 2012
  • When two bands have different look angle in a space-borne camera system, the registration between two bands is required. The registration cannot be modeled with constant parameters because of dynamic of platform and parallax effect. The parallax effect is caused by terrain relief, hence it causes local distortion between two bands. Therefore, the terrain relief correction in order to reduce the parallax effect is required for better registration result, especially for high resolution image data. Such terrain relief correction also can be applied to image data acquired from multiple detectors with different look angle within a band, which is a one of commonly used configuration for a wider swath in space-borne camera system, in order to reduce the distortion between detectors. The RFM is a popular abstract model in remote sensing field, which gives us the relationship between the image plane and geodetic coordinate system. Therefore, we propose a terrain relief correction method based on the RFM. The experiment showed very promising result.

Target Tracking based on Kernelized Correlation Filter Using MWIR and SWIR Sensors (MWIR 및 SWIR 센서를 이용한 커널상관필터기반의 표적추적)

  • Sungu Sun;Yuri Lee;Daekyo Seo
    • Journal of the Korea Institute of Military Science and Technology
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    • v.26 no.1
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    • pp.22-30
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    • 2023
  • When tracking small UAVs and drone targets in cloud clutter environments, MWIR sensors are often unable to track targets continuously. To overcome this problem, the SWIR sensor is mounted on the same gimbal. Target tracking uses sensor information fusion or selectively applies information from each sensor. In this case, parallax correction using the target distance is often used. However, it is difficult to apply the existing method to small UAVs and drone targets because the laser rangefinder's beam divergence angle is small, making it difficult to measure the distance. We propose a tracking method which needs not parallax correction of sensors. In the method, images from MWIR and SWIR sensors are captured simultaneously and a tracking error for gimbal driving is chosen by effectiveness measure. In order to prove the method, tracking performance was demonstrated for UAVs and drone targets in the real sky background using MWIR and SWIR image sensors.

A Survey on Moving Target Indication Techniques for Small UAVs : Parametric Approach (소형 무인항공기용 이동표적 표시기법에 대한기술 동향 분석 : 매개변수방식)

  • Yun, Seung Gyu;Kang, Seung Eun;Ko, Sang Ho
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.42 no.7
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    • pp.576-585
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    • 2014
  • In this paper, we survey the Moving Target Indication(MTI) techniques for small UAVs. MTI consists of image alignment phase and frame differencing correction phase, and image alignment has two ways of parametric approach which is mainly focused in this paper and non-parametric approach. Since small UAVs are operated in the low altitude, the parallax is considerable and the epipolar geometry is applied to compensate the parallax. The related works and future works are presented.

Simulation of Distortion in Image Space due to Observer's Rotation Movement in Stereoscopic Display, and Its Correction (스테레오스코픽 디스플레이에서 관찰자의 회전이동에 따른 영상공간의 왜곡과 왜곡 보정에 대한 전산모사)

  • Kim, Dong-Wook;Lee, Kwang-Hoon;Kim, Sung-Kyu;Chang, Eun-Young
    • Korean Journal of Optics and Photonics
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    • v.20 no.2
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    • pp.87-93
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    • 2009
  • Variation of the observer's viewing position is one of the major causes of image space distortion in the stereoscopic display. Especially, a large image distortion, which is caused by different depth direction positions of the observer's two eyes, is made by the observer's rotation movement in relation to the center of the screen. This is different from distortion of horizontal and depth directional movement of the observer. In this paper, we analyzed distortion of the image space due to the observer's rotation movement and showed the corrected result of distortion through simulation in the stereoscopic display. Finally, we showed that the distortion shape of the observer's rotation movement is different from horizontal and depth directional movement of the observer.

Development of Optical Sighting System for Moving Target Tracking

  • Jeung, Bo-Sun;Lim, Sung-Soo;Lee, Dong-Hee
    • Current Optics and Photonics
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    • v.3 no.2
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    • pp.154-163
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    • 2019
  • In this study, we developed an optical sighting system capable of shooting at a long-distance target by operating a digital gyro mirror composed of a gyro sensor and an FSM. The optical sighting system consists of a reticle part, a digital gyro mirror (FSM), a parallax correction lens, a reticle-ray reflection mirror, and a partial reflection window. In order to obtain the optimal volume and to calculate the leading angle range according to the driving angle of the FSM, a calculation program using Euler rotation angles and a three-dimensional reflection matrix was developed. With this program we have confirmed that the horizontal leading angle of the developed optical sighting system can be implemented under about ${\pm}8^{\circ}$ for the maximum horizontal driving angle (${\beta}={\pm}12.5^{\circ}$) of the current FSM. Also, if the ${\beta}$ horizontal driving angle of the FSM is under about ${\pm}15.5^{\circ}$, it can be confirmed that the horizontal direction leading angle can be under ${\pm}10.0^{\circ}$. If diagonal leading angles are allowed, we confirmed that we can achieve a diagonal leading angle of ${\pm}10.0^{\circ}$ with a vertical driving angle ${\alpha}$ of ${\pm}7.1^{\circ}$ and horizontal driving angle ${\beta}$ of ${\pm}12.5^{\circ}$.