• 제목/요약/키워드: correct orbit

검색결과 35건 처리시간 0.03초

위성 탑재용 궤도전파기의 자동 갱신에 관한 연구 (A Study on Autonomous Update of Onboard Orbit Propagator)

  • 정옥철;노태수;이상률
    • 한국항공우주학회지
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    • 제31권10호
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    • pp.51-59
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    • 2003
  • 본 논문에서는 위성 탑재용 궤도전파기의 자동 갱신 방안에 대하여 제안하였다. 위성 탑재용 궤도전파기는 비상시 위성 항법 장치의 대체 수단으로써 여러 이유로 지상국에 의한 갱신이 불가능할 경우에 대비하여 위성체 스스로 가장 최신의 탑재 궤도전파기 모델을 유지해야 한다. 이를 위해 GPS 수신기의 고장 시점까지 가용한 GPS 항행해나 탑재 궤도 결정 시스템으로부터의 자료를 이용하여 최소자승회귀법(Least Square Curve Fit)이나 칼만 필터를 통해 위성에 탑재된 궤도전파기를 위한 기준궤도 또는 잔차 재생함수의 계수를 반복적으로 갱신한다. 탑재 궤도전파기 갱신을 통해 만약 있을 수도 있는 지상국에서의 계산 오류를 스스로 보정할 수 있고, GPS와 탑재 궤도결정 시스템의 작동 불능 시점 직전까지의 자료에 근거하여 궤도를 예측하기 때문에 항상 최신의 궤도전파기 모델을 유지할 수 있다. 또한 아리랑 1호의 궤도 예측 자료를 이용하여 실제 운용시 최적화된 알고리즘을 통해 실시간 갱신을 이용한 궤도 전파 성능에 대하여 살펴보았다.

Relativistic Effects on Orbital Energies in AgH and AuH ; A Clue to the Origin of Relativistic Correlation Effects

  • Lee, Yoon-Sup;McLean, A. D.
    • Bulletin of the Korean Chemical Society
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    • 제8권2호
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    • pp.122-126
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    • 1987
  • Oribtal energies for AuH and AgH are calculated by an all-electron relativistic self-consistent-field method using Slater type basis functions. Major relativistic effects for AgH are spin-orbit splittings and those for AuH are large shifts in orbital energies in addition to spin-orbit splittings. Relativistic effects on orbital energies in AgH and AuH imply that changes in correlation energies for relativistic calculations of AuH will be significantly larger than those of AgH, providing partial explanation for the large discrepencies in equilibrium bond length and the dissociation energy between experiments and theoretical estimates for AuH. Large relativistic effects on orbital energies indicate that relativistic contributions should be included for the correct interpretation of ionization potentials for these molecules. Relativistic effects are also evident in dipole moments for these molecules.

The Operational Procedure on Estimating Typhoon Center Intensity using Meteorological Satellite Images in KMA

  • Park, Jeong-Hyun;Park, Jong-Seo;Kim, Baek-Min;Suh, Ae-Sook
    • 대한원격탐사학회:학술대회논문집
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    • 대한원격탐사학회 2006년도 Proceedings of ISRS 2006 PORSEC Volume I
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    • pp.278-281
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    • 2006
  • Korea Meteorological Administration(KMA) has issued the tropical storm(typhoon) warning or advisories when it was developed to tropical storm from tropical depression and a typhoon is expected to influence the Korean peninsula and adjacent seas. Typhoon information includes current typhoon position and intensity. KMA has used the Dvorak Technique to analyze the center of typhoon and it's intensity by using available geostationary satellites' images such as GMS, GOES-9 and MTSAT-1R since 2001. The Dvorak technique is so subjective that the analysis results could be variable according to analysts. To reduce the subjective errors, QuikSCAT seawind data have been used with various analysis data including sea surface temperature from geostationary meteorological satellites, polar orbit satellites, and other observation data. On the other hand, there is an advantage of using the Subjective Dvorak Technique(SDT). SDT can get information about intensity and center of typhoon by using only infrared images of geostationary meteorology satellites. However, there has been a limitation to use the SDT on operational purpose because of lack of observation and information from polar orbit satellites such as SSM/I. Therefore, KMA has established Advanced Objective Dvorak Technique(AODT) system developed by UW/CIMSS(University of Wisconsin-Madison/Cooperative Institude for Meteorological Satellite Studies) to improve current typhoon analysis technique, and the performance has been tested since 2005. We have developed statistical relationships to correct AODT CI numbers according to the SDT CI numbers that have been presumed as truths of typhoons occurred in northwestern pacific ocean by using linear, nonlinear regressions, and neural network principal component analysis. In conclusion, the neural network nonlinear principal component analysis has fitted best to the SDT, and shown Root Mean Square Error(RMSE) 0.42 and coefficient of determination($R^2$) 0.91 by using MTSAT-1R satellite images of 2005. KMA has operated typhoon intensity analysis using SDT and AODT since 2006 and keep trying to correct CI numbers.

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THE ADVANTAGE OF ON ORBIT NON-UNIFORMITY CORRECTION FOR MULTI SPECTRAL CAMERA (MSC)

  • Chang Young-Jun;Kong Jong-Pil;Huh Haeng-Pal;Kim Young-Sun;Park Jong-Euk
    • 대한원격탐사학회:학술대회논문집
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    • 대한원격탐사학회 2005년도 Proceedings of ISRS 2005
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    • pp.586-588
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    • 2005
  • The MSC (Multi Spectral Camera) system is a remote sensing payload to obtain high resolution ground image. This system uses lossy image compression method for &Direct mission& that transmit whole image during one contact. But some image degradation occurred especially at high compression ratio. To reduce this degradation, the MSC uses NUC (Non-uniformity Correction) Unit. This unit correct CCD (Charge Coupled Device)'s high-frequency non-uniformity. So high frequency contents of image can be minimized and whole system SNR can be maximized. But NUC has some disadvantage either. It decreases entire system reliability by adding one electronic system. Adding NUC also led to difficulty of electronic design, assembly and testability. In this paper, the comparison is performed between on-orbit non-uniform correction and on ground correction. by evaluating NUC advantage for the point of view of image quality. Using real MSC parameter and proper model, considerable reference point for the system design came to possible.

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인공위성 궤도의 추적과 예보의 기술개발(I) -예비궤도 결정법에 관한 연구- (A Study on the Tracking and Position Predictions of Artificial Satellites(I) - A Study on the Methods of the Preliminary Orbit Determination-)

  • 김천휘;신종섭;박필호;김두환;이병선;조중현;이정숙;박상영;최규홍
    • Journal of Astronomy and Space Sciences
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    • 제5권1호
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    • pp.45-51
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    • 1988
  • 지주주위를 선회하는 안공위성의 예"1궤도를 결정하는 대부분의 모든 땅뱀을을 채조사하였다. 조사판 앙법들을 이용하켜 기상위성 NOAA-10호의 예비궤도릎 결청하였고 그 결과들을 NASA에서 계산된 NOAA-10호 위성의 평균궤도요소와 비교하였다. 이 비교를 통하여 Ga-uss형 방법들에 의하여 결정된 예비궤도요소들이 Laplace형 방법들에 의한결과보다NASA의 평균궤도요소에 더 가깝게 계산되었다. 우리의 결과는 Gauss방법에 대한 Taff(l984) 의 비판이 재고되어야 함을 보여 주며 따라서 Marsden ( 1985 )의 견해를 뒷받침한다.

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인공위성 추적자료의 미분보정에 의한 궤도결정 (Orbit Determination from Tracking Data of Artificial Satellite Using the Method of Differential Correction)

  • 이병선;조중현;박상영;최규홍;김천휘
    • Journal of Astronomy and Space Sciences
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    • 제5권1호
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    • pp.31-43
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    • 1988
  • 인공위성의 추적자료로부터 예비궤도를 결정하고 이것을 초기값으로 해서 계산한 관측치 (C) 와 실제의 관측치(O)의 차이가 최소가 될때까지 반복계산함으로써, 어떤 시각에 있어서 실제의 궤도에 가장 가까운 접융궤도 요소를 얻어내는 미분보정의 과정을 수행했다. 추적한 인공 위성은 TIROS-N계열 위성인 NOAA - 9이고 추척자료는 컴퓨터에 의한 프로그랭 추척을 위해서 TBUS의 평균궤도요소로부터 미리 계산한 예측자료와 위성으후부터 송신되는 1.707GHz의 HRPT신호를 전파연구소의 직경 5m인 자동추적안테나로 추적해서 얻은 실제 자료를 이용했다. 예비궤도의 결정은 추적 자료에 따라 Gauss 방법과 Herrick -Gibbs 방법을 사용했고 미분보정의 과정에 있어서 미분보정행렬의 각 원소들은 Escobal(1975)의 해석적인 방법과 f, g급수를 이용한 수치적인 방법으로 각각 구해서 그 결과를 비교해 보았다. 해석적인 방법파 수치적인 방법의 결과는 거의 일치하였고 각 시간간격에 따른 예비궤도가 다름에도 불구하고 미분보정된 궤도는 같은 값으로 수령했다.

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The Generation of True Orthophotos from High Resolution Satellites Images

  • Chen, Liang-Chien;Wen, Jen-Yu;Teo, Tee-Ann
    • 대한원격탐사학회:학술대회논문집
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    • 대한원격탐사학회 2003년도 Proceedings of ACRS 2003 ISRS
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    • pp.885-887
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    • 2003
  • The purpose of this investigation is to generate true orthophotos from high resolution satellite images. The major works of this research include 4 parts: (1) determination of orientation parameters, (2) generating traditional orthophotos using terrain model, (3) relief correction for buildings, and (4) process for hidden areas. To determine the position of satellites, we correct the onboard orientation parameters to fine tune the orbit. In the generation of traditional orthophotos, we employ orientation parameters and digital terrain model(DTM) to rectify tilt displacements and relief displacements for terrain. We, then, compute relief displacements for buildings with digital building model (DBM). To avoid double mapping, we detect hidden areas. Due to the satellite’s small field of view, an efficient method for the detection of hidden areas and building rectification will be proposed in this paper. Test areas cover the city of Kaohsiung in southern Taiwan. Test images are from the QuickBird satellite.

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DSM GENERATION FROM IKONOS STEREO IMAGERY

  • Rau, Jiann-Yeou;Chen, Liang-Chien;Chang, Chih-Li
    • 대한원격탐사학회:학술대회논문집
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    • 대한원격탐사학회 2003년도 Proceedings of ACRS 2003 ISRS
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    • pp.57-59
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    • 2003
  • Digital surface model generation from IKONOS stereo imagery is a new challenge in photogrammetric community, especially when the satellite company does not provide the raw data as well as their ancillary ephemeris data. In this paper we utilized an estimated relief displacement azimuth and the nominal collection elevation data included in the metadata file to correct the relief displacement of GCPs, together with a linear transformation for geometric modeling of IKONOS imagery. Space intersection is performed by the trigonometric intersection assuming a parallel projection of IKONOS imagery due to its small FOV and frame size. In the experiment, less than 2-meters of RMSE in orbit modeling is achieved denoting the potential positioning accuracy of the IKONOS stereo imagery.

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외상 후 안면변형에 대한 지연재건술 (Delayed reconstruction of posttraumatic facial deformities)

  • 김용하
    • 대한의사협회지
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    • 제61권12호
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    • pp.740-748
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    • 2018
  • Posttraumatic facial deformities (PTFDs) are very difficult to correct, and if they do occur, their impact can be devastating. It may sometimes be impossible for patients to return to normal life. The aim of surgical treatment is to restore the deformed bone structure and soft tissue to create symmetry between the affected side and the opposite side. In the process of managing PTFD, correcting enophthalmos is one of the most challenging aspects for surgeons because of difficulties in overcoming the scar tissue and danger of injuring to the optic nerve. In this article, surgical options for reconstruction of the medial wall, floor, lateral wall, and roof of the orbit are described. To optimize aesthetic improvement, additional cosmetic procedures such as facial contouring surgery, blepharoplasty and rhinoplasty can be used. Plastic surgeons should join emergency trauma teams to implement an overall treatment plan containing rational strategies to avoid or minimize PTFD.

Correction of post-traumatic enophthalmos with anatomical absorbable implant and iliac bone graft

  • Choi, Ji Seon;Oh, Se Young;Shim, Hyung-Sup
    • 대한두개안면성형외과학회지
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    • 제20권6호
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    • pp.361-369
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    • 2019
  • Background: Trauma is one of the most common causes of enophthalmos, and post-traumatic enophthalmos primarily results from an increased volume of the bony orbit. We achieved good long-term results by simultaneously using an anatomical absorbable implant and iliac bone graft to correct post-traumatic enophthalmos. Methods: From January 2012 to December 2016, we performed operations on seven patients with post-traumatic enophthalmos. In all seven cases, reduction surgery for the initial trauma was performed at our hospital. Hertel exophthalmometry, clinical photography, three-dimensional computed tomography (3D-CT), and orbital volume measurements using software to calculate the specific volume captured on 3D-CT (ITK-SNAP, Insight Toolkit-SNAP) were performed preoperatively and postoperatively. Results: Patients were evaluated based on exophthalmometry, clinical photographs, 3D-CT, and orbital volume measured by the ITK-SNAP program at 5 days and 1 year postoperatively, and all factors improved significantly compared with the preoperative baseline. Complications such as hematoma or extraocular muscle limitation were absent, and the corrected orbital volume was well maintained at the 1-year follow-up visit. Conclusion: We present a method to correct enophthalmos by reconstructing the orbital wall using an anatomical absorbable implant and a simultaneous autologous iliac bone graft. All cases showed satisfactory results for enophthalmos correction. We suggest this method as a good option for the correction of post-traumatic enophthalmos.