• Title/Summary/Keyword: Flight Procedure

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A Research on Knowledge Sharing among Air Transportation Professionals (이직종간 지식공유 활성화 방안에 대한 연구 : 항공운항 분야를 중심으로)

  • Kim, Wan-Hyun;Park, Sang-Bum
    • The Journal of Industrial Distribution & Business
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    • v.8 no.6
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    • pp.61-73
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    • 2017
  • Purpose - Aviation control, navigation, and aircraft control in the air transportation area are very specialized. Each part is in progress for safety, efficiency, automation, and further. On the other hand co-work among each part including knowledge sharing has been inattentive for many reasons. The purpose of this research is to show how practicians and professionals in the air transportation area perceive the issue of knowledge sharing and to recall the necessity of knowledge sharing in the area. And we try to find ways to activate the knowledge sharing in the area. Research design, data, methodology - For the research, we inquired into whether practicians and professionals think knowledge sharing can effect safe aviation positively or not and what steps are necessary to activate knowledge sharing in the area. We adopted survey method using questionnaires for current practicians and interview for specialists. The survey and interview results were analyzed using regression analysis and AHP method. The interview for specialists and analyzing the results using AHP was to investigate what are the precedence factors to activate the knowledge sharing. Results - First, practicians perceive that knowledge sharing will affect aviation safe positively. Second objective knowledges such as, tower air traffic control procedure of aviation control area, flight principle and structure of aircraft control area, instrument landing system of navigation area, for knowledge sharing of each area were identified. Also the precedence factors such as, knowledge absorbability of personal factor, personal expectation of result of expectation factor, leadership of management of Structure factor, method of knowledge spread of application factor for knowledge sharing were found. Conclusions - Knowledge sharing for practicians and professionals in the aviation area is very important especially from the perspective of safety. However, for various many reasons including the environment of each special area that focusing on their own area, knowledge sharing has not been emphasized. We found that practicians in the area feel that knowledge sharing is necessary and helpful. For it, each practician's active participation is the most important and many ways such as chatting room to share knowledge are to be developed. And the organization culture should be changed to encourage knowledge sharing.

Real 3-D Shape Restoration using Lookup Table (룩업 테이블을 이용한 물체의 3-D 형상복원)

  • Kim, Kuk-Se;Lee, Jeong-Gi;Song, Gi-Beom;Kim, Choong-Won;Lee, Joon
    • Journal of the Korea Institute of Information and Communication Engineering
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    • v.8 no.5
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    • pp.1096-1101
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    • 2004
  • The 3-D shape use to effect of movie, animation, industrial design, medical treatment service, education, engineering etc.... But it's not easy to make 3-D shape from the information of 2-D image. There are two methods in restoring 3-D video image through 2-D image; First the method of using a laser; Secondly the method of acquiring 3-D image through stereo vision. Instead of doing two methods with many difficulties, I figure out the method of simple 3-D image in this research paper. We present here a simple and efficient method, called direct calibration, which doesn't require any equations at all. The direct calibration procedure builds a lookup table(LUT) linking image and 3-D coordinates by a real 3-D triangulation system. The LUT is built by measuring the image coordinates of a grid of known 3-D points, and recording both image and world coordinates for each point; the depth values of all other visible points are obtained by interpolation.

Clinical and Radiogical Outcomes of Endovascular Detachable Coil Embolization in Paraclinoid Aneurysms : A 10-Year Experience

  • Jin, Sung-Chul;Kwon, Do-Hoon;Ahn, Jae-Sung;Kwun, Byung-Duk;Song, Young;Choi, Choong-Gon
    • Journal of Korean Neurosurgical Society
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    • v.45 no.1
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    • pp.5-10
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    • 2009
  • Objective : Direct surgical clipping of paraclinoid aneurysms poses technical challenges to even very experienced neurosurgeons, making endovascular treatment an alternative treatment modality in many centers. We have therefore retrospectively evaluated the safety and efficacy of endovascular detachable coil embolization of paraclinoid aneurysms. Methods : From June 1997 to June 2007, 65 patients underwent endovascular detachable coiling for 67 paraclinoid aneurysms (of which 9 were ruptured and 58 were unruptured) in our institute. Their medical records, radiological images and readings, and operation records were reviewed retrospectively. Results : After the initial embolization procedure, complete occlusion was achieved in 29 (43.3%) of the aneurysms treated by endovascular detachable coiling. Six aneurysms required retreatment, with two each requiring one, two, or three additional endovascular procedures. Fifty-five (82.1%) aneurysms were measured by three-dimensional time of flight (TOF) magnetic resonance images (MRI) or transfemoral cerebral angiography (TFCA) at a mean follow-up of 29.7 months (range from 4 to 94 months), with 39 aneurysms (70.9%) showing complete occlusion. Thromboembolic events (3.8%) were the most frequent complication. Rupture did not occur during or after any of the procedures. According to the Glasgow Outcome Scale (GOS), 98.4% of the patients treated by coil embolization had a score of 4 or 5. Conclusion : Our results indicate that endovascular detachable coiling is a safe and effective treatment modality in paraclinoid aneurysms.

Study on Contralateral Collateral Needling(繆刺) from Neijing(黃帝內經) ("황제내경(黃帝內經)"에 나타난 무자(繆刺)에 대한 연구)

  • Kang, Jung-Soo
    • Journal of Haehwa Medicine
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    • v.22 no.1
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    • pp.1-10
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    • 2013
  • Through a consideration of the contralateral collateral needling(繆刺) from "Neijing", the conclusions are as follows. The contralateral collateral needing is defined as a disordered state, and also as the pricking bloodletting method. Unlike the seasonal deficiency pathogen(虛邪), which are affected by the four seasons, the subject of the contralateral collateral needling is the extra pathogen(奇邪), which is the cause of the extra disease(奇病), therefore the treatment should be different from the general. The contralateral collateral needling is generally used when a pain is generated from the veins(絡) by an external pathogen(邪). However, it can be used as the treatment for an emotional disorder, such as flight or sorrow, or a body constituent(身形) disorder caused by internal parts of the five viscera. Although the contralateral collateral needling(繆刺) and the contralateral meridian needling(巨刺) share the left and right cross treatment(右取左, 左取右) in common, but they are different in every aspect, as the causes, transmutation, location, and feature of disease, relation of qi and blood, and location and method of needling(刺鍼). The medical procedure of the contralateral collateral needling is collateral needling(刺絡) the parts of blood collaterals(血絡) or bruising(痏) well points(井穴) of the end of the both sides of limbs, and using the left and right cross treatment when the former methods are not making any progress. The symptoms of contralateral collateral needling are head, chest, and abdomen pains, and they are treated at the end of the limbs. The bloodletting method(刺絡法), extracting a little amount of blood at well points or blood collaterals, or the collateral vessel pricking therapy(瀉血法), extracting a lot of blood by using cupping(附缸), for example, are contemporary successions of the collateral needling(絡刺), the leopard-spot needling(豹文刺), and the contralateral collateral needling.

Flight Model Development of the MIRIS, the Main Payload of STSAT-3

  • Han, Won-Yong;Lee, Dae-Hee;Park, Young-Sik;Jeong, Woong-Seob;Moon, Bong-Kon;Park, Kwi-Jong;Park, Sung-Joon;Pyo, Jeong-Hyun;Lee, Duk-Hang;Nam, Uk-Won;Park, Jang-Hyun;Seon, Kwang-Il;Yang, Sun-Choel;Park, Jong-Oh;Rhee, Seung-Wu;Lee, Hyung-Mok;Matsumoto, Toshio
    • The Bulletin of The Korean Astronomical Society
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    • v.37 no.1
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    • pp.65.1-65.1
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    • 2012
  • MIRIS (Multipurpose Infra-Red Imaging System) is the first Korean Infrared Space Telescope developed by KASI (Korea Astronomy and Space Science Institute), and is the main payload of STSAT-3 (Science and Technology Satellite-3). The FM (fight model) of MIRIS has been recently completed, and various performance tests have been made to measure system parameters such as readout noise, system gain, linearity, and dark current. Final thermal-vacumm test of the MIRIS and the vibration test of the electronics box have been performed. Band response tests showed good agreement with the initial design requirements. No significant dark difference was measured within the expected temperature variation range during observation in orbit. Using Pa-alpha band from a uniform source, the readout noise and system gain were measured by mean variance test. To obtain uniform flat image, flat fielding tests were made for each band, and the data will be compared to that obtained in orbit for calibration. The final version of MIRIS FM will be delivered in March, and it will be integrated into the satellite system for the AIT (Assembly Integration, Test) procedure. The launch of MIRIS is expected in November 2012.

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Availability Performance Analysis of Korean Wide Area Differential GNSS Test Bed (한국형 광역보정시스템 테스트베드 가용성 성능 분석)

  • Yun, Ho;Kee, Chang-Don;Kim, Do-Yoon
    • Journal of Advanced Navigation Technology
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    • v.15 no.4
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    • pp.510-516
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    • 2011
  • For using Global Navigation Satellite System(GNSS) in the civil aviation, it should satisfies the Required Navigation Performances(RNPs) which are defined by International Civil Aviation Organization(ICAO). RNP defines the required accuracy, integrity, availability, continuity of each flight procedure. In order to guarantee user's integrity, user's protection level has to be overestimated. On the other hand, for improving user's availability, user's protection level has to be estimated tightly. Therefore protection level should be estimated as tight as possible while it assuring the user's integrity. This paper describes the current integrity function of Korean WAD GNSS test bed, and predicts the availability performance of Korean WAD GNSS by simulation.

Education and Training Measures on Multi-crew Pilot License(MPL) Application in Korea for Improving Air Navigation Safety (항행안전 증진을 위한 국내 부조종사자격증명(Multi-crew Pilot License; MPL)제도 도입 관련 교육·훈련방안)

  • Shin, Heakyung;Lee, Jang Ryong
    • Journal of Advanced Navigation Technology
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    • v.24 no.1
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    • pp.37-46
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    • 2020
  • Multi-crew pilot license (MPL) is a new pilot licensing concept introduced and operated by ICAO. Mostly, candidates for MPL are educated and drilled with competency-based trainings (CBTs). In this paper, to present education and training measures for the domestic MPL application, ICAO documents and Korea aviation laws for pilot licensing, domestic and foreign airlines' employee requirements, and status of operations related to MPL system are identified. Also feasibility of MPL application in Korea is reviewed by checking approved domestic aviation training institutions' capabilities, airlines' pilot demands, and concerns of airlines and trainees with MPL system. Finally, three education and training measures on MPL application in Korea for the air navigation safety are suggested.

Scaling Methods for Icing Wind Tunnel Test (결빙 풍동시험을 위한 스케일링 기법 연구)

  • An, Young-Gab;Myong, Rho-Shin
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.40 no.2
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    • pp.146-156
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    • 2012
  • In-flight icing remains as one of the most persistent hazards for aircraft operations. The effect of icing on aircraft performance and safety has to be evaluated during the development and airworthiness certification process. The scaling method is a procedure to determine the scaled test conditions in icing wind tunnels in order to produce the same result as when the reference model is exposed to the desired cloud conditions. In this study, a scaling program is developed to provide an easy-to-use tool to the aero-icing community. The Olsen and Ruff 4th methods are employed for this purpose and the velocity is calculated by matching the dimensionless Weber number. To validate the program, the results are compared with the NASA scaling results. The scaling examples based on FAR (Federal Aviation Regulation) Part 25 Appendix C are also presented. Finally, a validation study using a state-of-the-art icing simulation code FENSAP-ICE is presented.

The Aspects, Reasons and Outcomes of an Unmanned Air Vehicle Crash Caused By Engine Failure

  • Cuhadar, Ismet;Dursun, Mahir
    • International Journal of Aerospace System Engineering
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    • v.2 no.1
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    • pp.1-5
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    • 2015
  • The Unmanned Air Vehicle (UAV) systems are indispensable tools of air surveillance and reconnaissance nowadays. Via this systems, hazardous end risky intelligence gathering activities are handled easily. Although they are named as "Unmanned" the UAV systems are commanded by pilots/operators. So, because of weather conditions, enemy attacks etc. as well as pilot error it is possible to face with sudden Round per Minute (RPM) drops and subsequently engine cut/stop during a mission flight at high altitudes. In this case, there are some very urgent decisions to make and rapid "emergency procedure" steps to take in a very short time before Line of Sight (LOS) is lost. The time before crash and the distance to landing air base need to be calculated, the Return Home route need to be checked and the landing/crash side need to be determined. Therefore it is a vital necessity that UAV pilots have some extra qualifications like being determined, well instructed and trained, experienced apart from operating ability. Within this scope, for an education process of a UAV pilot experience sharing and lessons learned are as important as simulators even more. By means of lessons learned it is possible to find out the reasons, mistakes and prevent the likely UAV accidents. In this study it is told about a real UAV crash, experienced of the pilot, the dos and don'ts and the difficulties. Thus it is aimed to help the people who can experience the same or similar situations in future.

Thermal Vacuum Test of Kaistsat-4 Qm (과학위성 1호 인증모델 열진공 시험)

  • Kim, Do-Hyeong;Jeong, Yeon-Hwang;Tak, Gyeong-Mo;Lee, Jun-Ho;Cha, Won-Ho;Lee, Sang-Hyeon;Choe, Seok-Won;Mun, Gwi-Won
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.31 no.1
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    • pp.120-124
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    • 2003
  • KAISTSAT- 4, an experimental small satellite, is being developd by Satellite Technology Research Center in KAIST as a sequel mission to KITSAT-1, 2, and 3. The flight model scheduled to be launched in 2003, the qualification model construction and testing have been completed recently. The satellite subsystems of the qualification model have been tested under a thermal vacuum environment harsher than expected in the orbit. Thermal balance test has also been done in order to evaluate and tune the thermal analysis model of the qualification model. This paper describes the thermal vacuum test procedure, the results, as well as the lessons learned during the tests, which can be useful for future thermal vacuum tests of small satellites.