• Imaging Science in Dentistry
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• 제53권1호
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• pp.53-60
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• 2023

Purpose: This study evaluated maxillary sinus volume changes in military jet aircraft pilot candidates before and after the training program, in comparison with a control group, considering the effects of pressurization, altitude, and total flight hours, through multislice computed tomography. Materials and Methods: Fifteen fighter pilots were evaluated before initiating the training program and after the final approval. The control group consisted of 41 young adults who had not flown during their military career. The volumes of each maxillary sinus were measured individually before and at the end of the training program. Results: When comparing the initial and final volumes in the pilots, a statistically significant increase was observed both in the left and right maxillary sinuses. When evaluating the average total volume of the maxillary sinuses(i.e., the average volume of the right and left maxillary sinuses together), a significant increase in the volume of the maxillary sinuses was observed in the pilot group when compared to the control group. Conclusion: The maxillary sinus volumes in aircraft pilot candidates increased after the 8-month training program. This may be explained by changes in the gravitational force, the expansion of gas, and positive pressure from oxygen masks. This unprecedented investigation among pilots might lead to other investigations considering paranasal sinus alterations in this singular population.

• 대한기계학회:학술대회논문집
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• 대한기계학회 2004년도 추계학술대회
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• pp.625-630
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• 2004

An advanced method of Relaxed Static Stability (RSS) is utilized for improving the aerodynamic performance of modern version supersonic jet fighter aircraft. The laws of flight control system utilize RSS criteria in both longitudinal and lateral-directional axes to achieve performance enhancements. Particularly, the design of longitudinal control laws for utilizing RSS methods greatly affects the performance of the aircraft in Air-to-Air Tracking and Air-to-Ground modes, which improves weapon delivery. In the area of Airto- Air Tracking, the development of longitudinal control laws aids in the fine tracking and gross acquisition of other aircraft. This paper proposes that Air-to-Air fine tracking can be improved via RSS control law design methods without effecting Air-to-Air gross acquisition.

• 한국항공우주학회지
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• 제43권10호
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• pp.910-919
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• 2015

전투기 탑재용 무장제어 알고리듬은 교전상황에서 전투기의 임무 수행 및 생존과 직결된다. 공대지 유도탄의 경우 조종사에게 LAR로 알려진 발사 유효 범위를 무장제어 알고리듬을 통하여 전투기 MFD상에 전시해 준다. LAR는 교전 거리의 계산을 통해 산출된 사거리 테이블을 이용하여 생성된다. 본 논문에서는 AGM-84와 AGM-88 공대지 유도탄의 운용모의에 대하여 소개하고, 이를 바탕으로 Pseudo 6자유도 모델에 기반한 사거리 테이블 산출과 실시간 LAR 산출 알고리듬에 대한 내용을 언급하였다. 구성한 알고리듬의 성능 검증을 위하여 모의대상 유도탄의 교전 시뮬레이션을 수행하고 LAR를 산출하여 분석하였다.

• 한국항공우주학회지
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• 제42권9호
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• pp.762-772
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• 2014

전투기 탑재용 무장제어 알고리듬은 교전상황에서 전투기의 임무 수행 및 생존과 직결된다. 무장제어 알고리듬은 조종사에게 DLZ라 불리는 표적 격추 가능 범위를 HUD에 전시해 준다. DLZ는 교전거리 계산 알고리듬을 이용하여 생성된다. 본 논문에서는 AIM-9과 AIM-120 공대공 유도탄의 DLZ 구성요소에 대해 소개하였다. 다음으로 가상 6-자유도 실시간 시뮬레이션 프로그램에 기반한 DLZ 산출 알고리듬에 관한 내용을 다루었다. 다양한 교전 시나리오 하에서 공대공 유도탄의 DLZ 산출 알고리듬 운용상의 특징을 시뮬레이션을 통해 조사하였다.

• 항공우주의학회지
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• 제30권3호
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• pp.83-85
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• 2020

In commemoration of Vol. 30, Issue 3, our journal prepared five review articles and one original paper. The global outbreak of COVID-19 in 2020 has impacted our society, and especially the aviation and travel industries have been severely damaged. Kwon presented the aviation medical examination regulations related to COVID-19 announced by the Ministry of Land, Infrastructure, and Transport of the Republic of Korea. Lim summarized various efforts of airlines to overcome the crisis in the aviation industry. He also discussed the management of these aircraft as the number of airplanes landing for long periods increased. Finally, he suggested various quarantine guidelines at airports and onboard aircraft. COVID-19 has had a profound impact on mental health as well as physical effects. Kim investigated the impact of COVID-19 on mental health and suggested ways to manage the stress caused by it. The Internet of Things (IoT) refers to a technology in which devices communicate with each other through wired or wireless communication. Hyun explained the current state of the technology of the IoT and how it could be used, especially in the aviation field. In the area of airline service, various situations arise between passengers and crew. Therefore, role-playing is useful in performing education to prepare and respond to passengers' different needs appropriately. Ra introduced the conceptual background and general concepts of role-playing and presented the actual role-play's preparation process, implementation, evaluation, and feedback process. For a fighter to fly for a long time and perform a rapid air attack, air refueling is essential, which serves refueling from the air rather than from the aircraft base. Koo developed a questionnaire based on the HFACS (Human Factors Analysis and Classification System) model and used it to conduct a fighter pilot survey and analyze the results.

• 한국항공우주학회지
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• 제33권2호
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• pp.106-112
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• 2005

현대의 고성능 전투기는 공대공 및 공대지 전투 임무를 수행하기 위해 여러 가지 무장 형상을 하고 있고, 무장투하 시 비대칭 형상(Asymmetric Configuration)으로 임무를 수행하는 경우가 많다. 현재, 개발이 진행 중인 T-50 훈련기의 비대칭 무장형상 비행시험에서 세로축 기동 시 가로축 방향으로 조종사가 원하지 않는 운동이 발생하는데, 이는 항공기 안정성 및 조종성에 영향을 미칠 수 있다. 본 연구에서는 이러한 현상을 개선하기 위하여 기존의 가로축 제어법칙인 미끄럼각-미끄럼각속도 귀환 구조를 F-16과 같이 단순 롤각속도 귀환구조로 적용하였다. 연구결과, 단순 롤각속도 귀환구조로 가로축 제어법칙을 변경하였을 때 비대칭 무장형상에서 세로축 기동 시 가로축 운동의 발생이 줄어들었으며, 시스템의 안정도 여유는 설계기준에 만족한다는 것을 알 수 있었다.

• Journal of Acupuncture Research
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• 제39권3호
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• pp.202-212
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• 2022

Background: The aim of this study was to evaluate the effectiveness and safety of Cheong-A-Won Gagambang (JCE003) treatment for degenerative knee osteoarthritis. Methods: This was a single-center, randomized, double-blind, placebo-controlled pilot clinical trial. There were 36 adults with degenerative knee osteoarthritis who were randomly allocated into JCE003 1,000 mg, JCE003 2,000 mg, or the placebo group (in a 1:1:1 ratio). The participants received 12 weeks of treatment and had scheduled tests every 6 weeks. The primary outcomes were measured using the Korean Western Ontario and McMaster Universities scale, and the secondary outcomes were measured using the visual analog scale, European quality of life-5-dimensions, patient global impression of change, C-reactive protein, and erythrocyte sedimentation rate. Changes between baseline scores and scores following study completion were analyzed. Results: There were 29 participants whose data were analyzed in this study. The change of Korean Western Ontario and McMaster Universities, visual analog scale, European quality of life-5-dimensions scores showed significant improvement in the JCE003 1,000 mg group. The change of patient global impression of change was significantly improved in the placebo group. There were 14 adverse events, but there was no clinically significant relationship with the intake of JCE003 compared with the placebo. Conclusion: Taking JCE003 may be effective at improving knee pain in patients with degenerative knee osteoarthritis and appears to be safe. Based on this study, the concentration and feasibility of the test group may be used when conducting a large-scale clinical trial of degenerative knee osteoarthritis in the future.

• 제어로봇시스템학회논문지
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• 제17권1호
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• pp.12-16
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• 2011

Most car accidents occur when the driver does not look at the lane. Specially When the driver needs to find the path through the navigation, the driver have to look the other site. The number of such accidents can be prevented, if the driver receives the information without gazing other spot during the car is running. HUD (Head-Up Display) Technology, developed for enhancing the combat effectiveness and pilot's visibility in fighter, is applied to luxury cars for the safe operation of the driver. In recent years, the simple speed, lubrication status etc., as well as navigation information also shows through HUD. HUD is expected to increase in the future. But these HUD show the information elsewhere in the driver's eye focus. It is necessary to focus on the windshield for a few msec to check the information. In this paper, Introduced method display the HUD information in 3D as well as in similar distance the driver's eye focus so that the driver can operate the car more safely.

• 제어로봇시스템학회논문지
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• 제12권7호
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• pp.713-718
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• 2006

Supersonic jet fighter aircraft have several different weapon loading configuration to support air-to-air combat and air-to-ground delivery of weapon modes. Especially, asymmetric loading configurations could result in decreased handling qualities for the pilot maneuvering of the aircraft. The design of the T-50 lateral-directional roll axis control laws change from beta-betadot feedback structure to simple roll rate feedback structure and gains such as F-16 in order to improve roll-off phenomena during pitch maneuver in asymmetric loading configuration. Consequently, it is found that the improved control law decreases the roll-off phenomenon in lateral axes during pitch maneuver, but initial roll response is very fast and wing pitching moment is increased. In this paper, we propose the lateral control law blending between beta-betadot and simple roll rate feedback system in order to decreases the roll-off phenomenon in lateral axes during pitch maneuver without degrading of roll performance.

• 제어로봇시스템학회논문지
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• 제12권11호
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• pp.1130-1137
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• 2006

Relaxed Static Stability(RSS) concept has been applied to improve aerodynamic performance of modern version supersonic jet fighter aircraft. Therefore, the flight control systems are necessary to stabilizes the unstable aircraft and provides adequate handling qualities. The initial production flight control system are verified by flight test and it's always an elements of danger because of flight-critical nature of control law function and design error due to model base design method. These critical issues impact to flight safety, and it could be lead to a loss of aircraft and pilot's life. Therefore, development of an easily modifiable RFCS(Research Flight Control System) capable of reverting to a PFCS(Primary Flight Control System) of reliable control law must be developed to guarantee the flight safety. This paper addresses the concept of SSWM(Software Switching Mechanism) using the fader logic such as TFS(Transient Free Switch) based on T-50 flight control law. The result of the analysis based on non-real time simulation in-house software using SSWM reveals that the flight control system are switching between two computers without any problem.