• 한국품질경영학회:학술대회논문집
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• 한국품질경영학회 2010년도 춘계학술대회
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• pp.454-461
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• 2010

Six sigma is a business management strategy and is used to improve the quality of the products and processes in many organizations. However traditional six sigma methodology, namely DMAIC, is not suitable for developing products. This paper investigates DFSS methodologies and presents a DFSS methodology for order based industry. Specifically, we suggest a customized DMADV method for order based industry and present a case study for developing a configuration optimization of the flying simulators.

• 한국경영과학회:학술대회논문집
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• 한국경영과학회 2001년도 추계학술대회 논문집
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• pp.35-38
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• 2001

This study was conducted a comparative study to identify the differences in service quality between Incheon and Kimpo international Airport and critical factors influencing satisfaction of airport customers. According the results of this study, all service quality factors except the service factor of geographical location of Incheon international airport are better than those of Kimpo international airport. However, all of service quality factors of Incheon airport are evaluated as inferior to those of american, western european and japanese international airports by both the airport visitors and the employees of one korean airliner. In addition the service factors such as response, safety, airport facility and geographical location are found as critical factors influencing satisfaction of the airport visitors and the airliner's employees. Among them the service quality factor of geographical location of Incheon airport is much inferior to that of Kimpo airport comparing with other service quality factors. Thus, the results of this study suggest that the managing team implement TQM and six sigma to enhance the service quality level of the Incheon international airport up to that of the american and western european international airport. Especially, it is strongly required that the Korean governmen deliberate in deciding the geographical location in case of planning new international airport because geographical location is related to not only traffic to airport but also safety of landing, taking off and flying.

• 한국항공우주학회지
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• 제47권2호
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• pp.114-121
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• 2019

무미익 항공기는 꼬리 날개가 없기 때문에 일반적인 형태의 항공기에 비해 피탐성 낮으나 안정성이 좋지 않아 제어기를 설계하는 것이 쉽지 않다. 특히 비행 중에 임무장비 투하나 연료 소모 등에 의해 무게중심의 위치가 변화하는 것을 고려한다면 제어기 설계는 더욱 더 어렵게 된다. 본 논문에서는 이러한 문제점을 극복하기 위한 방법으로 L1 적응제어 방식을 제안하며 비선형 시뮬레이션을 통하여 제어기의 안정성과 성능을 검증하였다. 설계지표 선정을 위해 RPV Flying Quality Design criteria의 내용을 참고하였다. 시뮬레이션을 이용하여 급격한 관성량의 변화에 대해 설계된 적응제억기가 무미익 항공기 안정성을 유지하는 것을 보이고, 이득 스케쥴링 기법과 함께 사용 시 계산량이 줄어들 수 있음을 확인하였다.

• 한국측량학회지
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• 제39권2호
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• pp.81-91
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• 2021

Drone related research has been increasing recently due to the development and distribution of commercial unmanned aerial vehicles. However, most of the previous studies focused on the accuracy and utility of drone surveying. For drones, the resolution of the result is determined according to the flight altitude, but since 70% of Korea is mountainous, it is necessary to analyze the quality of the drone image according to the flight plan. In this study, the quality of drone photogrammetry results according to flight plans was analyzed. The flight plan was established by fixed altitude and considering the height of the terrain. Images were acquired for both cases and data was processed to generate ortho images. As a result of evaluating the accuracy of the generated ortho image, the accuracy was found to be -0.07 ~ 0.09m. The accuracy of Case I and Case II did not show a significant difference, but for RMSE, Case I showed a good value. These results indicate that the drone flight plan affects the quality of the results. Also, when flying at a fixed altitude, II showed a lower value than the originally set overlap according to the altitude of the object. In future surveys using drones, flight planning taking into account the height of the object will contribute to the improvement of the quality of the results.

• Journal of Astronomy and Space Sciences
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• 제28권4호
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• pp.285-290
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• 2011

This paper presents an algorithm that can provide initial conditions for formation flying at the beginning of a region of interest to maximize scientific mission goals in the case of a tetrahedral satellite formation. The performance measure is to maximize the quality factor that affects scientific measurement performance. Several path constraints and periodicity conditions at the beginning of the region of interest are identified. The optimization problem is solved numerically using a direct transcription method. Our numerical results indicate that there exist an optimal configuration and states of a tetrahedral satellite formation. Furthermore, the initial states and algorithm presented here may be used for reconfiguration maneuvers and fuel balancing problems.

• 제어로봇시스템학회:학술대회논문집
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• 제어로봇시스템학회 2005년도 ICCAS
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• pp.449-452
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• 2005

For home networking system with a function of air quality monitoring, a wireless sensor module with several air quality monitoring sensors was developed for indoor environment monitoring system in home networking. The module has various enlargements for various kinds of sensors such as humidity sensor, temperature sensor, CO2 sensor, flying dust sensor, and etc. The developed wireless module is very convenient to be installed on the wall of a room or office, and the sensors in the module can be easily replaced due to well designed module structure and RF connection method. To reduce the system cost, only one RF transmission block was used for sensors' signal transmission to 8051 microcontroller board in time sharing method. In this home networking system, various indoor environmental parameters could be monitored in real time from RF wireless sensor module. Indoor vision was transferred to client PC or PDA from surveillance camera installed indoor or desired site. Web server using Oracle DB was used for saving the visions by web-camera and various data from wireless sensor module.

• 복식
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• 제50권7호
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• pp.129-139
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• 2000

The Chonmachong (Tumulus No. 155 in Whangnam-dong, Kyungju, Korea), which was unearthed in 1973, is an ancient tomb built in the Shilla Era between the 5th∼6th centuries by the method of Juk-suk-mok-gwak. With the excavation of this tomb more than 11,500 articles of luxurious and splendid relics including gold and silver ornaments, weaponry and horse gears were obtained. Among the excavated articles, the saddle flap with a drawing of flying horse on it is the first relic of its kind from the Shilla Era. and 'Chonma'(a flying horse), the name of the tomb. was named after this drawing. The saddle flap is highly valuable in that it provides the idea of how goad the people of Shilla were at drawing. Although a lot of researches have been released about the relics from the Chonmachong, this study is to focus on the fabrics from the excavation, all of which are in the Kyongiu Museum's collection. The findings of this study are as follows : 1 The subject of this study is mainly on the fabrics used in horse gears, the pieces of cloth that were used to spread on a saddle or to underlay beneath a saddle. As the Shilla Dynasty tried to restrict excessive ornamentation on horses and it is assumed that the fabrics used are different. according to the social status. 2. The subject articles are four plain fabrics, three fabrics of combined -construction and one braid, the warp-faced compound woven silks of combined-construction was found for the first tinge in Korea, and is the typical quality sick with patterns woven with dyed threads in different colors. 3. It is ascertained by the Chonmachong excavation that polychrome woven silk was used not only for the clothes of the upper classes but also for the ornaments of their horses in the Era of the Three Kingdoms.

• 한국전자파학회논문지
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• 제15권3호
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• pp.311-318
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• 2004

PCM/FM과 같은 디지털 변조 방식의 텔레메트리 시스템에 있어서 비트 에러율(BER)을 최소화하여 수신된 신호의 품질을 향상시키기 위해서는 충분히 안정된 신호마진을 갖도록 회선설계가 이루어져야 한다. 특히 고속으로 이동하는 비행체의 경우에는 비행체 자세에 따른 송수신 안테나 사이의 안테나 이득패턴의 변화와 비행거리에 따른 손실이 동반되어지며 이로 인해서 회선상의 요동이 발생된다. 본 논문에서는 2002년 11월에 한국항공 우주연구원에서 시험 발사되었던 국내 최초 액체로켓 KSR-III의 비행시험 중에 S-대역 지상국에서 측정된 텔레메트리 신호의 신호대잡음비(SNR) 변화와 로켓의 비행 궤적 및 롤, 피치, 요 등의 자세변화를 고려하여 시뮬레이션으로 계산된 결과를 비교 분석하였으며 이를 통해 회선마진의 변화가 잘 일치함을 확인할 수 있었다. 또한, 탑재 안테나 개수가 1개인 경우와 롤 변화가 없는 가상의 비행 상황에 대해서 시뮬레이션을 수행하여 회선 변화를 예측할 수 있었다.

• 한국항공우주학회지
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• 제44권4호
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• pp.316-323
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• 2016

무인항공기는 자동모드에서는 사전에 계획된 항로점(비행이거나 이/착륙)들을 입력받아 자동으로 비행한다. 무인항공기는 수동모드에서도 유인항공기와 달리 조종사가 비행체에 탑승하지 않고 지상 통제실에서 조종입력을 인가하면 무선 데이터링크를 통하여 조종입력을 전달 받아 비행하게 된다. 데이터 링크는 여러 가지 이유로 통신두절이 될 수 있으며, 이때 무인항공기는 자동으로 비행모드를 수동에서 자동으로 전환하여 비행해야 한다. 그러므로 무인항공기에서 비행조종컴퓨터는 비행안전을 담당하는 매우 중요한 장비로 철저한 검증이 요구된다. 본 논문은 무인항공기의 비행제어컴퓨터가 비행성 요구조건을 만족하고, 다양한 고장이나 비상상황에서도 강건함을 입증할 수 있도록 비행제어 알고리즘의 검증환경인 HILS(Hardware In the Loop Simulation) 시험환경을 개발할 때 고려해야 할 사항들을 연구한 것으로 비행제어 HILS 시험환경의 구성장비들과 기타 고려사항 들을 제시한다.

• 한국항공우주학회지
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• 제40권3호
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• pp.251-257
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• 2012

무인기 및 유인기의 자동비행제어기는 다양한 비행성 규정, 안정도 여유 및 시간응답 특성에 대한 요구조건을 만족할 수 있도록 설계되어야 한다. 기존의 제어기 설계과정은 많은 시간과 시행오차를 수반하기 때문에 최적화 알고리즘을 활용하면 다양한 요구조건들을 충족시키는 제어기를 효율적으로 설계할 수 있다. 본 논문에서는 통합 최적화 제어설계 프로그램인 CONDUIT을 소형 무인기의 횡운동 SCAS 설계에 적용하여 그 효용성을 제시하였다. 최적화를 통해 설계된 롤 자세각 및 방위각 제어기는 시간응답특성만을 고려하여 설계한 기본제어기와 성능을 비교하고 분석하여, 최적화 기법을 적용한 제어기의 성능이 우수하고 다양한 비행성 요구조건을 충족시킬 수 있음을 확인하였다.