• International Journal of Aeronautical and Space Sciences
• /
• 제6권2호
• /
• pp.33-45
• /
• 2005

The 1/9-scale model of a fighter-type configuration was tested in the Micro-Craft 8ft ${\times}$ 12ft wind tunnel facility. An abrupt lift dump was found at a certain range of angle of attack under the pre-scheduled approach configuration. To avoid a probable unsatisfactory flight behavior due to the lift dump, various aerodynamic devices were suggested. Extensive tests applying the cutoff leading edge flaps, boundary layer fences, saw tooth and vortex generators were performed with flow visualization as well as force and moment measurements. Test results showed that the origin of the lift dump was caused by the secondary boundary layer flow separation generated from the strong interaction between wing and flap. Various solutions for avoiding the unfavorable feature were suggested with the merits and demerits.

• International Journal of Fuzzy Logic and Intelligent Systems
• /
• 제14권1호
• /
• pp.26-33
• /
• 2014

This study addresses the control problem of an unmanned aerial vehicle (UAV) during the transition period when the flying mode changes from hovering to translational motion in the horizontal plane. First, we introduce a compensation algorithm that improves height stabilization and reduces altitude drop. The main principle is to incorporate pitch and roll measurements into the feedforward term of the altitude controller to provide a larger thrust force. To further improve altitude control, we propose the fuzzy logic controller that improves system behavior. Simulation results presented in the paper highlight the effectiveness of the proposed controllers.

• 한국군사과학기술학회지
• /
• 제9권2호
• /
• pp.143-151
• /
• 2006

This paper investigates effects of reaction control jet on the aerodynamic performance of generic interceptor missile operating at supersonic flight condition. Parallelized CFDS code is used as a viscous flow solver. The generic interceptor missile configuration composed of a long and slender body and fixed tail fins. The behavior of normal force, axial force and pitching moment characteristics at altitude conditions corresponding to 10 km is studied according to the given control jet conditions, different angle of attacks based on the analysis of aerodynamic characteristics.

• 한국추진공학회:학술대회논문집
• /
• 한국추진공학회 2004년도 제23회 추계학술대회 논문집
• /
• pp.62-67
• /
• 2004

이 논문에서는 메탄을 연료로 하는 에어터보램제트(ATR) 엔진의 아음속 영역에서의 탈설계점 성능 해석을 수행하였다 이를 위하여 ATR 엔진을 수치적으로 모델링하여 성능을 모사하였다. 각 구성품에 대해 탈설계점 성능을 계산할 수 있도록 모델을 작성하였다. 압축기 작동점은 노즐과의 유량매칭(matching)에 의하여, 터빈 작동점은 일 매칭에 의하여 결정하였다. 성능 해석 결과, ATR 엔진은 기존의 개스 터빈 엔진과 비교해 상당히 다른 탈설계점 특성을 가지고 있음을 보였다.

• 항공우주시스템공학회지
• /
• 제17권1호
• /
• pp.24-32
• /
• 2023

본 논문에서는 기 개발된 로터 블레이드 해석 모델 중 구조 모델을 보완하여 기존에 수행한 HART II의 연구결과와 비교하였다. 구조 모델은 혼합변분 정식화 기반의 기하학적 정밀 보 모델이며, 블레이드의 기하학적 비선형 거동을 정밀하게 예측할 수 있다. 기존 해석 결과에서는 비틀림 변형과 구조하중 결과에서 실험결과 대비 위상차가 발생하였는데 본 연구에서는 기존 결과 대비 위상차가 현저히 감소한 결과를 도출하였다.

• 한국근적외분광분석학회:학술대회논문집
• /
• 한국근적외분광분석학회 2001년도 NIR-2001
• /
• pp.1627-1627
• /
• 2001

In this study, a newly constructed optical measurement system, whose main components were a parametric tunable laser and a near infrared photoelectric multiplier, was applied to detection of the information for the inside of Satsuma mandarin using time-of-flight near infrared spectroscopy (TOF-NIRS). The combined effects on the time resolved profile of sample diameter, sugar content, the wavelength of the laser beam, and the detection position of transmitted light were investigated in detail. The samples used were Satsuma mandarin (Citrus unshu $M^{ARC}$.) (location: Wakayama, Japan) having the diameters of 50-84 mm. The sugar content measured by a refractometer varied from 9.9 to 16.3 Brix%. Equator of sample was irradiated vertically with the pulsed laser, and transmitted output power was measured on the restricted position of the equator using the optical fiber cable. The sampling time and the number of averaging the output power were 100 ns and 100 times, respectively. The variation of the attenuance of peak maxima At, the time delay of peak maxima t and the variation of full width at half maximum w were strongly dependent on the detection position and the wavelength of the laser beam. At, t and w increased gradually as the sample diameter increased to be much absorbed and vigorously scattered. On the other hand, each optical parameter had a tendency to increase as the sugar content increased. Such behavior was remarkable when the transmitted light was detected at the side face of a sample. When we apply TOF-NIRS to detection of the information for the inside of fruit with high moisture content like Satsuma mandarin, it is very important to give attention to the difference in the scattered light within tissues and the semi-straightly propagated light. Furthermore, we tried to express the resulting phenomena by using a model samples composed of water, sucrose, and milk. The variation of the time resolved profile is strongly governed by the combination of the light absorption component, scattering medium, and refractive index.

• 한국근적외분광분석학회:학술대회논문집
• /
• 한국근적외분광분석학회 2001년도 NIR-2001
• /
• pp.1626-1626
• /
• 2001

In this study, a newly constructed optical measurement system, whose main components were a parametric tunable laser and a near infrared photoelectric multiplier, was applied to detection of the information for the inside of Satsuma mandarin using time-of-flight near infrared spectroscopy (TOF-NIRS). The combined effects on the time resolved profile of sample diameter, sugar content, the wavelength of the laser beam, and the detection position of transmitted light were investigated in detail. The samples used were Satsuma mandarin (Citrus unshu $M_{ARC}$.) (location: Wakayama, Japan) having the diameters of 50-84 mm. The sugar content measured by a refractometer varied from 9.9 to 16.3 Brix%. Equator of sample was irradiated vertically with the pulsed laser, and transmitted output power was measured on the restricted position of the equator using the optical fiber cable. The sampling time and the number of averaging the output power were 100 ns and 100 times, respectively. The variation of the attenuance of peak maxima At, the time delay of peak maxima $\Delta$t and the variation of full width at half maximum Δw were strongly dependent on the detection position and the wavelength of the laser beam. At, $\Delta$t and $\Delta$w increased gradually as the sample diameter increased to be much absorbed and vigorously scattered. On the other hand, each optical parameter had a tendency to increase as the sugar content increased. Such behavior was remarkable when the transmitted light was detected at the side face of a sample. When we apply TOF-NIRS to detection of the information for the inside of fruit with high moisture content like Satsuma mandarin, it is very important to give attention to the difference in the scattered light within tissues and the semi-straightly propagated light. Furthermore, we tried to express the resulting phenomena by using a model samples composed of water, sucrose, and milk. The variation of the time resolved profile is strongly governed by the combination of the light absorption component, scattering medium, and refractive index.

• 한국위성정보통신학회논문지
• /
• 제6권1호
• /
• pp.50-56
• /
• 2011

위성 탑재소프트웨어를 개발하는 과정에서 프로세서 에뮬레이터와 위성 시뮬레이터는 핵심 개발 툴로서, 탑재소프트웨어 개발/검증 전반에 사용하며 실제 하드웨어를 대체할 수 있는 수준까지 활용이 가능하다. 현재 한국항공우주연구원에서 개발하는 저궤도 위성의 경우 ERC32 프로세서를 사용하며 Aeroflex Gaisler에서 판매하는 TSIM-ERC32 에뮬레이터를 사용하여 탑재소프트웨어 시뮬레이터를 개발하여 탑재소프트웨어 개발 및 테스트에 사용하였으나, 실제 위성 시뮬레이터를 개발하는 과정에서 에뮬레이터 코어를 개발자가 원하는 방식으로 수정 및 변경할 수 없는 문제와 위성 시뮬레이터 연동 시 인터페이스를 쉽게 구현할 수 없는 문제가 발생한다. 본 논문에서는 이러한 문제들을 해결하기 위해 ERC32 코어를 정확히 에뮬레이션 할 수 있는 인터프리트 방식의 Cycle True 에뮬레이터 개발 방법에 대해서 기술하며 에뮬레이터를 이용한 RTOS 기반의 소프트웨어 개발 및 디버깅 환경에 대해서 설명한다.

• 한국추진공학회:학술대회논문집
• /
• 한국추진공학회 2009년도 제33회 추계학술대회논문집
• /
• pp.573-577
• /
• 2009

초음속제트 엔진의 동적거동 모사를 수행하고 흡입구에서의 버즈 마진 확보와 추력 제어를 위한 PI 제어 알고리즘을 연구하였다. 먼저 연료유량 제어를 통해 요구추력을 추종하고 노즐 목 면적 제어를 통해 흡입구에서의 버즈마진이 항상 양의 수를 갖도록 흡입구 출구 압력을 조절하였다. 비행 마하 수, 고도, 받음각 변화에 따라 추력제어와 버즈 마진 제어를 위한 비례 게인과 적분 게인을 각각 구하고 시뮬레이션 하였다. 그 결과 비행 마하 수 2.1에서 3.0, 받음각 $0^{\circ}$에서 $10^{\circ}$ 사이의 운용영역에서 제어목표를 만족함을 확인하였다.

• 한국환경과학회지
• /
• 제29권8호
• /
• pp.809-818
• /
• 2020

To conserve the population of a hesperiid butterfly, Leptalina unicolor, inhabiting the protected areas of Jaeyaksan, we provide ecological information on their behavior and propose habitat conservation measures, such as the creation of alternative habitats based on comprehensive information. The behavioral study used a method of re-capture after releasing the butterfly with enamel marks on the wings. Adult behaviors were shown in four patterns: flying, settling on a plant, nectar absorption, and water absorption. Both males and females had the highest proportion of flight movement overall; however, males had a slightly higher proportion of flight movement. As for duration, females spent more time settling on plants to select spawning sites, and males seemed to take a longer time for water absorption activities, to absorb minerals needed to form the spermatophore. The average travel distance of butterflies was 27.5 m for females and 46.7 m for males, with daily activity ranges from 11.2 m to 43.8 m, and 21.4 to 57.6 m, respectively. The most important condition to preserve the habitat of Leptalina unicolor is to maintain the community of Miscanthus sinensis, a food plant. Additionally, because this butterfly has a high rate of water absorption activities, wetlands should be maintained.