• 제목/요약/키워드: flight quality

검색결과 329건 처리시간 0.029초

임무 기반 드론의 최적성능 및 소요량 분석 방법론 연구 (The Study on analysis methodology of optimal performance and quantity for Mission-Based drones)

  • 하영석
    • 인터넷정보학회논문지
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    • 제21권1호
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    • pp.231-236
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    • 2020
  • 본 논문은 드론 운영개념에 따라 체공시간, 총 운영시간, 적정 소요량 등 작전운용성능과 소요량의 과학적 검증이 필요하나, 이를 체계적으로 분석할 수 있는 방법론이 없어 본 연구를 수행하였다. 본 연구는 임무기반한 모의분석을 통한 검증 6단계의 분석 방법론 연구 및 제안을 통해 드론의 운용개념 기반의 최적 ROC와 소요량을 제시할 수 있으며, 그 결과 기술적, 경제적 효과를 제시 하였다.

Adaptive k-means clustering for Flying Ad-hoc Networks

  • Raza, Ali;Khan, Muhammad Fahad;Maqsood, Muazzam;Haider, Bilal;Aadil, Farhan
    • KSII Transactions on Internet and Information Systems (TIIS)
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    • 제14권6호
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    • pp.2670-2685
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    • 2020
  • Flying ad-hoc networks (FANETs) is a vibrant research area nowadays. This type of network ranges from various military and civilian applications. FANET is formed by micro and macro UAVs. Among many other problems, there are two main issues in FANET. Limited energy and high mobility of FANET nodes effect the flight time and routing directly. Clustering is a remedy to handle these types of problems. In this paper, an efficient clustering technique is proposed to handle routing and energy problems. Transmission range of FANET nodes is dynamically tuned accordingly as per their operational requirement. By optimizing the transmission range packet loss ratio (PLR) is minimized and link quality is improved which leads towards reduced energy consumption. To elect optimal cluster heads (CHs) based on their fitness we use k-means. Selection of optimal CHs reduce the routing overhead and improves energy consumption. Our proposed scheme outclasses the existing state-of-the-art techniques, ACO based CACONET and PSO based CLPSO, in terms of energy consumption and cluster building time.

밀리미터파(W 밴드) 탐색기용 FMCW SAR 영상의 2차원 엔트로피 최소 자동 초점 기법 (Two-Dimensional Entropy Minimizing Autofocusing of Millimeter-Wave (W-Band) FMCW SAR)

  • 박재현;전주환;이혁중;송성찬
    • 한국전자파학회논문지
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    • 제29권4호
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    • pp.316-319
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    • 2018
  • 전방 이동지상 표적 탐지를 위해 미사일은 FMCW 레이다를 통해 획득한 SAR 영상을 활용할 수 있다. 하지만 미사일 이동 과정에서 난기류 또는 비행경로 상태에 따른 요동 오차로 인해 SAR 영상의 품질이 떨어지게 된다. 본 논문에서는 이러한 전방을 바라보는 SAR 영상의 요동 오차를 보상하기 위한 엔트로피 최소 자동초점기법을 제안한다. 특히, 전방을 바라보는 레이다 특성 상, 요동 오차는 2차원의 형태(방위각 및 시간 축)로 SAR 영상에 영향을 미치며, 이를 보상하기 위해 2차원 자동초점기법을 제시한다.

Chemotype Discrimination and Rapid Identification of Angelica Roots by DART-TOF-MS

  • Kim, Hye-Jin;Piao, Xiang-Lan;Jang, Young-Pyo
    • Natural Product Sciences
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    • 제17권3호
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    • pp.202-205
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    • 2011
  • The Angelica root has been used as a medicinal herb in many Asian countries including Korea, China, and Japan. Angelica gigas, A. sinensis, and A. acutiloba have been considered as Angelicae radix in Korean, Chinese, and Japanese Pharmacopoeia, respectively. Since the origins of Angelicae radix differ from country to country, there is a need to develop an efficient analytical method to identify the origin of the Angelica root. In order to obtain chemical fingerprints, three different Angelicae Radices were analyzed by direct analysis in real time mass spectrometry (DART-MS). Significantly different DART-MS spectra were observed from three different species of Angelicae Radix. Strong peaks of decursin or decusinol angelate, and its dimer were exclusively found from A. gigas. Ligustilide and linoleic acid were detected as the major component from A. acutiloba. The strongest ligustilide peak was observed from A. sinensis. DART-MS fingerprinting is a promising method for the rapid identification and/or quality control of Angelicae Radix.

Metabolite Profiling during Fermentation of Makgeolli by the Wild Yeast Strain Saccharomyces cerevisiae Y98-5

  • Kim, Hye Ryun;Kim, Jae-Ho;Ahn, Byung Hak;Bai, Dong-Hoon
    • Mycobiology
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    • 제42권4호
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    • pp.353-360
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    • 2014
  • Makgeolli is a traditional Korean alcoholic beverage. The flavor of makgeolli is primarily determined by metabolic products such as free sugars, amino acids, organic acids, and aromatic compounds, which are produced during the fermentation of raw materials by molds and yeasts present in nuruk, a Korean fermentation starter. In this study, makgeolli was brewed using the wild yeast strain Saccharomyces cerevisiae Y98-5, and temporal changes in the metabolites during fermentation were analyzed by ultra-high-performance liquid chromatography-quadrupole-time-of-flight mass spectrometry. The resultant data were analyzed by partial least squares-discriminant analysis (PLS-DA). Various metabolites, including amino acids, organic acids, sugar alcohols, small peptides, and nucleosides, were obviously altered by increasing the fermentation period. Changes in these metabolites allowed us to distinguish among makgeolli samples with different fermentation periods (1, 2, 3, 6, 7, and 8 days) on a PLS-DA score plot. In the makgeolli brewed in this study, the amounts of tyrosine ($463.13{\mu}g/mL$) and leucine ($362.77{\mu}g/mL$) were high. Therefore, our results indicate that monitoring the changes in metabolites during makgeolli fermentation might be important for brewing makgeolli with good nutritional quality.

무인비행기 (UAV) 영상을 이용한 농작물 분류 (Crops Classification Using Imagery of Unmanned Aerial Vehicle (UAV))

  • 박진기;박종화
    • 한국농공학회논문집
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    • 제57권6호
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    • pp.91-97
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    • 2015
  • The Unmanned Aerial Vehicles (UAVs) have several advantages over conventional RS techniques. They can acquire high-resolution images quickly and repeatedly. And with a comparatively lower flight altitude i.e. 80~400 m, they can obtain good quality images even in cloudy weather. Therefore, they are ideal for acquiring spatial data in cases of small agricultural field with mixed crop, abundant in South Korea. This paper discuss the use of low cost UAV based remote sensing for classifying crops. The study area, Gochang is produced by several crops such as red pepper, radish, Chinese cabbage, rubus coreanus, welsh onion, bean in South Korea. This study acquired images using fixed wing UAV on September 23, 2014. An object-based technique is used for classification of crops. The results showed that scale 250, shape 0.1, color 0.9, compactness 0.5 and smoothness 0.5 were the optimum parameter values in image segmentation. As a result, the kappa coefficient was 0.82 and the overall accuracy of classification was 85.0 %. The result of the present study validate our attempts for crop classification using high resolution UAV image as well as established the possibility of using such remote sensing techniques widely to resolve the difficulty of remote sensing data acquisition in agricultural sector.

가스터빈 결빙시험용 결빙모사장치 개발 (Development of Icing Simulation Device for Gas Turbine Icing Test)

  • 이경재;이진근;고성희;전용민;양수석;이대성
    • 항공우주기술
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    • 제5권2호
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    • pp.37-46
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    • 2006
  • 항공기 운항 시 나타날 수 있는 외부환경 조건은 상당히 가혹하다. 특히 차가운 대기조 건에서 항공기 운항 시에는 미세한 얼음 알갱이들에 의해 항공기의 성능에 큰 영향을 줄 수 있다. 기체의 날개 앞전에 얼음이 부착되면 날개의 형상을 변화시켜 비행특성을 저하시 키며, 엔진의 흡입구 앞전에 부착하게 되면 압축기 블레이드의 손상뿐 아니라 성능 및 항 공기의 안전에도 영향을 미치게 된다. 얼음 알갱이들로 인한 여러 가지 상황 중 엔진 입구 로 유입되거나 엔진 압축기 블레이드에 생성되는 얼음 알갱이들로 인한 엔진 성능 변화 추이를 분석하기 위하여 결빙모사장치의 제작을 수행하였다. 결빙모사장치는 FAA에서 정 의한 결빙조건을 만족할 수 있도록 제작하였으며, 결빙모사장치와 기존 액체공기시스템을 이용하여 결빙이 생성됨을 시험을 통하여 확인하였다.

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초공동 수중운동체의 천이구간 특성을 고려한 동역학 모델링 및 심도제어 연구 (Study on Dynamics Modeling and Depth Control for a Supercavitating Underwater Vehicle in Transition Phase)

  • 김선홍;김낙완
    • 대한조선학회논문집
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    • 제51권1호
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    • pp.88-98
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    • 2014
  • A supercavitation is modern technology that can be used to reduce the frictional resistance of the underwater vehicle. In the process of reaching the supercavity condition which cavity envelops whole vehicle body, a vehicle passes through transition phase from fully-wetted to supercaviting operation. During this phase of flight, unsteady hydrodynamic forces and moments are created by partial cavity. In this paper, analytical and numerical investigations into the dynamics of supercavitating vehicle in transition phase are presented. The ventilated cavity model is used to lead rapid supercavity condition, when the cavitation number is relatively high. Immersion depth of fins and body, which is decided by the cavity profile, is calculated to determine hydrodynamical effects on the body. Additionally, the frictional drag reduction associated by the downstream flow is considered. Numerical simulation for depth tracking control is performed to verify modeling quality using PID controller. Depth command is transformed to attitude control using double loop control structure.

특이섭동법을 이용한 비행체 자동착륙 유도제어 알고리즘 설계 (Design of Autolanding Guidance and Control Algorithm Using Singular Perturbation)

  • 하철근;최형식
    • 제어로봇시스템학회논문지
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    • 제11권8호
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    • pp.726-732
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    • 2005
  • This paper proposes an autolanding guidance and control algorithm with the lateral guidance law. This algorithm is basically formulated and designed in feedback linearization based on singular perturbation. Main features of this algorithm are two facts. One of those is that when a certain situation happens that airplane must realign to the runway suddenly assigned due to unexpected environment change around the landing site, the heading guidance in this algorithm is very valuable, and the other is the fact that the inner loop control of this algorithm is able to be designed directly based on the Handling Quality Requirements that most flight control systems must be satisfied with. To illustrate the potential of this algorithm, 6-DOF nonlinear simulation based on the nonlinear airplane model shown in Ref.[11] is carried out. The simulation results showed that the altitude response to the given landing trajectory is accurate, and the airplane heading alignment to the assigned runway from the lateral deviation is successful. It is noted that this algorithm is also applicable to unmanned aerial vehicle, which can be retrieved in autolanding technique, where the runway far retrieving the vehicle is in any direction for example at war field.

항공기의 고도, 속도 및 깊은 실속의 회복을 위한 자동회복장치 설계 및 검증에 관한 연구 (A Study on the Design and Validation of Automatic Pitch Rocker System for Altitude, Speed and Deep Stall Recovery)

  • 김종섭
    • 제어로봇시스템학회논문지
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    • 제15권2호
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    • pp.240-248
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    • 2009
  • Modem version of supersonic jet fighter aircraft must have been guaranteed appropriate controllability and stability in HAoA(High Angle of Attack). The HAoA flight control law have two parts, one is control law of departure prevention and the other is control law of departure recovery support. The control laws of departure prevention for advanced jet trainer consist of HAoA limiter, roll command limiter and rudder fader. The control laws of departure recovery support are consist of yaw-rate limiter and MPO(Manual Pitch Override) mode. The guideline of pitch rocking using MPO mode is simple, but operating skill of pitch rocking is very difficult by the pilot with inexperience of departure situation. Therefore, automatic deep stall recovery system is necessary. The system called the "Automatic Pitch Rocker System" or APRS, provided a pilot initiated automatic maneuver capable of an aircraft recoveries in situations of deep stall, speed and altitude. This paper addresses the design and validation for APRS to recovery of an deep stall without manual pitch rocking by the pilot. Also, this system is designed to recovery of speed, attitude and altitude after deep stall recovery using ATCS (Automatic Thrust Control System) and autopilot. Finally, this system is verified by real-time pilot evaluation using HQS (Handling Quality Simulator).