• Title/Summary/Keyword: Flight Model

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Land Cover Classification with High Spatial Resolution Using Orthoimage and DSM Based on Fixed-Wing UAV

  • Kim, Gu Hyeok;Choi, Jae Wan
    • Journal of the Korean Society of Surveying, Geodesy, Photogrammetry and Cartography
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    • v.35 no.1
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    • pp.1-10
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    • 2017
  • An UAV (Unmanned Aerial Vehicle) is a flight system that is designed to conduct missions without a pilot. Compared to traditional airborne-based photogrammetry, UAV-based photogrammetry is inexpensive and can obtain high-spatial resolution data quickly. In this study, we aimed to classify the land cover using high-spatial resolution images obtained using a UAV. An RGB camera was used to obtain high-spatial resolution orthoimage. For accurate classification, multispectral image about same areas were obtained using a multispectral sensor. A DSM (Digital Surface Model) and a modified NDVI (Normalized Difference Vegetation Index) were generated using images obtained using the RGB camera and multispectral sensor. Pixel-based classification was performed for twelve classes by using the RF (Random Forest) method. The classification accuracy was evaluated based on the error matrix, and it was confirmed that the proposed method effectively classified the area compared to supervised classification using only the RGB image.

THE SELENE MISSION AND JAPANESE LUNAR EXPLORATION SCENARIO

  • NODA HIROTOMO;HANADA HIDEO;KAWANO NOBUYUKI;IWATA TAKAHIRO
    • Journal of The Korean Astronomical Society
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    • v.38 no.2
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    • pp.311-314
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    • 2005
  • We report the current status of Japanese lunar exploration SELENE (SELenological and ENgineering Explorer). As of the end of 2004, scientific instruments onboard the Main Orbiter are under final checkout before they are provided to the proto-flight-model (PFM) integration test. Also, we present the future perspectives of the lunar based instruments and facilities. 'In-situ Lunar Orientation Mea-surement (ILOM)' experiment measures the lunar rotation with high accuracy by tracking stars on the Moon with a small photo-zenith-tube type optical telescope. A basic idea of a radio telescope array of very low frequency range on the lunar far-side is also mentioned.

소형위성 기능시험 및 열주기 시험

  • Park, Jong-Oh;Choi, Jong-Yeon;Kwon, Jae-Wook;Youn, Young-Su;Cho, Seung-Won;Kim, Young-Youn;An, Jae-Chel;Choi, Seok-Won
    • Aerospace Engineering and Technology
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    • v.2 no.2
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    • pp.58-65
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    • 2003
  • KARI Electrical Test Team performed the SOH (State Of Health) test and Thermal Cycling test for small satellite of KOMPSAT-1 PFM at KARI SITC Highbay as per Storage plan every year, and verified that the system/subsystem units function installed on PFM were good without significant degradation causing from long-term storage. This paper describes the test items, test method, test procedure and selected test result data.

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Flutter Safety Analysis of a Composite Smart UAV with T-tail Configuration (T-형 꼬리날개를 갖는 복합재 스마트 무인기의 플러터 안전성 해석)

  • Kim, D.H.;Yang, Y.J.;Jung, S.U.;Kim, S.J.;Choi, S.C.;Kim, S.C.;Shin, J.W.
    • Journal of the Korean Society for Aviation and Aeronautics
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    • v.13 no.1
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    • pp.20-31
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    • 2005
  • In this study, subsonic flutter analyses have been conducted for a composite smart UAV with T-tail configuration at the critical flight condition. Detailed three-dimensional finite element model for dynamic analysis is constructed including its nonstructural elements corresponding to installed electronic equipments and fuels. Computational structural dynamics and aeroelastic techniques are conducted using MSC/NASTRAN and originally developed in-house codes. The results for fundamental vibration characteristics and flutter instabilities are presented and compared to each other for different fuel conditions.

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Satellite data validation system using RC helicopter

  • Honda, Yoshiaki;Kajiwara, Koji
    • Proceedings of the KSRS Conference
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    • 2002.10a
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    • pp.746-749
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    • 2002
  • This paper is introducing a radio control helicopter as a new platform of ground truth measurement. This helicopter is normally used for spraying an agricultural chemical. It can do pinpoint hovering and programing flight using DGPS etc., A spectrometer with dual port can measure ground surface and white reference plate at the same time. And it can also take digital images by digital camera. It is needed to collect ground reflectance information as satellite sensor footprint size for satellite data validation. Generally it is possible to get such ground reflectance by an airplane measurement. But it is high cost and not so easy to make a measurement by airplane. Developed validation system can provide such ground reflectance in low cost and easy.

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A Study on Effective Information Delivery System in Aviation Maintenance (효율적인 항공정비 정보전달 체계에 관한 연구)

  • Kim, Chun-Yong;Hwang, Hyoe-Jung;Kim, Chil-Young
    • Journal of the Korean Society for Aviation and Aeronautics
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    • v.18 no.2
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    • pp.46-53
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    • 2010
  • In the aspect of the nature of aircraft maintenance work on divisible tasks carried out by a wide range of operation and expertise, any information transmission problems will not only cause a threat to flight safety but also reduce productivity by keeping the team from fulfilling its mission of delivering aircraft with airworthiness. In this regard, this study firstly identify the current status of information of aircraft maintenance and factors disturbing information transmission. Then, this article also find out the level of information culture of the AMT(Aircraft Maintenance Technicians) and problems in using information. Finally, suggestions on the model of the positive information culture in a field of aircraft maintenance through efficient use of the information including safety will be followed.

Peptide C-terminal Sequence Analysis by MALDI-TOF MS Utilizing EDC Coupling with Br Signature

  • Shin, Man-Sup;Kim, Hie-Joon
    • Bulletin of the Korean Chemical Society
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    • v.32 no.4
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    • pp.1183-1186
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    • 2011
  • The unique Br signature was utilized for C-terminal amino acid sequencing of model peptides. C-terminal carboxyl group was selectively derivatized in peptides, containing side chain carboxyl group, using 1-ethyl-3-[3-dimethylaminopropyl]carbodiimide hydrochloride (EDC) and Br was introduced using 4-bromophenylhydrazine hydrochloride (BPH) in a one pot reaction. Matrix-assisted laser desorption/ionization (MALDI) time-of-flight (TOF) tandem mass spectra were obtained carrying the Br signature in the y-series ions. The Br signature facilitated C-terminal sequencing and discrimination of C-terminal carboxyl groups in the free acid and amide forms.

Development of CAD/CAM system for dieless CNC forming (Dieless CNC Forming 을 위한 CAD/CAM 시스템 개발)

  • 최동우;진영길;강재관;왕덕현
    • Proceedings of the Korean Society of Precision Engineering Conference
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    • 2004.10a
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    • pp.405-408
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    • 2004
  • The sheet parts are formed with dies conventionally. But this conventional forming process is not suited to small volume and varied production for the reason of high cost. For the solution of this problem, a new forming process, which is called CNC incremental sheet forming, is being introduced. This process can form sheet parts without die, and is very well suited to small volume and varied production in space flight and automobile. In this paper, dieless CNC forming system based on a machining center is developed. A special device to grasp and pull the blank sheet built in the machining center and tool path generation S/W from STL file of 3-D model are developed. Several sheet parts are incrementally formed to verify the effectiveness of the developed system.

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A Study of the Effects of Hard Landing on Aircraft Structure (Hard Landing이 항공기 구조물에 미치는 영향성 연구)

  • Oh, Yong-Kyu;Sim, Sang-Ki;Shin, Ki-Su
    • Journal of the Korea Institute of Military Science and Technology
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    • v.14 no.5
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    • pp.805-811
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    • 2011
  • Aircraft MLG and wing structures have been recognized as fatigue critical structures and exposed to the risk of fatigue crack initiation and propagation. Furthermore, these structures are frequently subjected to serious dynamic loading condition during a Hard Landing which may lead to their failure. Especially, structural integrity of MLG and wing components is decreased as the flight time increased because of the fatigue damage accumulated on the aircraft. In this study, the effects of Hard Landing on the MLG and wing components of aging aircraft were evaluated by using numerical approach. To achieve the aim, a finite element model has been developed and simulations were conducted by varying the landing conditions. As a result, it was revealed that the high stress concentration phenomenon was occurred at the lower Side Brace of MLG. Thereby, the intensified inspection for the lower Side Brace should be considered to prevent unexpected aircraft mishap.

e-Business Impacts on Distribution Channel in Airlines (항공사 유통경로에 대한 e-비즈니스 파급효과)

  • Yoon Duk Young;Lee Hwi Young;Kim Kee Woong;Yoon Moon-Gil
    • Korean Management Science Review
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    • v.22 no.1
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    • pp.149-165
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    • 2005
  • From the growth of internet technology, many e-commerce principles have been Introduced In airline industry. The computer reservation systems(CRS) has been considered as the first real-time business application and the earliest examples of e-commerce. in airlines, the early e-business activity was to build the web site for providing flight Information to customers. Recently, many airlines are expanding the capability of the web site for selling tickets on the web to make use of the cheaper distribution channel. In this paper, we focus on the impacts of airline e-business being implemented in airline distribution channels. Using the conjoint analysis, we suggest a model for estimating the change of market sales for each distribution channel. With the empirical survey, we can find some implications on the e-business strategy and the effective internet marketing tools for airlines.