• Title/Summary/Keyword: O-2A 항공기

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Aircraft Deformation Measurement using Industrial Photogrammetry (산업사진측량기법을 이용한 항공기 변형 측정)

  • Lee Jae-Kee;Jung Sung-Heuk;Yu Jung-Hum
    • Journal of the Korean Society of Surveying, Geodesy, Photogrammetry and Cartography
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    • v.23 no.2
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    • pp.205-210
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    • 2005
  • As industries developed, industrial goods have got more precise. It led producers to feel like having a way to confirm whether the goods are good enough for the needs of consumers or not. Because of that, producers got interested in industrial photogrammetry that can get accurate data quickly with non-confect method. therefore, this study was examined by photographing an O-2A aircraft which was a large and precise one to check the application of Industrial photogrammetry. To measure the aircraft, the check points, that was attached to it was used as it was not possible to measure the aircraft by its design. The experiment was carried out in three parts considering arrangement of the check points and measured with Pro-spot to check any deformation of its external form. As a result, this study enables us to conferm a state of the aircraft alignment promptly and to provide accurate data for producers, which helps them to make a decision.

Design of Approximate Feedback Controller for Two-Time-Scale Aircraft Dynamics (양시등급 항공기 동력학의 근사 궤환 제어기 설계)

  • Shim, Kyu-Hong;Sawan, M.E.;Hong, Sung-Kyung
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.32 no.5
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    • pp.58-64
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    • 2004
  • A new method to obtain approximate solutions by placing the only poles of the slow subsystem for the two-time-scale aircraft dynamic systems. The two kinds of approximate solutions are obtained by a matrix block diagonalization. One is called the uncorrected solution, and the other is called the corrected solution. The former has an error of $O({\varepsilon})$, and the latter has an error of $O({\varepsilon}^2)$. Of course, both solutions are robust enough even though they are reduced solutions. The excellence of the proposed method is illustrated by an numerical example of an aircraft longitudinal dynamics.

Precision Measurement for Aircraft Alignment using Industrial Photogrammetry (산업사진측량을 이용한 항공기 얼라인먼트 정밀측정)

  • Jung, Sung-Heuk;Lee, Jae-Kee
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.33 no.6
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    • pp.57-63
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    • 2005
  • According to increasing of demand for high accurate and quick measuring technology, they became to interest in industrial photogrammetry that can satisfy with this needs. This study is examined O-2A aircraft to check the application of Industrial Photogrammetry technology. To measure the aircraft alignment, the check points marked on it were used without exact aircraft design data. And to check any deformation of its external original feature, Pro-spot system has been used.

Effects of Flight Conditions on IR Signature from Aircraft Exhaust Plume (비행조건에 따른 항공기 배기플룸의 IR 신호 특성)

  • Go, Gun-Yung;Kim, Man-Young;Baek, Seung-Wook
    • Journal of the Korean Society of Propulsion Engineers
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    • v.16 no.5
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    • pp.58-66
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    • 2012
  • The IR signature and radiative base heating from an aircraft plume have been important factors for aircraft survivability in modern battle fields. In order to enhance the aircraft survivability and reduce the base heating, infrared signatures emitted from an aircraft exhaust plume should be determined. In this work, therefore, IR signatures and radiative base heating characteristics are examined in the plume exhausted from the aircraft with operating at altitude of 5 km in M=0.9 and 1.6, respectively. As a result, it is found that the particular wavelength IR signature has high spectral characteristics because of $H_2O$ and $CO_2$ gases in the plume, and the radiative heat flux coming into the base plane increases with higher Mach number and shorter distance.

Effects of Flight Conditions on IR Signature from Aircraft Exhaust Plume (비행조건에 따른 항공기 배기플룸의 IR 신호 특성)

  • Go, Gun-Yung;Kim, Man-Young;Baek, Seung-Wook
    • Proceedings of the Korean Society of Propulsion Engineers Conference
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    • 2012.05a
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    • pp.282-289
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    • 2012
  • The IR Signature and radiative base heating from an aircraft plume have been important factors for aircraft survivability in modern battle fields. In order to enhance the aircraft survivability and reduce the base heating, infrared signatures emitted from an aircraft exhaust plume should be determined. In this work, therefore, IR signatures and radiative base heating characteristics are examined in the plume exhausted from the aircraft with operating at altitude of 5km in M=0.9 and 1.6, respectively. As a result, it is found that the particular wavelength IR signature has high spectral characteristics because of $H_2O$ and $CO_2$ gases in the plume, and the radiative heat flux coming into the base plane increases with higher Mach number and shorter distance.

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균일막 형성을 위한 항공기 부품용 타이타늄의 양극산화 최적 공정

  • Lee, Da-Yeong;Han, A-Yeong;Jeong, Na-Gyeom;Choe, Jin-Seop
    • Proceedings of the Korean Institute of Surface Engineering Conference
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    • 2018.06a
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    • pp.66.2-66.2
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    • 2018
  • 금속의 양극산화 공정(anodizing)은 전해질 내 금속에 인위적으로 전위를 가해 금속 표면에 얇은 산화막(oxide layer)을 형성하여 금속의 내식성, 내마모성을 증가시키는 공정이다. 타이타늄은 가볍고 단단하여 산업분야에 유용하게 사용되며 이와 같은 양극산화 공정을 통해 내식성, 내마모성을 크게 높일 수 있다. 본 연구에서는 항공기 부품용 타이타늄의 최적 양극산화 조건을 찾기 위해 전압의 파형, 전해액의 조성에 따라 양극산화 실험을 진행하였다. SEM, AFM, EDS, 분광측색계, 색채색차계 등을 이용하여 각 조건에 해당하는 타이타늄의 산화막($Tio_2$)의 두께, crack 형태, pore 형태, 균일도, 표면 조도, 내전압, 색 수치를 분석하였다. 그 결과 전압 DC 140 V, 주성분이 KOH $Na_3PO_4{\cdot}12H_2O$인 전해액으로 이루어진 양극산화 조건에서 가장 균일하고 색 재현성이 우수한 타이타늄의 산화막($Tio_2$)을 형성하였다.

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Design of Control Mixer for 40% Scaled Smart UAV (스마트무인기 축소모형의 조종면 혼합기 설계)

  • Gang, Yeong-Sin;Park, Beom-Jin;Yu, Chang-Seon
    • Aerospace Engineering and Technology
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    • v.5 no.2
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    • pp.240-247
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    • 2006
  • Tilt rotor aircraft is a multi-configuration airplane which has three independent flight modes; helicopter, conversion, and aiplane. The control surface mixer resign is reqctired to generate and distribute efficient control forces and moments in each flight mode. In the conversion mode, the thrust vector is changed from helicopter mode to airplane, therefore the thrust vector makes undesired forces and moments which affect on pitch, roll and yaw dynamics. This paper describes the design results of control surface mixer design which minimize the undesired forces and moments due to nacelles tilting angle change for 4O% scaled model.

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Measurement of Aircraft using Industrial Photogrammetry (산업사진측량에 의한 항공기 측정)

  • 유정흠;정성혁;함창학;이재기
    • Proceedings of the Korean Society of Surveying, Geodesy, Photogrammetry, and Cartography Conference
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    • 2004.11a
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    • pp.223-228
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    • 2004
  • As industries developed, industrial goods have got bigger and more precise. It led producers to feel like having a way to confirm whether the goods are good enough for the needs of consumers or not. Because of that, producers got interested in industrial photogrammetry that can get accurate data quickly without coming cotact with customers directly. Based on the need, this study is examined by photographing an O-2A aircraft which is a large and precise one to check the application of Industrial Photogrammetry.

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Fabrication and Resistance Characteristics of Smart Paint for Temperature Sensor (온도 센서를 위한 스마트 페인트 제작 및 저항 특성)

  • Ahn, Ju-Hun;Lee, Chang-Yull
    • Journal of Aerospace System Engineering
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    • v.13 no.2
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    • pp.43-50
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    • 2019
  • Satellite and aircraft components are greatly affected by the possibility for missions and safety due to temperature effects. In the field of fuel cells, research is actively carried out for UAV. For the efficiency and stability of the fuel cells, the temperature for operations must be confirmed. In this paper, a smart paint was fabricated with $BaTiO_3$ and $SrTiO_3$ ceramics in order to take advantage of the rapid characteristics of the PTC thermistor, which is the resistance changes abruptly above the Curie point. A coating agent was prepared to prevent the paint from peeling off the samples and the coated models were checked for resistance changes. Moreover, the resistance change of the $BaTiO_3$ and $SrTiO_3$ with temperature conditions was measured before and after coating.

A Survey on the Long-range Transport of Sulfur Compounds by Aircraft Measurement over the Yellow Sea in 1998 (황해상공에서의 항공기관측에 의한 황화합물 장거리이동 특징에 대한 조사)

  • 김병곤;안준영;김종호;박철진;한진석;나진균;최양일
    • Journal of Korean Society for Atmospheric Environment
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    • v.15 no.6
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    • pp.713-725
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    • 1999
  • Air pollutants($SO_2$, NOx, $O_3$ and aerosol number) were measured using an aircraft to investigate the characteristical features of long-range transport of sulfur compounds over the Yellow Sea for the periods of 26~27 April and 7~10 November in 1998. The mean $SO_2$ concentrations of April 26th~27th and November 7th~10th flight were 0.6~1.8 ppb and 0.5~8.3 ppb, respectively, and the sulfur transport was largely limited to the atmospheric boundary layer. Especially, $SO_2$ increased up to 8.3 ppb altogether with the increase of particle number concentraton especially on November 8, 1998. In addition, $O_3$ was remarkably decreased against the increase of $SO_2$and particle number concentrations. This enhanced $SO_2$ concentration occurred in the low level westerlies in association with the anticyclonic flow over Southern China and the cyclonic circulation over Manchuria. Aerosol analyses at Taean site also showed that sulfate concentration increased 2~3 times higher than those of another sampling days, which could suggest possible interactions between aerosol particels and tropospheric ozone. A rigorous evaluation will be possible after the more intensive measurements and quantitative analyses with detailed chemistry model including the postulated heterogeneous mechanism.

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