• Title/Summary/Keyword: Resizing

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A Study on H.264 Video Upsampling fitting to Display Screen (출력 화면에 적합한 H.264 비디오의 확대에 관한 연구)

  • Kwak, Nae-Joung;Kwon, Dong-Jin;Ryu, Sung-Pil
    • Proceedings of the Korea Contents Association Conference
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    • 2006.11a
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    • pp.520-523
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    • 2006
  • Lately, development of multimedia industry has multimedia data serviced through various wire wireless communicating environment. These multimedia data is displayed on the device of various sizes such as mobile telephone, PDA, notebook, PC. Therefore, there has needed to resize multimedia data appropriate to the screen size of user's display device. In this paper, we propose the method to resizing H.264 videos sequence fitting to the screen size of user's display device. The existing most methods reduce the size of video sequence, but this paper proposes the upsampling method. The results show the proposed method upsamples video sequences without blocking effects.

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FLOW CONTROL OF SMART UAV AIRFOIL USING SYNTHETIC JET (Synthetic jet을 이용한 스마트 무인기 익형 주위의 유동 제어)

  • Kim, Min-Hee;Kim, Sang-Hoon;Kim, Woo-Re;Kim, Chong-Am;Kim, Yu-Shin
    • 한국전산유체공학회:학술대회논문집
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    • 2009.04a
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    • pp.43-50
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    • 2009
  • In order to reduce the download around Smart UAV(SUAV) at hovering and transition mode, flow control using synthetic jet has been performed. Many of the complex tilt rotor flow features are captured including wing leading and trailing edge separation, and the large region of separated flow beneath the wing. First, in order to control the trailing edge separation, synthetic jet is located at 30, 95% of flap chord length. The flow control using synthetic jet on flap shows that stall characteristics depending on several mode can be improved through separation vortices resizing. Also, a flap jet and a 0.01c jet which control the separation efficiently are applied at the same time at each test case because controlling the leading edge separation is essential for download reduction. As a result, time averaged download is reduced about 18% comparing with no control case at hovering mode and 48% at transition mode. These research results show that if flow control using leading edge jet and trailing edge jet is used effectively to the SUAV in overall flight mode, flight performance and stability can be improved.

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Development of Image resizing algorithm based Human Visual System using DCT block (DCT블록을 이용한 인간 시각시스템 기반의 영상 리사이징 알고리즘 개발)

  • Yang, Dae-Gyu;Jeong, Sang-Hyeon;Seo, Tae-Seok
    • Proceedings of the Korean Society of Broadcast Engineers Conference
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    • 2008.11a
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    • pp.199-202
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    • 2008
  • 고객의 통신 니즈가 다양해지고 통신 인프라가 대용량, 고속화 되고 단말이 지능화됨에 따라 이를 기반으로 IPTV의 셋탑, 컴퓨터 모니터, 이동통신 핸드폰이 이르기 까지 다양한 화면 사이즈의 단말을 통하여 서비스를 제공하고 있다. 이를 위해 원영상을 화면의 크기에 적합하게 크기를 변환하는 영상 리사이징 기술을 이용하게 되며, 그 방식은 DCT 방식과 공간 방식으로 나눌 수 있다. DCT방식은 원영상의 고주파 영역의 조정하여 크기를 변화하는 방식으로 열화는 최소화되나 DCT 변환을 위한 계산량이 많고 고정 크기 블록을 사용하므로 유연성이 떨어진다. 공간영역은 객관적인 평가에서 품질이 열화되더라도 시각적으로 눈에 민감한 영역의 변화를 최소화하는 것이다. 본 논문은 인간시각시스템을 기반으로 눈의 민간도가 높은 망막 이심율이 작은 영역에서는 DCT블록의 크기를 변화를 최소화시키고 망막이심율이 큰 영역에서는 블록의 변화를 크게 하는 가변 블록방식을 제안한다. 이를 통해 우수한 영상 품질을 확보하면서도 시각적으로 뛰어난 리사이징 영상을 얻을 수 있다.

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MPEG-2 Decoder with Down-sampling for Fast Transcoding (고속 압축변환기를 위한 MPEG-2 복호기)

  • Oh, Seung-Kyun;Park, Hyun-Wook
    • Journal of the Institute of Electronics Engineers of Korea SP
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    • v.39 no.6
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    • pp.664-671
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    • 2002
  • 고속으로 압축변환을 하기 위해 DCT(Discrete Cosine Transform) 영역에서 영상의 해상도를 줄이는 MPEG-2 복호기를 제안한다. 제안하는 복호기는 움직임 보상을 하기 전에 DCT 영역에서 영상의 해상도를 줄이며 해상도가 줄어든 영상에 대해서 DCT 영역에서 움직임 보상을 수행한다. 본래 해상도의 영상 (N${\times}$CN)에서는 1/2화소 정밀도의 움직임 보상을 해야 하지만 해상도가 반으로 줄어든 영상(N/2${\times}$N/2)에 대해서는 1/4화소 정밀도의 움직임 보상을 수행해야 한다. 하지만 해상도가 줄어든 영상에 대해 1/4화소 정밀도의 움직임 보상을 수행하면 영상이 흐릿해지는 현상이 발생할 수 있다. 본 논문에서는 해상도를 줄인 영상에 대해 계산시간 뿐만 아니라 DCT 영역에서의 움직임 보상 시에 발생 할 수 있는 흐려짐도 줄일 수 있는 방법을 제안한다. 실험 결과는 제안한 방법이 높은 해상도의 영상을 낮은 해상도의 영상으로 효율적으로 복호할 수 있는 알고리즘이라는 것을 보여준다.

A Visual Enhancement of Web Content Adaptation for Mobile Devices (무선 단말기를 위한 웹 콘텐츠 적응의 시각적인 개선)

  • Kim, Won-Seop;Chai, Young-Joon;Kim, Tae-Yong
    • Journal of Korea Multimedia Society
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    • v.10 no.10
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    • pp.1229-1239
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    • 2007
  • In conversion of web pages for mobile devices, since existing web conversion systems eliminate unnecessary objects indiscriminately or only convert the layout of a page, the original intention of a web designer is spoiled. In spite of great advances in device technology, there still remain the problems of limited display sire and insufficient CPU power. In this paper, we propose an adaptation method that minimizes the loss of information and preserves the original intention of a web designer from the visual aspect. In image conversion, the proposed method extracts meaningful information from the background against conventional resizing methods, and performs layout-based conversion for the arrangement of image components. Experimental results show the efficiency of the method on the accuracy and the usability in comparison with existing methods.

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Wind Induced Vibration Design for High-rise buildings through Control of Natural Period (주기 조절을 이용한 고층 건물의 풍응답 조절 설계)

  • 김지은;차성희;서지현;박효선
    • Proceedings of the Computational Structural Engineering Institute Conference
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    • 2004.10a
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    • pp.43-51
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    • 2004
  • As the slenderness ratio of a high-rise building increases, the lateral load resisting system for the building is more often determined by serviceability design criteria. In serviceability design, the maximum drift and the level of vibration are controlled not to exceed the design criteria. Even though many drift method have been developed in various forms, no practical design method for wind induced vibration has been developed so far. Structural engineers rely upon heuristic or experience in designing wind induced vibration. Development of practical design method for wind induced vibration is required. Generally, wind induced acceleration responses are depending on several variables such as the weight density of a building, damping ratio, the natural period, and etc.. All parameters except the natural period or frequency are usually out of reach for structural engineers, then the wind acceleration response may be proportioned to the natural period. Therefore, in this paper, a wind induced vibration design method based on frequency control technique for high-rise is proposed. The method is applied to vibration design of a 25-story office building for performance evaluation.

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Quantitative Lateral Drift Control of RC Tall Frameworks using Dynamic Displacement Sensitivity Analysis (동적 변위민감도 해석을 이용한 고층 RC 골조구조물의 정량적인 횡변위 제어 방안)

  • Lee, Han-Joo;Kim, Ho-Soo
    • Journal of Korean Association for Spatial Structures
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    • v.6 no.3 s.21
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    • pp.103-110
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    • 2006
  • This study presents a technique to control quantitatively lateral drift of RC tall frameworks subject to lateral loads. To this end, lateral drift constraints are established by introducing approximation concept that preserves the generality of the mathematical programming and can efficiently solve large scale problems. Also the relationships of sectional properties are established to reduce the number of design variables and resizing technique of member is developed under the 'constant-shape' assumption. Specifically, the methodology of dynamic displacement sensitivity analysis is developed to formulate the approximated lateral displacement constraints. Three types of 10 and 50 story RC framework models are considered to illustrate the features of dynamic stiffness-based optimal design technique proposed in this study.

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A Study on Stiffness-based Optimal Design of Tall Plane Frameworks using Composite Member (합성부재를 이용한 고층평면골조의 강성최적설계에 관한 연구)

  • Kim, Ho-Soo;Lee, Han-Joo
    • Journal of Korean Association for Spatial Structures
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    • v.4 no.3 s.13
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    • pp.77-84
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    • 2004
  • This study presents an effective stiffness-based optimal technique to control quantitatively lateral drift for tall frameworks using composit member subject to lateral loads. To this end, displacement sensitivity depending on behavior characteristics of tall frameworks is established and approximation concept that preserves the generality of the mathematical programming and can efficiently solve large scale problems is introduced. Specifically, under the 'constant-shape' assumption, resizing techniqe of composite member is developed. Two types of 50 story frameworks are presented to illustrate the features of the quantitative lateral drift control technique proposed in this study.

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A Thumbnail Extraction Algorithm for DMB (DMB를 위한 요약영상 추출 알고리듬)

  • Kwon, Yong-Kwang;Won, Chee-Sun
    • Journal of Broadcast Engineering
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    • v.12 no.5
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    • pp.525-534
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    • 2007
  • H.264/AVC for DMB is the most advanced video compression standard which provides a high compression rate and a video quality by adopting new technologies. However, these new technologies prevent us from applying some conventional algorithms directly to the H.264/AVC compression domain. For example, we need to study new image resizing schemes in the compressed bit-stream. So, in this paper, we propose a new thumbnail extraction method which can be applied to H.264. The proposed method shows that it can extract a 1/16 size thumbnail video, saving the operation time up to 50% to 70%.

SEPARATION CONTROL MECHANISM USING SYNTHETIC JET ON AIRFOIL (익형에서의 synthetic jet을 이용한 박리제어 mechanism)

  • Kim, S.H.;Kim, W.;Hong, W.;Kim, C.
    • 한국전산유체공학회:학술대회논문집
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    • 2007.10a
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    • pp.60-66
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    • 2007
  • Separation control has been performed using synthetic jets on airfoil at high angle of attack. Computed results demonstrated that stall characteristics and control surface performance could be substantially improved by resizing separation vortices. It was observed that the actual flow control mechanism and flow structure is fundamentally different depending on the range of synthetic jet frequency. For low frequency range, small vortices due to synthetic jet penetrated to the large leading edge separation vortex, and as a result, the size of the leading edge vortex was remarkably reduced. For high frequency range, however, small vortex did not grow up enough to penetrate into the leading edge separation vortex. Instead, synthetic jet firmly attached the local flow and influenced the circulation of the virtual airfoil shape which is the combined shape of the main airfoil with the separation vortex. Theses results show the characteristic of unsteady flow of single synthetic jet. Beside, we researched on multi-array synthetic jet to obtain applicable synthetic jet velocity. Multi-location synthetic jet is proposed to eliminate small vortex on suction surface of airfoil. With the results, we concluded that the flow around airfoil is stable by high frequency synthetic jet with elimination of small vortex and confirmation of stable flow. Moreover, performance of multi-array/multi-location synthetic jet can be improved by changing phase angle of multi-location synthetic jet.

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