• Title/Summary/Keyword: Design space exploration

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Exploration of Isovist Fields to Model 3D Visibility With Building Facade

  • Chang, Dong-Kuk;Park, Joo-Hee
    • Architectural research
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    • v.13 no.3
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    • pp.19-29
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    • 2011
  • Visibility of a space have been defined in several different ways: such as the axial line covering a convex space, a convex space defining the fattest shape in a space and an Isovist field formed by a field of vision at a given vantage point. Isovist fields are referred to as a descriptive medium to describe a movement by reviewing and analyzing geometric properties in them. Many descriptive methods for analysis of three-dimensional isovist are applied to analyzing the morphological properties in a 3D space more realistically. Although these models are regarded as a more advanced method for describing spatial properties, they have pros and cons such as complex mathematical calculations and somewhat arbitrary calibration in addition to huge consumption of memory space. These difficulties lead to the development of a three-dimensional visual accessibility model that explores the implication of building shape on the calculation of isovist fields drawn on a 2D plane. We propose a conceptual framework of how to measure the isovist field not as a 3D volume but as a combination of 2D plane on the ground with the 3D building shape of it's facade.

Preliminary Analysis on Launch Opportunities for Sun-Earth Lagrange Points Mission from NARO Space Center

  • Song, Young-Joo;Lee, Donghun
    • Journal of Astronomy and Space Sciences
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    • v.38 no.2
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    • pp.145-155
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    • 2021
  • In this work, preliminary launch opportunities from NARO Space Center to the Sun-Earth Lagrange point are analyzed. Among five different Sun-Earth Lagrange points, L1 and L2 points are selected as suitable candidates for, respectively, solar and astrophysics missions. With high fidelity dynamics models, the L1 and L2 point targeting problem is formulated regarding the location of NARO Space Center and relevant Target Interface Point (TIP) for each different launch date is derived including launch injection energy per unit mass (C3), Right ascension of the injection orbit Apoapsis Vector (RAV) and Declination of the injection orbit Apoapsis Vector (DAV). Potential launch periods to achieve L1 and L2 transfer trajectory are also investigated regarding coasting characteristics from NARO Space Center. The magnitude of the Lagrange Orbit Insertion (LOI) burn, as well as the Orbit Maintenance (OM) maneuver to maintain more than one year of mission orbit around the Lagrange points, is also derived as an example. Even the current work has been made under many assumptions as there are no specific mission goals currently defined yet, so results from the current work could be a good starting point to extend diversities of future Korean deep-space missions.

Path Tracking Controller Design and Simulation for Korean Lunar Lander Demonstrator

  • Yang, Sungwook;Son, Jongjun;Lee, Sangchul
    • International Journal of Aeronautical and Space Sciences
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    • v.16 no.1
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    • pp.102-109
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    • 2015
  • In Korea, Lunar exploration program has been prepared with the aim of launching in the 2020's. As a part of it, a lunar lander demonstrator was developed, which was the model for verifying the system such as structure, propulsion, and control system, before launching into the deep space. This paper deals with the path tracking performance of the lunar lander demonstrator with respect to the thruster controller based on Pulse Width Pulse Frequency Modulator (PWPFM) and Pulse Width Modulator (PWM). First, we derived equations of motion, considering the allocation of the thrusters, and designed the path tracking controller based on Euler angle. The signal generated from the path tracking controller is continuous, so PWPFM and PWM modulator are adopted for generating ON/OFF signal. Finally, MATLAB simulation is performed for evaluating the path tracking ability. We compared the path tracking performances of PWPFM and PWM based thrust controller, using performance measures such as the total impulse and the position error with respect to the desired path.

A Study on Education Example for Office Design (업무공간디자인 교육사례 연구)

  • Byun, Dae-Joong
    • Proceedings of the Korean Institute of Interior Design Conference
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    • 2005.05a
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    • pp.225-226
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    • 2005
  • In early 20th century, This study focus on exploration of a education for office design This class is focused on planning an office space. Selection of the right places, Setting a concept room plans, and such are studied along with systematically analyzing spaces. Applying concepts, interior plans, interior elements, color and selection of materials are introduced and developed into systematical plans. And the students produce efficiently a portfolio by complementing and/or developing the visual materials and readjusting all the concept of the accomplished assignments during this course that were presented visually by applying techniques of presentation leaned majoring in interior design, in an aesthetical and creative ways.

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Design Space Exploration of Many-Core Processors for Mobile Ultrasound Image Signal Processing (모바일 초음파 영상신호처리를 위한 매니코어 프로세서 디자인 공간 탐색)

  • Choi, Byong-Kook;Kim, Jong-Myon
    • Proceedings of the Korea Information Processing Society Conference
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    • 2011.04a
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    • pp.183-186
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    • 2011
  • 본 논문에서는 모바일 초음파(mobile ultrasound) 영상신호의 빔포밍 알고리즘에서 요구되는 고성능 및 저전력을 만족시키는 매니코어 프로세서에 대한 디자인 공간 탐색 방법을 소개한다. 매니코어 프로세서의 디자인 공간 탐색을 위해 매니코어의 각 프로세싱 엘리먼트(Processing Element, PE)당 초음파 영상신호 데이터의 수를 변화시키는 실험을 통해 실행시간, 에너지 효율 및 시스템 면적 효율을 측정하고, 측정된 결과를 바탕으로 최적의 매니코어 프로세서 구조를 선택하였다.

A Model-based Methodology for Application Specific Energy Efficient Data path Design Using FPGAs (FPGA에서 에너지 효율이 높은 데이터 경로 구성을 위한 계층적 설계 방법)

  • Jang Ju-Wook;Lee Mi-Sook;Mohanty Sumit;Choi Seonil;Prasanna Viktor K.
    • The KIPS Transactions:PartA
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    • v.12A no.5 s.95
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    • pp.451-460
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    • 2005
  • We present a methodology to design energy-efficient data paths using FPGAs. Our methodology integrates domain specific modeling, coarse-grained performance evaluation, design space exploration, and low-level simulation to understand the tradeoffs between energy, latency, and area. The domain specific modeling technique defines a high-level model by identifying various components and parameters specific to a domain that affect the system-wide energy dissipation. A domain is a family of architectures and corresponding algorithms for a given application kernel. The high-level model also consists of functions for estimating energy, latency, and area that facilitate tradeoff analysis. Design space exploration(DSE) analyzes the design space defined by the domain and selects a set of designs. Low-level simulations are used for accurate performance estimation for the designs selected by the DSE and also for final design selection We illustrate our methodology using a family of architectures and algorithms for matrix multiplication. The designs identified by our methodology demonstrate tradeoffs among energy, latency, and area. We compare our designs with a vendor specified matrix multiplication kernel to demonstrate the effectiveness of our methodology. To illustrate the effectiveness of our methodology, we used average power density(E/AT), energy/(area x latency), as themetric for comparison. For various problem sizes, designs obtained using our methodology are on average $25\%$ superior with respect to the E/AT performance metric, compared with the state-of-the-art designs by Xilinx. We also discuss the implementation of our methodology using the MILAN framework.

Overview of Fire Safety onboard International Space Station(ISS): Characteristics of Flame Ignition, Shape, Spread, and Extinction in Microgravity (국제우주정거장 화재안전 연구개괄: 마이크로중력화염의 특성(점화/형상/전파/소멸특성))

  • Park, Seul-Hyun;Hwang, Cheol-Hong
    • Journal of the Korean Society of Combustion
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    • v.17 no.4
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    • pp.21-29
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    • 2012
  • Due to a significant leap in the science and technology, the manned space exploration that has started with suborbital flights is now being expanded into the deep space. The space superpowers such as the U.S. and Russia have been making an effort to further develop the manned space technology. Among such technologies, the fire safety technology in microgravity has recolonized as one of the most critical factors that must be considered for the manned space mission design since the realistic fire broke out onboard the Mir station in 1997. In the present study, the flame characteristics such as flame ignition, shape, spread, and extinction that are critical to understand the fire behavior under microgravity conditions are described and discussed. The absence of buoyancy in microgravity dominates the mass transport driven by diffusiophoretic and thermophorectic fluxes (that are negligible in normal gravity) and influences the overall flame characteristics-flame ignition, shape, spread, and extinction. In addition, the cabin environments of the pressurized module (PM) including the oxygen concentration, ambient pressure, and ventilation flow(which are always coupled with microgravity condition during the ISS operation) are found to be the most important aspects in characterizing the fire behavior in microgravity.

A Study on Observation Type at the Process of Visual Understanding - Focused on the Lobby in the Public Space - (공간의 시각적 이해과정에 나타난 주시유형에 관한 연구 - 공공공간의 로비를 중심으로 -)

  • Kim, Jong-Ha;Cho, Eun-Kil;Ban, Young-Sun
    • Korean Institute of Interior Design Journal
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    • v.21 no.2
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    • pp.92-100
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    • 2012
  • This study was to examine the pattern of visual interpretation in the process of eye-tracking. I categorized the subjects' observation inclination for analysis so that I could find out which element the user observing the space concentrated and explored. First, for 2 minutes of observation, there occurred 171 times of eye-fixations and 9.8 times of observation frequency on average, which showed that the subject, through this observing fixation, spent 44.5% of the entire time performing the visual activity in order to acquire the "visual understanding" of the lobby-space. Second, I found out that there was a consistent observation type as the time passed. I could categorize the subjects observing the space into 6 concentrating types and 3 discontinuing ones of observation types, which category can be utilized as data for analyzing the subjects' characteristics at space-observation. Third, the type, which was so intensive as to get the visual understanding on the space, was mostly of the case that (1) the subject had a kind of high degree of observation type, exploring the space, again having high degree of the observation type [Type A], (2) the subject repeated the concentration from the early part to the latter [Type C], which can be considered to be the observation type generally shared. Fourth, in the case of observing the space, 45.8% of the subjects showed a high rate of concentration at the time of starting the observation and in less than two minutes. The subjects of type A can be considered to understand the space visually by distinctively repeating the concentration and exploration.

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Thermal Design and On-Orbit Thermal Analysis of 6U Nano-Satellite High Resolution Video and Image (HiREV) (6U급 초소형 위성 HiREV(High Resolution Video and Image)의 광학 카메라의 열 설계 및 궤도 열 해석)

  • Han-Seop Shin;Hae-Dong Kim
    • Journal of Space Technology and Applications
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    • v.3 no.3
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    • pp.257-279
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    • 2023
  • Korea Aerospace Research Institute has developed 6U Nano-Satellite high resolution video and image (HiREV) for the purpose of developing core technology for deep space exploration. The 6U HiREV Nano-Satellite has a mission of high-resolution image and video for earth observation, and the thermal pointing error between the lens and the camera module can occur due to the high temperature in camera module on mission mode. The thermal pointing error has a large effect on the resolution, so thermal design should solve it because the HiREV optical camera is developed based on commercial products that are the industrial level. So, when it operates in space, the thermal design is needed, because it has the best performance at room temperature. In this paper, three passive thermal designs were performed for the camera mission payload, and the thermal design was proved to be effective by performing on-orbit thermal analysis.

Expanded Characteristics of JUUN. J's Fashion Design (준지(JUUN. J) 패션 디자인에 나타난 확장의 특성)

  • Yoon Joo Park;Gee Yun Hwang;Younhee Lee
    • Journal of the Korea Fashion and Costume Design Association
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    • v.25 no.3
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    • pp.165-184
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    • 2023
  • The purpose of this study is to analyze the expanded characteristics that can be found in the fashion designs of JUUN. J. For the study, the concept and discourse related to theme expansion have been theoretically reviewed, and various types of expansive characteristics were derived by reviewing prior research related to the keyword expanded characteristics. Photo data required for the analysis were collected through the official website of JUUN. J and Vogue, a worldwide fashion magazine. The scope of the survey was limited to 983 photographs collected from 28 collections from 2009 S/S through 2022 F/W. The results are as follows. First, the expansion of the human body, which is achieved by adding an empty space between the body and the clothing or using various materials to express the volume of the body, is expressed through two different forms in the designs of JUUN. J. Second, the expansion of time expresses the combination of different timelines, the meeting of the past and present or awe toward the unpredictable future. Third, the expansion of style, which is expressed by reinterpreting existing costumes or styles, is a type of expansion' that appears individually in the fashion designs of JUUN J. Such expansion of style can be found in the military inspired designs. Fourth, the expansion of space, which diversifies our perception of space by re-recognizing the concept of space, was implemented into the works and designs of JUUN. J through the convergence of different cultural aspects. Fifth, the expansion of gender, which is expressed through the continuous exploration of the borders of gender and the delivery of social messages, has appeared in the works of JUUN J. in the form of genderless design.