• Title/Summary/Keyword: Space division

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A Study on Space Arrangement and Interior Space Division of Superyachts (수퍼요트의 공간배치와 실내공간구획에 관한 연구)

  • Lee, Han-Seok;Byun, Lyang-Soun
    • Korean Institute of Interior Design Journal
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    • v.16 no.6
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    • pp.224-231
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    • 2007
  • Superyachts are passenger vessels whose hull exceeds 24m. They are a kind of luxurious leisure ships. Interior designers can contribute in the field of space design of superyachts. This study is intended to investigate the space elements and their organization of superyachts for putting the base of superyachts interior design. Especially it is focused on the interior space division by structural elements such as the watertight bulkheads and decks. In this study we analyze general arrangements, floor plans of decks, of 31 superyachts and extract space elements and their disposition in three dimension. On the basis of the space arrangement we classify the types of space organization of superyachts. And then we inquire the interior space division of superyachts, which is characterized by the structural elements of the ship. The watertight compartments made by the bulkheads and decks have a great effect on interior space design in super yachts. The results of this study are summed up as follows: At first, the small-size superyacht has 3 decks and the midium or large-size superyachts has 4decks. Secondly, depending on the number of decks the superyachts has several typical patterns of space organization. Thirdly, in general there are 5-6 watertight compartments on a deck depending on the superyachts scale. Finally, there are distinct separation between the passenger's movement and the crew's movement on the ship.

A Study on the Space Planning and Formal Design of Nursing Lab (대학 간호학 실습실의 공간구성 및 형태계획에 관한 연구)

  • Lee, Joo-Hye
    • Proceedings of the Korean Institute of Interior Design Conference
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    • 2007.05a
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    • pp.67-70
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    • 2007
  • The meaning of the space planning which has from modern interior space has played important role, space composition planning itself is the concept creation tool as well as the unique expression sphere in field of interior space far away from fixed idea relevant to the existing space which was only simple division or secondary element in design. Thus, this current work expresses that the space-Function is related with space-division as well as basic designed-conceptual work process including the space is formed. Furthermore, through the side-composition with form, it activates the various space aspect perceptually, which created the visual environment in using lightning, reflection of glass and penetrated nature etc. The keyword on elevation design concept is as like various aspects, third dimension, non-materiality and symbolical meaning. In addition, it provides the color space equipped with functionality and artistry capable to arouse the diverse sensual capacity to space users on default of image language.

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40.8 MHz coherent scatter ionospheric radar observations of E- and F-region field aligned irregularities over Korea

  • Yang, Tae-Yong;Kwak, Young-Sil;Lee, Jae-Jin;Choi, Seong-Hwan;Hwang, Jung-A;Park, Young-Deuk
    • The Bulletin of The Korean Astronomical Society
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    • v.36 no.2
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    • pp.81.1-81.1
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    • 2011
  • The new coherent scatter ionospheric radar has been operating at Gyerong city ($36.18^{\circ}N$, $127.14^{\circ}E$, dip lat $26.7^{\circ}N$), South Korea. This VHF radar is consisted of 24 Yagi antennas having 5 elements and observes the E- and F-region field-aligned irregularities (FAIs) in a single frequency of 40.8 MHz with a peak power of 24 kW. We present the first results of the E- and F-region FAIs over Korea by using the new VHF coherent scatter ionospheric radar. The morphological and echo characteristics are studied in terms of their echo strength, Doppler velocity and also by spectral width values. From the continuous observations from December 2009, we found ionospheric E- and F-region FAIs appeared frequently. The most interesting and striking observations for E region are occurrence of daytime E-region irregularities and strong Quasi-Periodic (QP) echoes at nighttime. And for F region, strong post-sunset and pre-sunrise FAIs appeared frequently. The VHF radar observations over Korea are discussed in the light of current understanding of mid-latitude E- and F-region FAIs.

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Digital Image Simulation of Electro-Optical Camera(EOC) on KOMPSAT-1

  • Shim, Hyung-Sik;Yong, Sang-Soo;Heo, Haeng-Pal;Lee, Seung-Hoon;Oh, Kyoung-Hwan;Paik, Hong-Yul
    • Proceedings of the KSRS Conference
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    • 1999.11a
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    • pp.349-354
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    • 1999
  • Electro-Optical Camera (EOC) is the main payload of the KOMPSAT-1 satellite to perform the mission of cartography that builds up a digital map of Korean territory including a digital terrain elevation map. This paper discusses the issues of the digital image simulation of EOC for the generation of EOC simulated scene as taken by EOC at 685km altitude on orbit. For the purpose, simulation work has been performed with the sensor models of EOC and the satellite platform motions models through image chain analysis from the illumination source (Sun) to a simulated image output in digital number. MODTRAN fur radiance calculation, MTF models of optics, detector and motions of EOC for system point spread function (PSF), and signal chain equations for digital number output are described. Several noise models of EOC are also considered. The final output is the EOC simulated image in digital number. The simulation technique can be used in several phase of a spaceborne electro-optical system development project, feasibility study phase, design, manufacturing, test phases, ground image processing phases, and so on.

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Development of a Dual-Circular Polarizer for the KVN Receivers

  • Chung, Moon-Hee;Je, Do-Heung;Han, Seog-Tae;Lee, Jung-Won
    • Journal of Astronomy and Space Sciences
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    • v.26 no.3
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    • pp.345-354
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    • 2009
  • A stepped septum polarizer has been designed and fabricated for the 43 GHz band KVN receiver system. The dual-circular polarizer converts left and right hand circularly polarized signals into linear polarizations in two separated rectangular waveguides. Measurements show that the performance of the designed septum polarizer covering 42-48 GHz frequency band is adequate to meet the requirement of KVN receivers. Especially, a polarizer for the KVN receiver of 85-95 GHz frequency band can be fabricated by scaling the dimensions of the septum polarizer developed in this paper.

Korea Pathfinder Lunar Orbiter (KPLO) Operation: From Design to Initial Results

  • Moon-Jin Jeon;Young-Ho Cho;Eunhyeuk Kim;Dong-Gyu Kim;Young-Joo Song;SeungBum Hong;Jonghee Bae;Jun Bang;Jo Ryeong Yim;Dae-Kwan Kim
    • Journal of Astronomy and Space Sciences
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    • v.41 no.1
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    • pp.43-60
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    • 2024
  • Korea Pathfinder Lunar Orbiter (KPLO) is South Korea's first space exploration mission, developed by the Korea Aerospace Research Institute. It aims to develop technologies for lunar exploration, explore lunar science, and test new technologies. KPLO was launched on August 5, 2022, by a Falcon-9 launch vehicle from cape canaveral space force station (CCSFS) in the United States and placed on a ballistic lunar transfer (BLT) trajectory. A total of four trajectory correction maneuvers were performed during the approximately 4.5-month trans-lunar cruise phase to reach the Moon. Starting with the first lunar orbit insertion (LOI) maneuver on December 16, the spacecraft performed a total of three maneuvers before arriving at the lunar mission orbit, at an altitude of 100 kilometers, on December 27, 2022. After entering lunar orbit, the commissioning phase validated the operation of the mission mode, in which the payload is oriented toward the center of the Moon. After completing about one month of commissioning, normal mission operations began, and each payload successfully performed its planned mission. All of the spacecraft operations that KPLO performs from launch to normal operations were designed through the system operations design process. This includes operations that are automatically initiated post-separation from the launch vehicle, as well as those in lunar transfer orbit and lunar mission orbit. Key operational procedures such as the spacecraft's initial checkout, trajectory correction maneuvers, LOI, and commissioning were developed during the early operation preparation phase. These procedures were executed effectively during both the early and normal operation phases. The successful execution of these operations confirms the robust verification of the system operation.

A Study on the Satisfaction and Demand of Housework Space in Apartment -Based on the division types of housework- (아파트 가사공간 만족도 및 요구도에 관한 연구 -가사분담유형을 중심으로-)

  • 윤재웅;한지영
    • Journal of the Korean housing association
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    • v.12 no.4
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    • pp.131-139
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    • 2001
  • The purpose of this study is to find out conformable method of housework space planning as the division style of housework. For this purpose it is surveyed satisfaction and demand of housework space in apartment dwellers. The 785 data is collected from interviewing housewives through questionnaire designed for this study. The data were analyzed by using Frequencies, Mean, χ²-test, t-test, ANOVA, and MDS. The results of the study are as follows: (1) The division types of housework are ‘Homemaker’, ‘Partially to homemaker’, ‘Equally division’, ‘Regularity division’ and ‘Service using’. The ‘Homemaker’ and Partially to homemaker' were more than the others. (2) the homeworks were performed in various spaces. (3) The satisfaction and demand of housework space differed significantly according to style division of housework. The highest style is ‘Equally homemaker’, and the lowest style is ‘homemaker’.

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Geostationary Orbit Surveillance Using the Unscented Kalman Filter and the Analytical Orbit Model

  • Roh, Kyoung-Min;Park, Eun-Seo;Choi, Byung-Kyu
    • Journal of Astronomy and Space Sciences
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    • v.28 no.3
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    • pp.193-201
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    • 2011
  • A strategy for geostationary orbit (or geostationary earth orbit [GEO]) surveillance based on optical angular observations is presented in this study. For the dynamic model, precise analytical orbit model developed by Lee et al. (1997) is used to improve computation performance and the unscented Kalman filer (UKF) is applied as a real-time filtering method. The UKF is known to perform well under highly nonlinear conditions such as surveillance in this study. The strategy that combines the analytical orbit propagation model and the UKF is tested for various conditions like different level of initial error and different level of measurement noise. The dependencies on observation interval and number of ground station are also tested. The test results shows that the GEO orbit determination based on the UKF and the analytical orbit model can be applied to GEO orbit tracking and surveillance effectively.