• Title/Summary/Keyword: 진입시퀀스

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The Compositions of Approaching Sequence in Exterior Space of Tadao Ando′s Works (안도 타다오 건축의 외부공간에 나타난 진입시퀀스의 구성방식)

  • 문정민;안우진;고성룡
    • Korean Institute of Interior Design Journal
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    • no.29
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    • pp.27-34
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    • 2001
  • The concept of homogeneous space which was made in during the modern architecture was criticize for making our circumstances uniformly. The difference of place disappeared. The concept of place, however, has been watching in Contemporary Architecture. A basis for the concept of place is 'movement in space'through the sense of the body. Thus, architectural methods for experiencing place are composing the sequence through the continuous time. It is important that the composition of sequences in place makes the spatial experiences with harmonies of architecture and environments in exterior space for people who enter the building. Tadao Ando makes place in terms of experiencing body. Compositions of sequence in his works are expressed very well at the approaching stages in the process of exterior space. This stud is to survey the compositions of approaching sequence in Tadao Ando's Works.

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Design of Interrogator for Airspace Surveillance in Multilateration Systems (항공용 다변측정 감시시스템 적용을 위한 질문기 설계)

  • Koh, Young-Mok;Kim, Su-Hong
    • Journal of Advanced Navigation Technology
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    • v.19 no.2
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    • pp.108-115
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    • 2015
  • Multilateration systems are used to provide the position of aircraft in flight or on airport runways. In the multilateration systems, the interrogator is an important transmitter that used to interrogate the airplanes with appropriately scenario in surveillance airspace. Whisper-Shout interrogation sequence, which is one of the key functions of the interrogator, can control airport traffic density when intruder airplanes are coming into the surveillance airspace. Therefore collision chance between airplanes could be reduced and also get highly accurate location of incoming airplane in multilateration systems. In this paper, we developed the interrogator that allows it to transmit Mode A/C and Mode S interrogations which is similar to existing secondary surveillance radar. With appropriately controlled Whisper-Shout sequence in the interrogator, the multilateration systems can avoid synchronous garbling and FRUIT phenomenons caused by receiving multiple responses from a number of airplanes.

Opcode category sequence feature and machine learning for analyzing IoT malware (IoT 악성코드 분석을 위한 op 코드 카테고리 시퀀스 특징과 기계학습 알고리즘 활용)

  • Mun, Sunghyun;Kim, Youngho;Kim, Donghoon;Hwang, Doosung
    • Proceedings of the Korea Information Processing Society Conference
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    • 2021.11a
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    • pp.914-917
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    • 2021
  • IoT 기기는 취약한 아이디와 비밀번호 사용, 저사양 하드웨어 등 보안 취약점으로 인해 사이버 공격 진입점으로 이용되고 있다. 본 논문은 IoT 악성코드를 탐지하기 위한 op 코드 카테고리 기반 특징 표현을 제안한다. Op 코드의 기능별 분류 정보를 이용해서 n-gram 특징과 엔트로피 히스토그램 특징을 추출하고 IoT 악성코드 탐지를 위한 기계학습 모델 평가를 수행한다. IoT 악성코드는 기능 개선과 추가를 통해 진화하였으나 기계학습 모델은 훈련 데이터에 포함되지 않은 진화된 IoT 악성 코드에 대한 예측 성능이 우수하였다. 또한 특징 시각화를 이용해서 악성코드의 비교 탐지가 가능하다.

Introduction to Chang'e-3 and Analysis of Estimated Mission Trajectory (창어 3호 개요 및 임무궤적 추정결과 분석)

  • Choi, Su-Jin;Lee, Donghun;Bae, Jonghee;Rew, Dong-Young;Ju, Gwanghyeok;Sim, Eun-Sup
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.43 no.11
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    • pp.984-997
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    • 2015
  • Chang'e-3 consisting of a lunar lander and exploration rover was launched on December 1, 2013 aboard a Long March 3B rocket flying from Xichang space launch center. Chang'e-3 was inserted into the lunar orbit after about a 5-day transit to the Moon and landed on the targeted landing site after orbiting around the Moon for 8 days. The successful landing of the Chang'e-3 gives a lot of help to analyze the future needs of the subsystem technologies and to figure out the trajectory from launch to lunar landing as well as operation sequences in the development of Korean lunar exploration is scheduled. Therefore, the configuration and analysis of overall mission of Chang'e-3 is performed based on the public information from the press and website. As a result, overall mission trajectory is reconstructed by solving boundary condition and then estimating control variable. Visibility status and eclipse status also analyzes so communication and power charge condition is as good as to operate lunar lander. Mass budget of the lander is derived using ${\Delta}V$ according to specific impulse.