• Title/Summary/Keyword: Technologies for Aerospace

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Survey on Visual Navigation Technology for Unmanned Systems (무인 시스템의 자율 주행을 위한 영상기반 항법기술 동향)

  • Kim, Hyoun-Jin;Seo, Hoseong;Kim, Pyojin;Lee, Chung-Keun
    • Journal of Advanced Navigation Technology
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    • v.19 no.2
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    • pp.133-139
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    • 2015
  • This paper surveys vision based autonomous navigation technologies for unmanned systems. Main branches of visual navigation technologies are visual servoing, visual odometry, and visual simultaneous localization and mapping (SLAM). Visual servoing provides velocity input which guides mobile system to desired pose. This input velocity is calculated from feature difference between desired image and acquired image. Visual odometry is the technology that estimates the relative pose between frames of consecutive image. This can improve the accuracy when compared with the exisiting dead-reckoning methods. Visual SLAM aims for constructing map of unknown environment and determining mobile system's location simultaneously, which is essential for operation of unmanned systems in unknown environments. The trend of visual navigation is grasped by examining foreign research cases related to visual navigation technology.

Review of Radio Frequency Identification and Wireless Technology for Structural Health Monitoring

  • Dhital, Dipesh;Chia, Chen Ciang;Lee, Jung-Ryul;Park, Chan-Yik
    • Journal of the Korean Society for Nondestructive Testing
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    • v.30 no.3
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    • pp.244-256
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    • 2010
  • Radio frequency identification(RFID) combined with wireless technology has good potential for structural health monitoring(SHM). We describe several advantages of RFID and wireless technologies for SHM, and review SHM examples with working principles, design and technical details for damage detection, heat exposure monitoring, force/strain sensing, and corrosion detection in concrete, steel, carbon fiber reinforced polymer(CFRP), and other materials. Various sensors combined with wireless communication are also discussed. These methodologies can be readily developed, implemented, and customized. There are some technical difficulties, but solutions are being addressed. Lastly, a surface acoustic wave-based RFID system is presented, and possible future trends of SHM based on RFID and wireless technology are presented.

Analysis of Supporting Function for Invigorating Aerospace Cluster focused on the case of Gyeongsangnam-do (항공산업 클러스터 활성화를 위한 지원 기능 분석 -경남을 중심으로-)

  • Han, Kwan-Hee;Jeong, Dong-Min;Ok, Ju-Seon;Jeon, Jeong-Hwan
    • The Journal of the Korea Contents Association
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    • v.14 no.4
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    • pp.314-324
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    • 2014
  • Aerospace industry is a combination of high technologies which has several characteristics such as product reliability, precision, light weight, and energy efficiency. Nowadays, each country is trying to invigorating knowledge and information sharing between the companies for the synergy effect of aerospace industry. However, the research and empirical analysis on the vitalization of aerospace industry cluster are insufficient. Therefore, this study aims to firstly classify the supporting functions of government for aerospace industry cluster into five types by analyzing existing literatures and status reports issued by government. Secondly, companies are surveyed on the five classified types of supporting functions by questionnaire. Questionnaire survey responded by 30 aerospace companies in Gyeongnam aerospace industry cluster are analyzed. Quantitative analysis methods were used for statistical analysis. Based on the analysis, improvement directions of government supporting functions are suggested. The results of this study is expected to help policy making for invigorating the aerospace industry cluster.

Research Activities on PGC Propulsion based on RDE, Part I: Basic Studies (RDE 기반 PGC 추진기관 연구 동향, Part I: 기초연구)

  • Kim, Jung-Min;Niyasdeen, Mohammed;Han, Hyung-Seok;Oh, Sejong;Choi, Jeong-Yeol
    • Journal of the Korean Society of Propulsion Engineers
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    • v.21 no.5
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    • pp.97-107
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    • 2017
  • Fluid dynamic constant volume combustion technology detonation has been paid attention as a "game-changing" technology to overcome the efficiency and performance limitation of the present constant pressure combustion systems. For the past several years, a number of experimental and CFD-based theoretical studies have been conducted for the basic operation tests of RDE's. Present paper include a comprehensive survey on the research activities on RDE and its core technologies comprehensively to provide a direction for the future RDE researches, yet unfamiliar domestically.

Sustainability Analysis in Titanium Alloy Machining (항공용 티타늄 합금 가공 공정의 지속가능성 평가)

  • Lee, Jin-Hyeok;Kim, Ho-Yung;Yoon, Hae-Sung
    • Journal of the Korean Society of Manufacturing Process Engineers
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    • v.18 no.12
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    • pp.73-81
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    • 2019
  • Titanium alloys have been spotlighted in numerous industries owing to their superior mechanical properties, such as high specific strength. However, the high heat and wear resistance of titanium alloys also lower their machinability and limit the wider application of the material. Many researchers have investigated the processing of titanium alloys, and it is required to evaluate the effectiveness and efficiency of developed technologies. From this perspective, this research studied sustainability in titanium alloy machining. The power consumption of the machine was measured during the process and analyzed in terms of process parameters and individual machine components. Here, an end mill specially designed for titanium was also investigated and compared with a general-purpose cutting tool. Based on the experimental results, a model was constructed to predict the power consumption of the overall process. It is expected that this study will contribute to the more effective and efficient processing of titanium alloys.

Analysis of effectiveness of solar system internet to deep space exploration (태양계 인터넷이 심우주 탐사에 미치는 영향 분석)

  • Koo, Cheolhea;Kim, Changkyun;Rew, Dongyoung;Choi, Gihyuk
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.44 no.3
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    • pp.240-246
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    • 2016
  • The hottest news and achievements of space science and research in recent years may be NASA Curiosity rover's exploration (2013) of Mars, China Chang'e 3's exploration (2013) of Moon, ESA Rosetta's exploration (2014) of Comet 67P/Churyumov-Gerasimenko, and NASA New Horizons' exploration (2015) of Pluto, which are very astonishing achievement since such a deep space journey was possible with current technology. In contrast the wonderful cruise and navigation technologies evolution of explorer in deep space, there are no remarkable changes in deep space data communication, it is still in conservative area, of which much changes are reluctantly accepted so far. But there are some movements of deep space exploration in order to allow ground brilliant technologies to deep space. One of those experiments is internet, whose main topic of this paper. In this paper, we will present the analysis of effectiveness of solar system internet to deep space exploration.

Development of a UAV Using a Humanoid Robot (휴머노이드 로봇을 이용한 무인항공기 개발)

  • Song, Hanjun;Lee, Dasol;Shim, David Hyunchul
    • Journal of Institute of Control, Robotics and Systems
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    • v.20 no.11
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    • pp.1112-1117
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    • 2014
  • Unmanned aerial vehicles (UAVs) are a popular research topic because of a great ripple effect in the future. However, current UAV technologies cannot be applied to manual aerial vehicles without any modification. As an alternative to current UAV technology, humanoid robots are adopted as pilots. If a humanoid robot controls an aerial vehicle autonomously, not only could manual aerial vehicles be utilized as UAVs, but the humanoid robot would also be put into an environment created for humans and conduct some missions suitable for humans. Humanoid robots are also able to handle tools and equipment designed for humans. In order to prove that a humanoid robot can pilot an airplane, an experiment is performed and the results of this experiment are shown in this paper.

Feasibility Study for Practical Application of Aerospace Derivative Technology - Vertical Wind Tunnel (항공우주 파생기술 실용화를 위한 타당성 연구 - 수직 풍동)

  • Kwon, Kijung
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.45 no.2
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    • pp.148-153
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    • 2017
  • KARI LSWT(Korea Aerospace Research Institute Low Speed Wind Tunnel) has accumulated close to 20 years of know-how since its completion in 1998 and is trying to commercialize related technologies. As part of this research, KARI LSWT is studying design of vertical wind tunnel equipped with a skydiving simulator. KARI carries out concept design together with high performance/low noise design and is to transfer the related technology to a domestic producible company to increase commercialization possibility. In addition, KARI is seeking cooperation with related organizations in China to enter Chinese market.

An Application of the Cross-impact Hierarchy Process to Evaluate Aeronautics Technologies: A Case Study (상호영향계층분석방법을 이용한 항공기술의 평가에 관한 연구)

  • Kwon, Cheol-Shin;Cho, Keun-Tae
    • Proceedings of the Korean Operations and Management Science Society Conference
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    • 2000.10a
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    • pp.259-262
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    • 2000
  • The Cross-impact Hierarchy Process (CHP), an extended model of the Analytic Hierarchy Process(AHP) which is linked to Cross Impact Analysis(CIA), is a powerful decision making tool to assist in the ranking of large number of dependent technological alternatives. In this paper, we will describe an application of the CHP to the aerospace industry. We here conducted a questionnaire survey for S company that is one of the representative aerospace companies in Korea. A questionnaire was designed to obtain both the priority with dependence (the CHP priority) and the priority with independence (the AHP priority) in order to compare the priority derived by each of two methods. The hierarchy in this case study is concerned with priority setting for R&D area to ensure dependent aerospace design technology of the company, The result shows that there exists the difference hard to neglect between the final priorities gained by two methods.

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Design & Test of Stereo Camera Ground Model for Lunar Exploration

  • Heo, Haeng-Pal;Park, Jong-Euk;Shin, Sang-Youn;Yong, Sang-Soon
    • Korean Journal of Remote Sensing
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    • v.28 no.6
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    • pp.693-704
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    • 2012
  • Space-born remote sensing camera systems tend to be developed to have very high performances. They are developed to provide extremely small ground sample distance, wide swath width, and good MTF (Modulation Transfer Function) at the expense of big volume, massive weight, and big power consumption. Therefore, the camera system occupies relatively big portion of the satellite bus from the point of mass and volume. However, the camera systems for lunar exploration don't need to have such high performances. Instead, it should be versatile for various usages under various operating environments. It should be light and small and should consume small power. In order to be used for national program of lunar exploration, electro-optical versatile camera system, called MAEPLE (Multi-Application Electro-Optical Payload for Lunar Exploration), has been designed after the derivation of camera system requirements. A ground model of the camera system has been manufactured to identify and secure relevant key technologies. The ground model was mounted on an aircraft and checked if the basic design concept would be valid and versatile functions implemented on the camera system would worked properly. In this paper, results of design and functional test performed with the field campaigns and air-born imaging are introduced.