• Title/Summary/Keyword: Space vehicles

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Color Segmentation of Vehicle License Plates in the RGB Color Space Using Color Component Binarization (RGB 색상 공간에서 색상 성분 이진화를 이용한차량 번호판 색상 분할)

  • Jung, Min Chul
    • Journal of the Semiconductor & Display Technology
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    • v.13 no.4
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    • pp.49-54
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    • 2014
  • This paper proposes a new color segmentation method of vehicle license plates in the RGB color space. Firstly, the proposed method shifts the histogram of an input image rightwards and then stretches the image of the histogram slide. Secondly, the method separates each of the three RGB color components and performs the adaptive threshold processing with the three components, respectively. Finally, it combines the three components under the condition of making up a segment color and removes noises with the morphological processing. The proposed method is implemented using C language in an embedded Linux system for a high-speed real-time image processing. Experiments were conducted by using real vehicle images. The results show that the proposed algorithm is successful for most vehicle images. However, the method fails in some vehicles when the body and the license plate have the same color.

Hierarchical Behavior Control of Mobile Robot Based on Space & Time Sensor Fusion(STSF)

  • Han, Ho-Tack
    • International Journal of Fuzzy Logic and Intelligent Systems
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    • v.6 no.4
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    • pp.314-320
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    • 2006
  • Navigation in environments that are densely cluttered with obstacles is still a challenge for Autonomous Ground Vehicles (AGVs), especially when the configuration of obstacles is not known a priori. Reactive local navigation schemes that tightly couple the robot actions to the sensor information have proved to be effective in these environments, and because of the environmental uncertainties, STSF(Space and Time Sensor Fusion)-based fuzzy behavior systems have been proposed. Realization of autonomous behavior in mobile robots, using STSF control based on spatial data fusion, requires formulation of rules which are collectively responsible for necessary levels of intelligence. This collection of rules can be conveniently decomposed and efficiently implemented as a hierarchy of fuzzy-behaviors. This paper describes how this can be done using a behavior-based architecture. The approach is motivated by ethological models which suggest hierarchical organizations of behavior. Experimental results show that the proposed method can smoothly and effectively guide a robot through cluttered environments such as dense forests.

Power Line Extraction based on thermal Image (열영상 기반의 전력선검출)

  • Kim, Dong-Wook
    • The Journal of the Korea institute of electronic communication sciences
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    • v.5 no.3
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    • pp.245-250
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    • 2010
  • In this paper, an efficient extraction technique of power lines is proposed. Power line extraction technique is used to operate unmanned autonomous vehicles. To achieve the extraction of power lines, an angle space segmentation and grouping method of Hough transform are developed. In simulation results for the proposed algorithm, our algorithm shows a good detection results in experiments for several aerial images which contain different line components.

Propellants helium saturated efforts and its effects for HTV(H-II transfer vehicle) propulsion system ground firing tests

  • Nakai, Shunichiro;Ishizaki, Shinichiro;Yamamoto, Mio;Okudera, Hiroyuki;Imada, Takane;Matsuo, Shinobu
    • Proceedings of the Korean Society of Propulsion Engineers Conference
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    • 2008.03a
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    • pp.399-402
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    • 2008
  • It is well known that helium saturated propellants significantly effects the dynamics of propulsion system, thruster cross coupling, water hammer and thruster performance. Especially for the propulsion systems, which have multiple high thrust engines, such as HTV(H-II transfer vehicle), the effect is more important. Therefore full-saturated propellants should be used at ground tests of HTV propulsion system and evaluate its effects. HTV is an advanced space vehicle being developed by Japan Aerospace Exploration Agency(JAXA) to enhance cargo delivery capabilities of the fleet of vehicles visiting the International Space Station(ISS). This paper presents an overview of the successful effort of the testing with saturated propellants(MMH/MON3) for HTV propulsion system during the ground firing tests.

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Remedial Junction of Proton Irradiated Single Walled Carbon Nanotubes using Heat Treatment For Solar Energy Harvesting (태양에너지 획득 양성자 조사 단일벽 탄소나노튜브의 열처리에 의한 교정결합)

  • Kim, Tae Gyu;Park, Young Min;Kim, Young Bae;Kim, Dae Weon
    • Journal of the Korean Society for Heat Treatment
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    • v.32 no.1
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    • pp.29-35
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    • 2019
  • The remedial junction is found in the network of single walled carbon nanotubes after the irradiation of protons not only for the better mechanical strength but also for the higher property of electrical conductivity. The irradiated proton formed a beam transferred sufficient energy to change the sp2 structure of atomic carbon as much as damage of crystalline formation, however it is shown the cross bonding while recovery of structure. This improved network in 2-D atomic chain of carbon is expected to use in a critical part in space energy harvesting system related with the solar radiation.

LEO 5G-NTN Service Trends (저궤도 5G-NTN 서비스 동향)

  • B.W. Kim;G.E. Choi
    • Electronics and Telecommunications Trends
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    • v.38 no.5
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    • pp.114-124
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    • 2023
  • Recently, there have been the World Economic Forum's space economy guidelines, the International Telecommunication Union's regulations for each satellite orbit, the development of chips using satellite communication by global manufacturers and service providers, and the registration of key telecommunication businesses. Accordingly, trends in low-orbit 5G satellite communication services in Korea were investigated and analyzed, and the current situation in Korea was diagnosed. Korea's satellite communications accounts for 0.31% of all satellites when analyzed centering on countries with 20 or more satellites. Korea's communication satellite holdings are insufficient compared to 187 times that of the United States, 45 times that of Russia, and 18 times that of China. There is no link technology between 5G and LEO, and the cost of launch vehicles is high. In addition, it is judged that the ecosystem of equipment companies in the low-orbit 5G-NTN business model is insufficient.

Opening New Horizons with the L4 Mission: Vision and Plan

  • Kyung-Suk Cho;Junga Hwang;Jeong-Yeol Han;Seong-Hwan Choi;Sung-Hong Park;Eun-Kyung Lim;Rok-Soon Kim;Jungjoon Seough;Jong-Dae Sohn;Donguk Song;Jae-Young Kwak;Yukinaga Miyashita;Ji-Hye Baek;Jaejin Lee;Jinsung Lee;Kwangsun Ryu;Jongho Seon;Ho Jin;Sung-Jun Ye;Yong-Jae, Moon;Dae-Young Lee;Peter H. Yoon;Thiem Hoang;Veerle Sterken;Bhuwan Joshi;Chang-Han Lee;Jongjin Jang;Jae-Hwee Doh;Hwayeong Kim;Hyeon-Jeong Park;Natchimuthuk Gopalswamy;Talaat Elsayed;John Lee
    • Journal of The Korean Astronomical Society
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    • v.56 no.2
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    • pp.263-275
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    • 2023
  • The Sun-Earth Lagrange point L4 is considered as one of the unique places where the solar activity and heliospheric environment can be observed in a continuous and comprehensive manner. The L4 mission affords a clear and wide-angle view of the Sun-Earth line for the study of the Sun-Earth and Sun-Moon connections from he perspective of remote-sensing observations. In-situ measurements of the solar radiation, solar wind, and heliospheric magnetic field are critical components necessary for monitoring and forecasting the radiation environment as it relates to the issue of safe human exploration of the Moon and Mars. A dust detector on the ram side of the spacecraft allows for an unprecedented detection of local dust and its interactions with the heliosphere. The purpose of the present paper is to emphasize the importance of L4 observations as well as to outline a strategy for the planned L4 mission with remote and in-situ payloads onboard a Korean spacecraft. It is expected that the Korean L4 mission can significantly contribute to improving the space weather forecasting capability by enhancing the understanding of heliosphere through comprehensive and coordinated observations of the heliosphere at multi-points with other existing or planned L1 and L5 missions.

Implementation of Small Automatic Lubrication Device for Automated Processes in Smart Factory (스마트 공장에서 자동화 공정을 위한 소형 자동 윤활 장치 구현)

  • Lee, Yoo-Ri;Kim, Hyeong-Jun;Kim, Man-Ho
    • Journal of the Korean Society of Industry Convergence
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    • v.23 no.5
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    • pp.765-771
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    • 2020
  • Automatic lubrication devices are applied in various fields, such as huge machinery, construction machinery or commercial vehicles, to lower maintenance costs and protect the devices. In addition, the automatic lubrication device reduces frequent component failures cause by friction and allows the machine to replace the lubricating oil replenishment work carried out by the manager. However, the automatic lubricating device used in large machinery or commercial vehicles is relatively large, containing a large amount of lubricant in the space to be lubricated. On the other hand, a smart factory, such as a home appliance or cosmetics factory, lacks space to install large automatic lubrication devices, and it is difficult to distribute electricity. Therefore, there is a need for an automatic lubrication device that can be used in various environments that require lubrication. In this paper, a small automatic lubrication device is proposed for smart factories that have changed parts of existing factories, such as electronics factories, to minimize friction arising from mechanical parts, etc. In particular, the structure of lubricating pumps and component parts that are the core of automatic lubrication devices was described so that they could be utilized in various fields. Finally, a test bed environment is established for the proposed automatic lubrication device to evaluate its performance and verify its applicability.

Development of Direct drive Electro-mechanical Actuation System for Thrust Vector Control of KSLV-II (한국형발사체 추력벡터제어 직구동 방식 전기기계식 구동장치시스템 개발)

  • Lee, Hee-Joong;Kang, E-Sok
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.44 no.10
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    • pp.911-920
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    • 2016
  • For the pitch and yaw axis attitude control of launch vehicle, thrust vector control which changes the direction of thrust during the engine combustion is commonly used. Hydraulic actuation system has been used generally as a drive system for the thrust vector control of launch vehicles with the advantage of power-to-weight ratio. Nowadays, due to the developments of highly efficient electric motor and motor control techniques, it has done a lot of research to adopt electro-mechanical actuator for thrust vector control of small-sized launch vehicles. This paper describes system design and test results of the prototype of direct drive electro-mechanical actuation system which is being developed for the thrust vector control of $3^{rd}$ stage engine of KSVL-II.

Mathematical Prediction of the Lunar Surface Temperature Using the Lumped System Analysis Method (집중계 해석법을 이용한 달 표면온도 예측)

  • Kim, Taig Young;Lee, Jang-Joon;Chang, Su-Young;Kim, Jung-Hoon;Hyun, Bum-Seok;Cheon, Hyeong Yul;Hua, Hang-Pal
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.46 no.4
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    • pp.338-344
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    • 2018
  • The lunar surface temperature is important as a environmental parameter for the thermal design of the lunar exploration vehicles such as orbital spacecraft, lander, and rovers. In this study, the temperature is numerically predicted through a simplified lumped system model for the energy conservation. The physical values required for the analysis of the energy equation are derived by considering the geometric shape, and the values presented in the previous research results. The areal specific heat, which is the most important thermo-physical property of the lumped system model, was extracted from the temperature measurements by the Diviner loaded on the LRO, and the value was predicted by calibration of the analytical model to the measurements. The predicted temperature distribution obtained through numerical integration has sufficient accuracy to be applied to the thermal design of the lunar exploration vehicles.