• Title/Summary/Keyword: Satellite communication

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Link Relay H-ARQ mode for Throughput improvement in a Satellite Communication network (위성통신망에서 Throughput 향상을 위한 Link Relay H-ARQ 방식)

  • Hwang, Lan-Mi;Lee, Byung-Jin;Yeo, Bong-Gu;Cho, Ju-Phil;Kim, Kyung-Seok
    • The Journal of the Institute of Internet, Broadcasting and Communication
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    • v.16 no.1
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    • pp.121-127
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    • 2016
  • Satellite communication is a communication method using a satellite as a repeater communication on the air and have a communication range is wide and is possible to transmit high-speed data, so Satellite communication has been highlighted as the next generation communication. However, because the distance between the ground and the satellite is far away, there is a disadvantage that propagation delay time is very long and packet is damaged. Therefore, this study was applied to Link Relay H-ARQ system in order to complement the damage to the packet. Furthermore, we propose the Modified Link Relay H-ARQ scheme is a new scheme to supplementation the delay time. By applying the Markov channel for implementing a channel of satellite communications, the results of analyzing the performance, when applying the Link Relay HARQ scheme, BER and PER performance was improved, when applying the Modified Link Relay H-ARQ scheme, Throughput performance was confirmed improvement.

Lunar Exploration Satellite Communication Link Analysis (달 탐사 위성의 통신 링크 분석)

  • Kim, Ah-Leum;Lee, Seul-Ki;Lee, Woo-Kyung
    • Journal of Satellite, Information and Communications
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    • v.6 no.1
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    • pp.1-5
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    • 2011
  • In recent space industry, It has become a major trend to launch lunar exploration satellites to extend activities in the deep space environment. In this paper, a link budget analysis is carried out for the lunar exploration satellite. One of the major difference between the lunar satellite and LEO spacecraft lies in the orbit parameters. The vast distance between spacecraft and the Earth station imposes a challenging task for the spacecraft designers in terms of achieving stable communication link budget. The satellite tool kit software has been adopted to simulate the lunar exploring satellite. The relative distance between the spacecraft and the ground stations are tracked and the communication link budget is calculated accordingly.

The Construction of voice network in the island using the satellite communication system (위성통신망을 이용한 도서지역 음성네트워크 구축)

  • Kim, Soo-Bae;Hyun, Duck-Hwa;Kim, Myong-Soo;Lee, Sang-Jin
    • Proceedings of the KIEE Conference
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    • 2005.10b
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    • pp.298-300
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    • 2005
  • There are several types of communication method which is used for providing the supply of electric power stably. But the communication methods used in KEPCO have weak points in the viewpoint of economy, technology and management. Therefore the power plant located in the island could not be provided the communication service because of above reasons. Because the Satellite communication systems have competitive power in price and technology nowdays, the utility could provide the communication service in even back land. This paper presents some of design efforts for the satellite communication systems as the voice network in the island.

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Radiation Analysis of Communications and Broadcasting Satellite

  • Park, Jae-Woo;Chung, Tae-Jin;Lee, Seong-Pal;Seon, Jong-Ho;Jeong, Yun-Whang
    • International Journal of Aeronautical and Space Sciences
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    • v.3 no.2
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    • pp.40-45
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    • 2002
  • A radiation analysis is performed for the Ka and Ku-band transponder of the Communications and Broadcasting Satellite (CBS) that is planned for launch into the geo-synchronous orbit. A particular attention is given to calculation of Total Ionizing Dose (TID) for the mission life time of 15 + 3 years. A numerical modeling of the charged particles at the geo-synchronous orbit is undertaken. The charged particles from the modeling are then transported through the mechanical structure and component housings of the transponder. A set of locations are selected for the detailed calculation of TID. The results from the present calculation show that three-dimensional modeling of the component housings as well as the mechanical structure of the spacecraft is requisite in order to acquire a reliable calculation of TID.

The Desing and Implementation for 1553B using Aircraft and Satellite (항공과 위성에 이용하는 1553B 통신설계 및 Debugging에 관한 연구)

  • Lee, Hyun-Seock;Lim, Ki-Tak;Jang, Jong-Jin
    • Proceedings of the IEEK Conference
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    • 2008.06a
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    • pp.1065-1066
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    • 2008
  • We discuss about Design and Debugging for 1553B Communication. 1553B Communication is used in Aircraft and Satellite System. When we design a Satellite Control Computer, we apply a 1553B Communication among Satellite Control Computer and others. Satellite Control Computer has a PM32 Module, it is CPU and control module especially. In this paper, we show you a 1553B Communication Design and Debugging in the Satellite System.

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Data envelopment analyses on evaluating efficiencies of satellite communication and broadcasting R&D outcomes in Korea

  • Ahn, Jae-Kyoung;Ahn, Do-Seob;Ku, Bon-Jun
    • Journal of Satellite, Information and Communications
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    • v.3 no.2
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    • pp.54-59
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    • 2008
  • Traditionally R&D evaluation has been performed by experts who can understand the contents of the study area very well. Recently extensive application of quantitative evaluation methods have been attempted for introducing the administrative management system that poses greater importance on records and results. More objective reviews on the R&D outcomes are called for gaining public supports. In this paper a bibliometrical analysis is to be performed to evaluate satellite communication and broadcasting public R&D outcomes for last 7 years. Data envelopment analysis method is selected for evaluating the efficiencies of multiple outputs (papers, patents, royalties, technology transfers) where multiple inputs (number of researchers and R&D expenses) are given. R&D outcomes from 22 research institutes are being compared and satellite communication and broadcasting R&D efforts turn out to be highly efficient.

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THERMAL CONTROL DESIGN FOR COMS (COMS 특별세션)

  • Jun, Hyoung-Yoll;Kim, Jung-Hoon;Kim, Sung-Hoon;Yang, Koon-Ho
    • Proceedings of the KSRS Conference
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    • 2007.10a
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    • pp.199-202
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    • 2007
  • COMS (Communication, Ocean and Meteorological Satellite) is a geostationary satellite and has been developing by KARI for communication, ocean observation and meteorological observation. Conventional thermal control design, using MLI (Multi Layer Insulation), OSR (Optical Solar Reflector), heater and heat pipe, is utilized. Ka-band components are installed on South wall, while other equipment for sensors are installed on the opposite side, North wall. High dissipating communication units are located on external (surface) heat pipe and are covered by internal insulation blankets to decouple them from the rest of the satellite. External satellite walls are covered by MLI or OSR for insulation from space and for rejection internal heat to space. The ocean and meteorological sensors are installed on optical benches on the top floor to decouple thermally from the satellite. Single solar array wing is adopted in order to secure clear field of view of radiant cooler of IR meteorological sensor. This paper presents principles of thermal control design for the COMS.

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Performance enhancement of GSO FSS TCP/IP network (정지위성 TCP/IP 네트워크 전송 성능 향상)

  • Hong, Wan-Pyo
    • The Journal of Korean Institute of Communications and Information Sciences
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    • v.32 no.2B
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    • pp.118-123
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    • 2007
  • This paper studied the transmission control protocol over IP network to enhance the performance of the GSO satellite communication networks. The focus of this study is how to reduce the long round trip time and the transmission data rates over satellite link in the bidirectional satellite network. To do it, this study applied the caching and spoofing technology. The spoofing technology is used to reduce the required time for the link connection during communication. The caching technology is to improve the transmission bandwidth efficiency in the high transmission data rate link The tests and measurements in this study was performed in the commercial GSO communication satellite network and the terrestrial Internet network. The results of this paper show that the studied protocol in this paper highly enhance the performance of the bidirectional satellite communication network compare to the using TCP/IP satellite network protocol.

End-to-End Soft QoS Approach for IMS-based Integrated Satellite/Terrestrial Network Architecture

  • Chowdhury, Mostafa Zaman;Jang, Yeong-Min
    • Journal of Satellite, Information and Communications
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    • v.2 no.2
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    • pp.85-91
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    • 2007
  • The satellite networks provide global coverage. The integration of terrestrial networks with a satellite network is the most attractive approach to develop a global communication system. The IP Multimedia Subsystem (IMS) is intended to be the system that will merge the internet with the telecom world. A user with a dual-mode terminal can access both the satellite network and terrestrial network. The seamless handoff between two networks and a user's QoS level is the major issue concerning this integration. In this paper, we propose IMS-based satellite/terrestrial integrated network architecture for a global communication system. Based on the proposed architecture, an inter-network handoff and end-to-end soft QoS procedure is discussed. Our proposed soft QoS scheme is also analyzed to calculate the number of rejected calls.

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COMMUNICATIONS SATELLITE SYSTEM BY USING MOON ORBIT SATELLITE CONSTELLATION

  • Lee, Sang-Uk;Kim, Jae-Hoon;Lee, Seong-Pal
    • Journal of Astronomy and Space Sciences
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    • v.20 no.4
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    • pp.313-318
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    • 2003
  • A communications satellite system placed in three-Lagrange points, $L_3$, $L_4$ and $L_5$, of the restricted three-body problem in Earth-Moon system is proposed in this paper. LEO satellite constellation has been another choice of communications system. The proposed system which is alternatives of limited geostationary orbit resources, has some weak points such as long distance from the Earth, relatively expensive launch cost, long delay time, more required power, and so on. It has good points like less efforts (fuel) for station keeping, less eclipses, etc. This system has limitations for applications to provide commercial services but it is still some attractive points.