• Title/Summary/Keyword: Up-link Station

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Modeling & Implementation of Operational Test and Evaluation, Offline Monitoring Software for Korea Augmentation Satellite System Uplink Station (한국형 위성항법 보정시스템 위성통신국 운용시험평가 오프라인감시 소프트웨어 모델링 및 구현)

  • Lee, Sanguk;You, Moonhee;Hyoung, Chang-Hee;Jeong, InCheol;Choi, SangHyouk;Sin, Cheon Sig
    • Journal of Satellite, Information and Communications
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    • v.11 no.4
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    • pp.74-80
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    • 2016
  • In this paper, the modeling and implementation results of the operational test and evaluation tool of the KASS up-link station composed of the GEO(Geostationary Earth Orbit) satellite signal analysis tool model that analyzes the GEO satellite signal and the GEO message analysis tool model that analyzes the GEO satellite navigation message. In addition, we describe the results of software modeling and implementation of some software models of GEO satellite and KASS up-link stations that can generate and provide simulated signals to operational test and evaluation tools of these KASS up-link stations.

Design of Ground Station System for CubeSat STEP Cube Lab. (큐브위성 STEP Cube Lab.의 지상국 시스템 설계)

  • Jeon, Younghyeon;Chae, Bonggeon;Jeong, Hyeonmo;Jeon, Seongyong;Oh, Hyunung
    • Journal of Aerospace System Engineering
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    • v.6 no.4
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    • pp.34-39
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    • 2012
  • CubeSats classified as pico-class satellite require a ground station to track the satellite, transmit a command, and receive an on-orbit data such as SOH (State-of-Health) and mission data according to the operation plan. For this, ground station system has to be properly designed to perform a communication to with the satellite with enough up- and down-link budgets. In this study, a conceptual design of the ground station has been performed for the CubeSat named as STEP Cube Lab. (Cube Laboratory for Space Technology Experimental Project). The paper includes a ground station hardware interface design, link budget analysis and a ground station software realization. In addition, the operation plan of the ground station has been established considering the STEP Cube Lab. mission requirements.

Link Label-Based Optimal Path Algorithm Considering Station Transfer Penalty - Focusing on A Smart Card Based Railway Network - (역사환승페널티를 고려한 링크표지기반 최적경로탐색 - 교통카드기반 철도네트워크를 중심으로 -)

  • Lee, Mee Young
    • KSCE Journal of Civil and Environmental Engineering Research
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    • v.38 no.6
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    • pp.941-947
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    • 2018
  • Station transfers for smart card based railway networks refer to transfer pedestrian movements that occur at the origin and destination nodes rather than at a middle station. To calculate the optimum path for the railway network, a penalty for transfer pedestrian movement must be included in addition to the cost of within-car transit time. However, the existing link label-based path searching method is constructed so that the station transfer penalty between two links is detected. As such, station transfer penalties that appear at the origin and destination stations are not adequately reflected, limiting the effectiveness of the model. A ghost node may be introduced to expand the network, to make up for the station transfer penalty, but has a pitfall in that the link label-based path algorithm will not hold up effectively. This research proposes an optimal path search algorithm to reflect station transfer penalties without resorting to enlargement of the existing network. To achieve this, a method for applying a directline transfer penalty by comparing Ticket Gate ID and the line of the link is proposed.

Analysis of Data Rate on Optical Communication Links between Geo-Satellite and Earth Station (정지궤도 위성과 지구국간 광통신 링크의 전송속도 해석)

  • Han, Jong-Seok;Jung, Jin-Ho;Kim, Yung-Kwon
    • Journal of IKEEE
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    • v.1 no.1 s.1
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    • pp.120-137
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    • 1997
  • Han's model, which is able to analyze optical communication between earth station and geo-satellite as a function of atmospheric conditions and elevation angles. is presented. In Han's model, atmospheric conditions are roughly classified into six basic types; clear sky, cloud, haze, fog, rain and snow. Data rate satisfying for the BER below $10^{-7}$ is analyzed by Han's model in case of up-link and down-link, respectively. Data rate is more limited by up-link than by down-link because the pointing loss caused by atmosphere on the up-link is greater than the spatial coherence degradation caused by atmosphere on the down-link.

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The design of transmitting antenna on the optical satelite communication up-link in rain (광위성 통신시 업링크에서 강우에 따른 송신 안테나 설계)

  • 정진호
    • Journal of the Korean Institute of Telematics and Electronics D
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    • v.34D no.6
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    • pp.75-82
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    • 1997
  • Today's wireless communication needs the super-high speed for picture transmission as well as voice. The optical communication with the very wide bandwidth is suitable for this demand. To fulfill the optical wireless communication, however, the atmospheric attenuation in rainy weather condition must be overcome. In the optical satellite up-link communication between geo-satellite and earth station, the factors of attenuation are turbulence, pointing error, scattering, and so on. The most serious factor for these is the scattering by rain. Under the weather conditiion of rain and cloud, in this paper, the atmospheic attenuation which affects the optical satellite up-link communication was considered, and the optimum idameter of the optical satellite transmitting antenna in the earth station versus elevation angles, data rates and rainfall rates was presented.

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Design of Ground Station System for CubeSat STEP Cube Lab. (큐브위성 STEP Cube Lab.의 지상국 시스템 개발)

  • Jeon, Younghyeon;Chae, Bonggeon;Jeong, Hyeonmo;Jeon, Seongyong;Oh, Hyunung
    • Journal of Aerospace System Engineering
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    • v.9 no.4
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    • pp.37-42
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    • 2015
  • The CubeSats is classified as a pico-class satellite which requires a ground station to track the satellite, transmit commands, and receive an on-orbit data such as SOH (State-of-Health) and mission data according to the operation plan. In order to this, the ground station system has to be properly designed to perform a communication to with the satellite with enough up- and down-link budgets. In this study, a conceptual design of the ground station has been performed for the CubeSat named as STEP Cube Lab. (Cube Laboratory for Space Technology Experimental Project). The paper includes a ground station hardware interface design, a link budget analysis and a ground station software realization. In addition, the operation plan of the ground station has been established considering the STEP Cube Lab. mission requirements.

A SNR Estimation Algorithm for Digital Satellite Transponder (디지털 위성트랜스폰더를 위한 SNR 추정 알고리즘)

  • Seo, Kwang-Nam;Choi, Seung-Woon;Kim, Chong-Hoon
    • The Journal of Korean Institute of Communications and Information Sciences
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    • v.35 no.9C
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    • pp.729-734
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    • 2010
  • In the initial stage of the communications between a base station and a satellite transponder, the base station transmits the frequency-sweeping un-modulated up-link carrier within a certain frequency range to acquire the doppler frequency shift and signal power between the base station and the satellite in orbital flight. The satellite transponder acquires and tracks the carrier in order to initialize the communication. To control such initialization process, the satellite receiver should analyze the input carrier signal in various ways. This paper presents an SNR estimation algorithm to control the initialization process. The proposed algorithm converts the input signal into the baseband polar coordinate representation and estimates the SNR via the statistics of the angular signal components as well as the status parameters to control the receiver. The Monte-Carlo simulations shows the validity of the estimation proposed.

A Realization of the Synchronization Module between the Up-Link and the Down-Link for the WiBro System (WiBro 시스템에서 상향링크와 하향링크 간 시간 동기 장치 구현)

  • Park Hyong-Rock;Kim Jae-Hyung;Hong Een-Kee
    • Journal of The Institute of Information and Telecommunication Facilities Engineering
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    • v.4 no.1
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    • pp.7-13
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    • 2005
  • In this paper, we propose the time synchronization module on fiber optic repeater to use optic line delay for obtaining time synchronization between up-link and down-link, in the 2.3 GHz WiBro network using TDD/OFDM (Time Division Duplex/Orthogonal Frequency Division Multiplexing) Generally, when we use fiber optic repeater to remove the shade area, it occurs transmission delay which is caused by optic transmission between RAS (Radio Access Station) and fiber optic repeater and inner delay of fiber optic repeater. Because the WiBro system is adopting a TOO method and there exists the difference of switching time which is caused by these delay between up-link and down-link, it occurs ISI (Inter Symbol Interference), ICI (Inter Carrier Interference). These interference results in the reduction of the coverage. And the inconsistency between Up-Link and Down-Link switching time maybe gives rise to the interruption of communication. In order to prevent these cases, we propose synchronization module using analog optic line delay as the one of synchronizing up-link and down-link. And we propose the consideration factor for the designing time synchronization module and the feature of optic line of analog method. The measurement result of optic line time synchronization module of structure proposed is as follows, the delay error of $0.5{\mu}g$ and the insertion loss value below maximum 4.5dB in range of $0{\sim}40{\mu}s$. These results fully meet the specification of WiBro System.

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The optimum design of optical transmitting antenna versus elevation angle on the optical satellite communication up-link for B-ISDN (B-ISDN용 광위성 통신 업링크의 앙각에 따른 송신안테나 최적설계에 관한 연구)

  • 한종석;이준구;정진호;김영권
    • Journal of the Korean Institute of Telematics and Electronics A
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    • v.32A no.10
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    • pp.64-72
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    • 1995
  • In this paper, atmospheric turbulence and absorption under clear weather condition, which affect the optical satellite up-link communication between geo-satellites and earth station, were studied. In case of the up-link communication, the received optical power is weakened by pointing loss caused by beam tilt which is the main effect of turbulent atmosphere. This pointing loss directly has relation to the diameter of optical transmitting antenna. From the inverse proportion of the pointing and spaced loss, it is the regions where the diameter of transmitting antenna increases abruptly and the efficient design of transmitting antenna is impossible. In case of using channel coding, it was shown that the peak value of diameter moved to the lower regions of elevation angle with increasing the coding gain and its width was also decreased. In case of considering both coding gain and transmission rate on the design of transmitting antenna, it was known that more coding gain was necessary as transmission rate was increased.

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KOMPSAT-2 RF COMPATIBILITY TEST FOR S-BAND

  • Cho Seung-Won;Youn Young-Su;Choi Jong-Yeon;Choi Seok-Weon
    • Bulletin of the Korean Space Science Society
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    • 2004.10b
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    • pp.344-346
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    • 2004
  • KOMPSAT-2 (Korea Multi Purpose Satellite 2) which is scheduled to launch in 2005 year will communicate with KARI TTC (Tracking, Telemetry, and Command) station flying along sun synchronous orbits (685 km). The command from KARI TTC passes S-band omni-antenna, RF assembly, and transponder and finally reachs OBC (On Board Computer). The telemetry from KOMPSAT-2 arrives at KARI TTC through inverse procedure. In this paper, RF compatibility test between KOMPSAT-2 and KARI TTC station is demonstrated. RF interface for this test was established through real space and uplink signal test and downlink signal test and uplink & downlink signal test were performed.

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