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Jang, Ik-Hyeon
- Proceedings of the Korea Information Processing Society Conference
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- 2001.10a
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- pp.267-270
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- 2001
본 논문에서는 이동통신망에서의 효율적인 인과순서 알고리즘을 채널전환 알고리즘과 함께 제안한다. 인과순서를 유지하기 위해서는 순서를 유지하기 위한 제어정보를 교환하여야 하며, 송수신 양측은 메시지를 보내거나 받은 전후에 각각의 제어정보를 수정하여야 한다. 특히 이동유닛이 다른 셀로 이동한 경우, 채널전환 프로토콜은 기존의 기지국과 새로운 기지국에서 동시에 제어정보 관리를 위한 작업을 수행하여야 하며, 기존의 기지국에 있는 이동 유닛의 제어정보는 새로운 기지국으로 전달되어야 한다. 따라서 제어정보의 크기가 채널전환시간과 메시지 지연시간에 직접적인 영향을 주기 때문에, 전송되는 제어정보의 양을 최소화하여야 한다. 본 논문에서는 제어정보의 양을 줄이기 위하여 유효한 통신패턴을 분석하여 중복으로 교환되는 제어정보가 최소화되는 인과순서 알고리즘을 제안하였으며, 모의실험을 통하여 제안된 알고리즘이 기존의 알고리즘에 비해 효율적임을 보였다.
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Kim, Young-Wan
- Journal of the Korea Institute of Information and Communication Engineering
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- v.11 no.3
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- pp.444-451
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- 2007
The design parameters of transmitter and receiver channel systems for COMS, which provides meteorological and ocean data services, were analyzed and the channel design parameters for a proper design of a small user-terminal were proposed in this paper. The COMS transmits the oceanic observation data by using the S/L-band link to the earth station. The meteorological data also are transmitted to the earth station, the meteorological data services, which are processed in the earth station, are provided to user. The sensor data are transmitted as digital signal type and are received by bilateral small-sized user terminals. So the optimal channel system for transmission and reception of sensor data should be designed on the basis of the channel modeling and analyzed results for primary technologies.
https://doi.org/10.6109/jkiice.2007.11.3.444 인용 PDF KSCI

Jeon, Moon-Jin;Kim, Eunghyun;Lim, Seong-Bin
- Aerospace Engineering and Technology
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- v.13 no.1
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- pp.37-43
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- 2014
The ground station which operates the LEO satellite performs monitoring state of health of the satellite, sending the commands for the imaging mission of receiving the images during about 10 minutes of contact time. To finish the planned procedure in limited contact time, specific level of autonomy is applied in the satellite and the ground system. For example, the attitude and orbit control logic has high level of autonomy because it must be operated alone for long period without operator intervention. On the other hand, the fault management logic has relatively low level of autonomy because of that failure detection and safing operation are performed on-board, whereas failure identification and recovery are on-ground operation. The level of autonomy of the satellite affects also the ground operation. The command set for mission operation is generated by ground system. If the satellite has higher level of autonomy, some of operation currently done on-ground can be performed on-board, so the ground operation can be simplified. In this paper, we discuss the level of autonomy and propose a concept for improving the level of autonomy of an LEO satellite.
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