Abstract:
본 발명은 정지궤도 위성의 원격명령 실행 장치 및 그 방법, 위성 관제 시스템의 원격명령 실행 검증 장치 및 그 방법을 제공하는 것이다. 본 발명에 의한 위성의 원격명령 실행은 실행한 원격명령에 대해 명령실행 검증워드를 생성하여 원격측정 전송 프레임에 추가함으로써 위성 관제 시스템이 용이하게 원격명령 실행을 실시간으로 검증할 수 있도록 한다. 또한 본 발명에 의한 위성 관제 시스템의 원격명령 실행 결과 검증은, 위성에서 제공하는 명령실행 검증워드, 위성 관제 시스템에서 제공하는 원격명령 이미지 데이터베이스, 원격명령 검증자 데이터베이스, 원격명령 검증기를 통해, 시간 지연 없이 타임태그 원격명령의 실행 결과를 검증할 수 있기 때문에, 원격명령, 특히 타임태그 원격명령의 전송부터 검증까지의 일련의 과정을 실시간으로 운용자의 개입 없이 자동화하여 처리할 수 있게 된다. 위성관제(Satellite Ground Control), 원격명령(Telecommand), 원격측정(Telemetry), 검증(Verification), 타임태그 원격명령(Time-tag Telecommand), 명령실행 검증워드(Command Execution Verification Words)
Abstract:
본 발명은 실시간 e러닝 서비스를 위한 입체 음향 구현 방법 및 그 시스템에 관한 것으로, 실시간 e러닝 서비스가 제공하는 강의에 참여한 강의 참여자들의 영상을 디스플레이하는 e러닝 화면 인터페이스; 상기 강의 참여자들의 영상에 대하여 상기 e러닝 화면 인터페이스 상에서의 위치 정보를 검출하는 영상 위치 검출기; 상기 검출된 위치 정보에 따라 상기 각 영상의 음성 출력을 다수의 스피커별로 서로 다르게 조절하는 음성 이득 조절기를 포함하여 구성되며, 이에 의하여 사용자의 서비스 사용 편의를 증대시키고, 사용자가 여러 원격 참여자 중에서 현재의 화자를 용이하게 파악하도록 하는 효과를 가진다. 입체음향, 실시간 e러닝 서비스
Abstract:
본 발명은 IP기반 통합 맞춤형 방송 서비스 시스템 및 방법에 관한 것으로, 방송프로그램 또는 IP기반 콘텐츠를 사용자가 제공받고자 하는 시점에 맞춘 가입자 편성표를 생성하는 가입자 편성표 제공 서버부 및 상기 가입자 편성표에 따라 상기 방송프로그램을 제공할 경우 상기 사용자에게 해당 방송프로그램을 송출하고, 상기 IP기반 콘텐츠를 제공할 경우 상기 사용자가 시청가능한 방송서비스 형태로 변환하여 제공하는 방송서버부를 포함하며, VoD나 UCC/PCC 콘텐츠도 방송에 이용할 수 있어 방송 프로그램이 다양해 질 수 있다. IP기반 방송 서비스 시스템, VoD 콘텐츠, UCC 콘텐츠
Abstract:
An apparatus for supporting handover based on the mobile IP network by using the 2-layer information and a method thereof are provided to maintain the Internet connection continuously by using the 2-layer information even in case a wireless Internet terminal has to perform the handover during the movement, thereby preventing the interception of a service. A registration request message receiving unit(210) receives a registration request message from a mobile terminal which predicts the handover from the first network(204) to the second network(203). A registration request message transmitting unit(220) transmits the registration request message to a home server to instruct registration of the address of the second network and the tunneling of data to be transmitted to the mobile terminal to the second network. A data forwarding unit(230) forwards the tunneled data to the first network until the mobile terminal connects to the second network.
Abstract:
The telecommand execution apparatus and method of a geostationary satellite and the telecommand execution apparatus and method of a satellite control system are provided to verify whether a telecommand such as a time-tage telecommand which is executed at a preset time is accurately performed, automatically, thereby minimizing the intervention of an operator and improving the real-time processing performance. A telecommand receiver(110) receives a telecommand signal from a satellite control system, and then extracts a telecommand transfer frame from the received telecommand signal. A link control unit(130) determines the validity related to whether the extracted telecommand transfer frame is normally transmitted. An on-board computer(150) extracts a telecommand packet from the telecommand transfer frame, and then determines whether the extracted result is a real-time telecommand or a time-tage telecommand which is executed at a preset time. A time tag telecommand memory(170) receives a time tag command from the on-board computer, and then stores the command until the on-board computer executes the command. A telemetry transmitter(190) generates a telemetry transfer frame including general telemetry data and a command execution verification word, and then transmits the generated telemetry transfer frame to the satellite control system.
Abstract:
A vehicle clock synchronization method according to a navigation system is provided to revive precise situations of a vehicle at the time of accident by supplying precise time data to a vehicle black box by using a navigation system. A satellite navigation receiver(120) receives a navigation signal from one or more navigation satellites(110) to carry out clock synchronization between the navigation satellites and the satellite navigation receiver(22). Interface is established between clock-using devices(130,140) and the satellite navigation receiver(23). The satellite navigation receiver is set in the condition for transferring time data(24) and transmits the time data to the clock-using devices(25) so that the clock synchronization is realized between the satellite navigation receiver and the clock-using devices.
Abstract:
An apparatus for transceiving remotely-measured data and a method thereof are provided to enable a satellite control system which receives the remotely-measured data from the satellite to easily and conveniently restore the received data. The first grouping part(310) classifies remotely-measured data about the states of plural subsystems comprising a satellite according to each subsystem, and then assigns the first identifier to the first group. The second grouping part(320) classifies the second groups within the first group according to the standards which is set up by a user in advance, and then assigns the second identifier to the second group. A data insertion part(330) inserts the first and second identifiers and the remotely-measured data, which belongs to the second group having the second identifier, into a data field of a transmission frame. A data configuration information insertion part(340) inserts data configuration information about the configuration relation of the data field into a data configuration information field.
Abstract:
A system for determining a satellite orbit in real time by using the observed orbit data and a method thereof are provided to increase the precision when determining the location of a satellite used for processing video data. A system for determining a satellite orbit in real time receives the orbit data, observed through the distance measuring and angle tracking process from a satellite at predetermined time intervals, and stores the received data in a designated directory(S410). A system for determining a satellite orbit in real time performs the following steps of: receiving the orbit data, observed through the distance measuring and angle tracking process from a satellite at predetermined time intervals, and storing the received data in a designated directory; judging whether the received orbit data has defects(S420); generating a dynamics model for the satellite in consideration of the wheel off-loading control and location maintenance control of the satellite, and then generating calculated orbit data based on the dynamics model(S430); and receiving the observed orbit data or determining the orbit of the satellite by the difference between the calculated orbit data and the observed orbit data(S440).
Abstract:
A real time electronic program guide providing system and a method thereof are provided to supply contents information which is generated or upgraded by using SIP to a user, thereby enabling the user to check the contents information in real time. A contents providing server(10) includes generated or upgraded contents information in the first SIP(Session Initiation Protocol) message and transmits the message to an electronic program guide server. A settop box(12) requests transmission of the content information by using the second SIP message. The electronic program guide server registers or upgrades the contents information of the first SIP message and includes the contents information requested by the second SIP message or upgraded information of the requested contents in the third SIP message and transmits the third SIP message to the settop box.
Abstract:
An apparatus and a method for transmitting a satellite command for the acceptance of an urgent observation request are provided to receive an urgent observation request from an observation demander and to transmit the urgent observation request command to a low earth orbit satellite at the communication possible time between the satellite and a ground satellite control system. A collection part(202) collects an observation request inputted from an external observation demander(201), and a mission scheduling part(203) produces a mission schedule according to the management of a satellite and an observation request from the collection part. A satellite command plan part(204) receives the urgent observation request inputted from the observation demander and integrates the received urgent observation request to the previously produced satellite command plan according to the mission schedule from the mission scheduling part so that the integrated command plan is produced. A satellite command generation part(205) generates the satellite command according to the integrated command plan from the satellite command plan part. A satellite command transmission part(206) transmits the satellite command from the satellite command generation part.