发明名称 Apparatus and method for controlling geostationary orbit satellite
摘要 An apparatus and method for controlling a geostationary orbit satellite is provided. The method including generating remote measurement data by measuring a state of a geostationary orbit satellite, transmitting the remote measurement data, receiving a remote command signal, and controlling an orbit and a pose of the geostationary orbit satellite relative to inclined geosynchronous space debris.
申请公布号 US9399527(B2) 申请公布日期 2016.07.26
申请号 US201313913005 申请日期 2013.06.07
申请人 Electronics and Telecommunications Research Instit 发明人 Lee Byoung Sun;Hwang Yoo La
分类号 B64G1/24;B64G1/10;B64G1/00;B64G1/52 主分类号 B64G1/24
代理机构 William Park & Associates Ltd. 代理人 William Park & Associates Ltd.
主权项 1. An apparatus for controlling a geostationary orbit satellite, the apparatus comprising: a data processing unit to generate remote measurement data by measuring a state of a geostationary orbit satellite; a signal transmitting/receiving unit to receive a remote command signal and to transmit the remote measurement data; and a satellite control unit to control an orbit and a pose of the geostationary orbit satellite relative to inclined geosynchronous space debris, wherein the geostationary orbit satellite is maintained at a predetermined safe distance from the inclined geosynchronous space debris when the inclined geosynchronous pace debris passes through an equatorial plane of earth, wherein the satellite control unit controls a radial separation between the geostationary orbit satellite and the inclined geosynchronous space debris to maintain the predetermined safe distance for collision avoidance when the inclined geosynchronous space debris passes through the equatorial plane of the Earth, and wherein the satellite control unit adjusts a velocity of the geostationary orbit satellite to maintain the predetermined safe distance for collision avoidance between the geostationary orbit satellite and the inclined geosynchronous space debris.
地址 Daejeon KR