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デブリ除去衛星のシステム検討デブリ除去衛星のシステム検討AA11800503
System Design of Active Space Debris Removal Satellite |
"/大塚, 聡子/"大塚, 聡子 ,
"/桑尾, 文博/"桑尾, 文博 ,
"/鈴木, 哲明/"鈴木, 哲明 ,
"/廣田, 賢治/"廣田, 賢治 ,
"/渡辺, 順一郎/"渡辺, 順一郎 ,
"/河本, 聡美/"河本, 聡美 ,
"/青山, 順一/"青山, 順一 ,
"/山元, 透/"山元, 透 ,
"/村上, 尚美/"村上, 尚美 ,
"/中島, 悠/"中島, 悠 ,
"/Otsuka, Akiko/"Otsuka, Akiko ,
"/Kuwao, Fumihiro/"Kuwao, Fumihiro ,
"/Suzuki, Tetsuaki/"Suzuki, Tetsuaki ,
"/Hirota, Kenji/"Hirota, Kenji ,
"/Watanabe, Junichiro/"Watanabe, Junichiro ,
"/Kawamoto, Satomi/"Kawamoto, Satomi ,
"/Aoyama, Jun-ichi/"Aoyama, Jun-ichi ,
"/Yamamoto, Toru/"Yamamoto, Toru ,
"/Murakami, Naomi/"Murakami, Naomi ,
"/Nakajima, Yu/"Nakajima, Yu
2015-10-07 , 日本航空宇宙学会(JSASS) , The Japan Society for Aeronautical and Space Sciences (JSASS)
NII書誌ID(NCID):AA11800503
内容記述
System design of Active Space Debris Removal (ADR) Satellite will be presented. The ADR Satellite equipped with the extension arm will grapple the upper stage of rocket and de-orbit it using Electrodynamic Tether (EDT). Through the research on the scenario of ADR mission, the roles of the ground control and the on-orbit control are specified and the measures to secure the resource during the ground control are clarified. The ADR satellite will approach to the debris using the information by the navigation sensors such as visible cameras and Infra-Red (IR) cameras. The algorithm for processing the camera images was designed and the simulation results of estimating the distance and attitude of the debris by processing the camera images of the rocket upper stage scale model are presented.
会議情報: 第59回宇宙科学技術連合講演会（2015年10月7日-9日. かごしま県民交流センター), 鹿児島市, 鹿児島県
形態: カラー図版あり
Physical characteristics: Original contains color illustrations
