タイトル | 超小型深宇宙探査機PROCYONにおける姿勢系FDIRアルゴリズムの軌道上実証結果 |
その他のタイトル | In Orbit Demonstration of a FDIR Algorithm for the Attitude Control System of Micro Interplanetary Spacecraft PROCYON |
DOI | info:doi/10.2322/jjsass.68.89 |
著者(日) | 五十里, 哲; 伊藤, 琢博; 小栗, 健士朗; 稲守, 孝哉; 坂井, 真一郎; 川勝, 康弘; 冨木, 淳史; 船瀬, 龍 |
著者(英) | Ikari, Satoshi; Ito, Takahiro; Oguri, Kenshiro; Inamori, Takaya; Sakai, Shinichiro; Kawakatsu, Yasuhiro; Tomiki, Atsushi; Funase, Ryu |
著者所属(日) | 東京大学; 宇宙航空研究開発機構宇宙科学研究所(JAXA)(ISAS); University of Colorado Boulder; 名古屋大学; 宇宙航空研究開発機構宇宙科学研究所(JAXA)(ISAS); 宇宙航空研究開発機構宇宙科学研究所(JAXA)(ISAS); 宇宙航空研究開発機構宇宙科学研究所(JAXA)(ISAS); 東京大学 |
著者所属(英) | The University of Tokyo; Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA)(ISAS); University of Colorado Boulder; Nagoya University; Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA)(ISAS); Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA)(ISAS); Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA)(ISAS); The University of Tokyo |
発行日 | 2020-04-05 |
発行機関など | 日本航空宇宙学会 Japan Society for Aeronautical and Space Sciences |
刊行物名 | 日本航空宇宙学会論文集 Journal of the Japan Society for Aeronautical and Space Sciences |
巻 | 68 |
号 | 2 |
開始ページ | 89(33) |
終了ページ | 95(39) |
刊行年月日 | 2020-04-05 |
言語 | jpn eng |
抄録 | A Fault Detection, Isolation, and Recovery (FDIR) algorithm for attitude control systems is a key technology to increasing the reliability and survivability of spacecraft. Micro/nano interplanetary spacecraft, which are rapidly evolving in recent years, also require robust FDIR algorithms. However, the implementation of FDIR algorithms to these micro/nano spacecraft is difficult because of the limitations of their resources (power, mass, cost, and so on). This paper shows a strategy of how to construct a FDIR algorithm in the limited resources, taking examples from micro deep space probe PROCYON. The strategy focuses on function redundancies and multi-layer FDIR. These ideas are integrated to suit the situation of micro/nano interplanetary spacecraft and demonstrated in orbit by the PROCYON mission. The in-orbit results are discussed in detail to emphasize the effectiveness of the FDIR algorithm. |
内容記述 | 形態: 図版あり 著者名の誤記: 坂井, 信一郎 Physical characteristics: Original contains illustrations The clerical error of an author's name: 坂井, 信一郎 |
キーワード | FDIR; Interplanetary Micro-Spacecraft; Attitude Determination and Control |
資料種別 | Journal Article |
NASA分類 | Spacecraft Design, Testing and Performance |
ISSN | 1344-6460 |
ISSN(online) | 2432-3691 |
NCID | AA11307372 |
SHI-NO | AA2040002005 |
URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/955566 |