HISAKI Project Team
  1. 研究者リスト
  2. 坂東 信尚

坂東 信尚

バンドウ ノブタカ  (Nobutaka Bando)

基本情報

所属
国立研究開発法人宇宙航空研究開発機構 宇宙科学研究所 宇宙機応用工学研究系
研究者番号
10415896
J-GLOBAL ID
202001008437142898
researchmap会員ID
R000015178

研究キーワード

 1

研究分野

 1

経歴

 1

論文

 30
  • Junji Kikuchi, Chikako Hirose, Naoki Morishita, Ryo Hirasawa, Kakeru Tokunaga, Nobutaka Bando, Tatsuaki Hashimoto
    Acta Astronautica 213 665-675 2023年12月  
  • Tatsuaki Hashimoto, Junji Kikuchi, Ryo Hirasawa, Kota Miyoshi, Wataru Torii, Naoki Morishita, Nobutaka Bando, Atsushi Tomiki, Shintaro Nakajima, Masatsugu Otsuki, Hiroyuki Toyota, Kakeru Tokunaga, Chikako Hirose, Tetsuo Yoshimitsu, Hiroshi Takeuchi
    Proceedings of the International Astronautical Congress, IAC 2023-October 2023年  
    A 6U CubeSat “OMOTENASHI” was developed to be the world's smallest moon lander. It was launched by NASA's SLS Artemis-1 on November 16, 2022. However, because of the spacecraft anomaly, the battery was depleted and the communication with the spacecraft had been lost. After we gave up the moon landing experiment, we have been conducting a search and rescue operation till September 2023. But it was unsuccessful, unfortunately. In this article, the mission objective, the spacecraft design, the planed mission scenario, and the in-orbit operation results are presented. Additionally, lessons learned from the development and the in-orbit operation are presented.
  • Shuhei Shigeto, Shinji Mitani, Nobutaka Bando, Tatsuaki Hashimoto
    AIAA Scitech 2020 Forum 1 2020年  
    This paper describes a method providing active vibration control of multiple mechanical coolers for space applications. Typical observation satellites have multiple mechanical coolers and their induced micro vibrations degrade pointing accuracy and cooler efficiency. In order to reduce such the vibration, active control is proposed. However, in the conventional control method for mechanical coolers, only considers the vibration of a single cooler and single axis has considered. Here we propose a method to simultaneously control the vibration of a satellite equipped with multiple mechanical coolers. We will discuss the condition of controllability, and actuator position and direction, and present the result of a simulation study.
  • Makoto Tashiro, Hironori Maejima, Kenichi Toda, Richard Kelley, Lillian Reichenthal, Leslie Hartz, Robert Petre, Brian Williams, Matteo Guainazzi, Elisa Costantini, Ryuichi Fujimoto, Kiyoshi Hayashida, Joy Henegar-Leon, Matt Holland, Yoshitaka Ishisaki, Caroline Kilbourne, Mike Loewenstein, Kyoko Matsushita, Koji Mori, Takashi Okajima, F. Scott Porter, Gary Sneiderman, Yoh Takei, Yukikatsu Terada, Hiroshi Tomida, Hiroya Yamaguchi, Shin Watanabe, Hiroki Akamatsu, Yoshitaka Arai, Marc Audard, Hisamitsu Awaki, Iurii Babyk, Aya Bamba, Nobutaka Bando, Ehud Behar, Thomas Bialas, Rozenn Boissay-Malaquin, Laura Brenneman, Greg Brown, Edgar Canavan, Meng Chiao, Brian Comber, Lia Corrales, Renata Cumbee, Cor de Vries, Jan Willem Den Herder, Johannes Dercksen, Maria Diaz-Trigo, Michael DiPirro, Chris Done, Tadayasu Dotani, Ken Ebisawa, Megan Eckart, Dominique Eckert, Satoshi Eguchi, Teruaki Enoto, Yuichiro Ezoe, Carlo Ferrigno, Yutaka Fujita, Yasushi Fukazawa, Akihiro Furuzawa, Luigi Gallo, Nathalie Gorter, Martin Grim, Liyi Gu, Kohichi Hagino, Kenji Hamaguchi, Isamu Hatsukade, David Hawthorn, Katsuhiro Hayashi, Natalie Hell, Junko Hiraga, Edmund Hodges-Kluck, Takafumi Horiuchi, Ann Hornschemeier, Akio Hoshino, Yuto Ichinohe, Sayuri Iga, Ryo Iizuka, Manabu Ishida, Naoki Ishihama, Kumi Ishikawa, Kosei Ishimura, Tess Jaffe, Jelle Kaastra, Timothy Kallman, Erin Kara, Satoru Katsuda, Steven Kenyon, Mark Kimball, Takao Kitaguchi, Shunji Kitamoto, Shogo Kobayashi, Akihide Kobayashi, Takayoshi Kohmura, Aya Kubota, Maurice Leutenegger, Muzi Li, Tom Lockard, Yoshitomo Maeda
    Proceedings of SPIE - The International Society for Optical Engineering 11444 2020年  
    The X-Ray Imaging and Spectroscopy Mission (XRISM) is the successor to the 2016 Hitomi mission that ended prematurely. Like Hitomi, the primary science goals are to examine astrophysical problems with precise high-resolution X-ray spectroscopy. XRISM promises to discover new horizons in X-ray astronomy. XRISM carries a 6 x 6 pixelized X-ray micro-calorimeter on the focal plane of an X-ray mirror assembly and a co-aligned X-ray CCD camera that covers the same energy band over a large field of view. XRISM utilizes Hitomi heritage, but all designs were reviewed. The attitude and orbit control system were improved in hardware and software. The number of star sensors were increased from two to three to improve coverage and robustness in onboard attitude determination and to obtain a wider field of view sun sensor. The fault detection, isolation, and reconfiguration (FDIR) system was carefully examined and reconfigured. Together with a planned increase of ground support stations, the survivability of the spacecraft is significantly improved.
  • Tatsuaki Hashimoto, Junji Kikuchi, Ryo Hirasawa, Naoki Morishita, Nobutaka Bando, Atsushi Tomiki, Wataru Torii, Yuta Kobayashi, Shintaro Nakajima, Masatsugu Otsuki, Tetsuo Yoshimitsu, Tetsuya Yamada, Kota Miyoshi, Hiroyuki Toyota, Kakeru Tokunaga, Chikako Hirose, Toshinori Ikenaga, Aiko Nagamatsu, Hitoshi Morimoto
    Proceedings of the International Astronautical Congress, IAC 2020-October 2020年  
    A 6U CubeSat “OMOTENASHI” will be the world's smallest moon lander which is launched by NASA SLS Artemis-1. Because of its severe mass and size limitation, it will adopt semi-hard landing scheme. That is, OMOTENASHI is decelerated from orbital velocity to less than 50 m/s by a small solid rocket motor and shock absorption mechanism has been developed to withstand the high-speed impact. Ultra small communication system (X-band and P-band) is also developed. It observes radiation environment of Earth and moon region with portable dosimeters. This paper shows the mission outline, the design, and the development results of OMOTENASHI.
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MISC

 47
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書籍等出版物

 1
  • 大内, 正己, 池内, 了, 勝川, 行雄, 川村, 静児, 小久保, 英一郎, 田村, 元秀, 橋本, 樹明, 半田, 利弘, 坂東, 信尚
    小学館 2018年6月 (ISBN: 9784092173095)

講演・口頭発表等

 16
  • Ryo Hirasawaa, Tatsuaki Hashimotob, Kakeru Tokunagab, Nakajima Shintarob, Kota Miyoshi, Chikako Hiroseb, Junji Kikuchi, Nobutaka Bando, Naoki Morishita, Atsushi Tomiki, Wataru Torii, Taichi Itob, Masatsugu Otsukib, Tetsuo Yoshimitsub, Yasuo Ishigeb, Hiroshi Takeuchib, Yukio Yamamotob
    SPACEOPS 2023 the 17th international conference on space operations 2023年3月6日
  • Junji Kikuchi, Chikako Hirose, Naoki Morishita, Ryo Hirasawa, Kakeru Tokunaga, Nobutaka Bando, Tatsuaki Hashimotob
    73rd International Astronautical Congress 2022年9月22日
  • 三桝 裕也, 岩城 拓弥, 宇佐美 尚人, 坂東 信尚, 津田 雄一
    第32回アストロダイナミクスシンポジウム 2022年7月26日
  • Tatsuaki Hashimoto, Junji Kikuchi, Ryo Hirasawa, Shintaro Nakajima, Naoki Morishita, Atsushi Tomiki, Wataru Torii, Masatsugu Otsuki, Tetsuo Yoshimitsu, Yasuo Ishige, Kota Miyoshi, Nobutaka Bando, Chikako Hirose, Hiroshi Takeuchi, Hiroyuki Toyota, Keiichi Hori, Kakeru Tokunaga, Aiko Nagamatsu, Hitoshi Morimoto, Toshinori Ikenaga
    33rd International Symposium on Space Technology and Science 2022年3月1日
  • 平澤 遼, 橋本 樹明, 菊池 隼仁, 徳永 翔, 三好 好太, 中島 晋太郎, 廣瀬 史子, 森下 直樹, 坂東 信尚, 冨木 淳史, 鳥居 航, 大槻 真嗣, 吉光 徹雄, 石毛 康夫
    宇宙科学シンポジウム 2022年1月6日
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所属学協会

 3

共同研究・競争的資金等の研究課題

 3
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