惑星分光観測衛星プロジェクトチーム
  1. 研究者リスト
  2. 楠本 哲也

楠本 哲也

クスモト テツヤ  (Tetsuya Kusumoto)

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 プロジェクト研究員
J-GLOBAL ID
202201003026553270
researchmap会員ID
R000032272

論文

 4
  • Tetsuya Kusumoto, Shun Yasuda, Yoshiki Sugawara, Osamu Mori
    Acta Astronautica 223 36-48 2024年10月  査読有り筆頭著者
  • Toshihiro CHUJO, Yuki KUBO, Tetsuya KUSUMOTO
    Journal of Evolving Space Activities 2023年  査読有り
  • Tetsuya Kusumoto, Osamu Mori, Shota Kikuchi, Yuki Takao, Naoko Ogawa, Takanao Saiki, Yuichi Tsuda
    Journal of Spacecraft and Rockets 1-11 2021年10月29日  査読有り筆頭著者
    Deployable payloads have been used to expand mission opportunities and enable autonomous navigation and guidance under uncertain terrain conditions. A spacecraft may deploy an artificial marker toward the surface of the target body. An estimation of the deployment trajectory of markers can provide important information for guidance and navigation. We propose a method estimating the deployment trajectory using only images and evaluate its accuracy and reliability. In addition, to determine the spacecraft's relative attitude with respect to the asteroid surface, we introduce an attitude estimation method using the spacecraft's own shadow. The results shown in this paper confirm that the estimated trajectory is sufficiently accurate and thus the proposed method is a viable option for future missions for determining the trajectory of deployable payloads using only images of a deployment.
  • Shota Kikuchi, Naoko Ogawa, Osamu Mori, Takanao Saiki, Yuto Takei, Fuyuto Terui, Go Ono, Yuya Mimasu, Kent Yoshikawa, Stefaan Van Wal, Hiroshi Takeuchi, Hitoshi Ikeda, Atsushi Fujii, Yuki Takao, Tetsuya Kusumoto, Naru Hirata, Naoyuki Hirata, Kei Shirai, Toru Kouyama, Shingo Kameda, Manabu Yamada, Satoru Nakazawa, Makoto Yoshikawa, Satoshi Tanaka, Seiji Sugita, Sei-ichiro Watanabe, Yuichi Tsuda
    Icarus 358 114220-114220 2021年4月  査読有り

MISC

 1
  • Tetsuya Kusumoto, Yuki Takao, Osamu Mori, Junichiro Kawaguchi
    Proceedings of the International Astronautical Congress, IAC 2020-October 2020年10月  
    Copyright © 2020 by the International Astronautical Federation (IAF). All rights reserved. The removal of space debris from an orbit is one of the definitive solutions to the increasing Earth-orbiting satellites issue. To achieve active removal of space debris, accurate estimation of the state of motion of the target is crucial. In addition to that, a safe approach is preferable. Many strategies have been proposed for estimation of motion of a non-cooperative target, but there are still problems with regards to conducting precise, robust and cost-effective estimation in real-time. This study proposes a new strategy to solve this issue - a real-time and practical method based on optical navigation around small bodies. A computer simulation results show the efficacy of the proposed method and verifies that it can be a viable option for use in the capture of non-cooperative space debris targets.
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