研究者業績

尾崎 直哉

オザキ ナオヤ  (Naoya Ozaki)

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 准教授
総合研究大学院大学 先端学術院 宇宙科学コース 准教授
学位
博士(工学)(東京大学)

研究者番号
90836222
ORCID ID
 https://orcid.org/0000-0002-8445-1575
J-GLOBAL ID
201801006720467786
Researcher ID
GXH-5604-2022
researchmap会員ID
B000312477

論文

 61

MISC

 50
  • Takayuki Hosonuma, Takeshi Miyabara, Naoya Ozaki, Ko Ishibashi, Yuta Suzaki, Peng Hong, Masayuki Ohta, Takeshi Takashima
    2025年4月2日  
    DESTINY+ is an upcoming JAXA Epsilon medium-class mission to flyby multiple asteroids including Phaethon. As an asteroid flyby observation instrument, a telescope mechanically capable of single-axis rotation, named TCAP, is mounted on the spacecraft to track and observe the target asteroids during flyby. As in past flyby missions utilizing rotating telescopes, TCAP is also used as a navigation camera for autonomous optical navigation during the closest-approach phase. To mitigate the degradation of the navigation accuracy, past missions performed calibration of the navigation camera's alignment before starting optical navigation. However, such calibration requires significant operational time to complete and imposes constraints on the operation sequence. From the above background, the DESTINY+ team has studied the possibility of reducing operational costs by allowing TCAP alignment errors to remain. This paper describes an autonomous optical navigation algorithm robust to the misalignment of rotating telescopes, proposed in this context. In the proposed method, the misalignment of the telescope is estimated simultaneously with the spacecraft's orbit relative to the flyby target. To deal with the nonlinearity between the misalignment and the observation value, the proposed method utilizes the unscented Kalman filter, instead of the extended Kalman filter widely used in past studies. The proposed method was evaluated with numerical simulations on a PC and with hardware-in-the-loop simulation, taking the Phaethon flyby in the DESTINY+ mission as an example. The validation results suggest that the proposed method can mitigate the misalignment-induced degradation of the optical navigation accuracy with reasonable computational costs suited for onboard computers.
  • Shota Ito, Hironori Sahara, Naoya Ozaki, Dario Izzo
    AAS/AIAA Space Flight Mechanics Meeting 2025年1月  
  • Risa Ito, Naoya Ozaki
    AAS/AIAA Space Flight Mechanics Meeting 2025年1月  最終著者
  • Akira Hatakeyama, Shota Ito, Toshihiko Yanase, Naoya Ozaki
    AAS/AIAA Space Flight Mechanics Meeting 2025年1月  最終著者
  • Ryo Yasufuku, Yasuhiro Kawakatsu, Naoya Ozaki
    AAS/AIAA Space Flight Mechanics Meeting 2025年1月  最終著者

主要なWorks(作品等)

 4

主要な共同研究・競争的資金等の研究課題

 8

メディア報道

 3