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A practical application of accurate non-gravitational disturbance model with pre-computed tensor method

Research Project

Project/Area Number 17H06615
Research Category

Grant-in-Aid for Research Activity Start-up

Allocation TypeSingle-year Grants
Research Field Aerospace engineering
Research InstitutionThe University of Tokyo

Principal Investigator

Ikari Satoshi  東京大学, 大学院工学系研究科(工学部), 助教 (00802977)

Project Period (FY) 2017-08-25 – 2019-03-31
Project Status Completed (Fiscal Year 2018)
Budget Amount *help
¥2,990,000 (Direct Cost: ¥2,300,000、Indirect Cost: ¥690,000)
Fiscal Year 2018: ¥1,560,000 (Direct Cost: ¥1,200,000、Indirect Cost: ¥360,000)
Fiscal Year 2017: ¥1,430,000 (Direct Cost: ¥1,100,000、Indirect Cost: ¥330,000)
Keywords軌道上外乱 / 太陽輻射圧 / 空力外乱 / 熱輻射圧 / 軌道決定 / 精密軌道決定 / 非重力外乱 / 姿勢解析 / 準天頂衛星 / PROCYON / 航空宇宙工学 / 測位衛星
Outline of Final Research Achievements

In order to realize a high-accurate space operation, we have to precisely predict position and attitude behavior of spacecraft. A precise calculation method for small non-gravitational disturbances (e.g., solar radiation pressure, air drag, and so on) is essential for precise prediction of the position and attitude. The author have proposed "pre-computed geometry tensor method" for accurate and quick calculation of solar radiation pressure in the previous research.
This research expanded the proposed method to air drag and thermal radiation pressure calculations. In addition, the proposed method is applied to actual spacecraft analyses by using real observation data to verify the usefulness of the method. The analyses showed that the proposed method can precisely and quickly calculate non-gravitational disturbances in the real problem.

Academic Significance and Societal Importance of the Research Achievements

本研究は,非重力外乱(太陽輻射圧や空力外乱など)という微小な力に焦点を当てている.これらの力は地上では重力や摩擦力に対して小さすぎて無視されているが,宇宙空間では大きな問題となる.一件,社会的意義の小さな研究に見えるが,この微小な力を高精度に計算することで,人間社会で必要不可欠になっているGPSシステムの精度向上につながる.また,将来の高度な宇宙ミッション(宇宙重力波望遠鏡など)を実現するためには,このような微小な力を高精度に計算し,宇宙機の動きを予測する必要がある.
本研究はこの微小な非重力外乱を数値計算上だけでなく,現実的な問題の中で高精度に計算し評価したという点で意義深いといえる.

Report

(3 results)
  • 2018 Annual Research Report   Final Research Report ( PDF )
  • 2017 Annual Research Report
  • Research Products

    (9 results)

All 2019 2018 2017

All Journal Article (2 results) (of which Peer Reviewed: 2 results) Presentation (7 results) (of which Int'l Joint Research: 5 results)

  • [Journal Article] Accurate Aerodynamic Model of Membranes in Free-Molecular Flow for Deorbit Device Design2019

    • Author(s)
      FUNABIKI Nobuhiro、IKARI Satoshi、ISHIKAWA Akihiro、FUNASE Ryu、NAKASUKA Shinichi
    • Journal Title

      TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES, AEROSPACE TECHNOLOGY JAPAN

      Volume: 17 Issue: 2 Pages: 189-196

    • DOI

      10.2322/tastj.17.189

    • NAID

      130007607470

    • Related Report
      2018 Annual Research Report
    • Peer Reviewed
  • [Journal Article] Active use of solar radiation pressure for angular momentum control of the PROCYON micro-spacecraft2018

    • Author(s)
      Ito T.、Ikari S.、Funase R.、Sakai S.、Kawakatsu Y.、Tomiki A.、Inamori T.
    • Journal Title

      Acta Astronautica

      Volume: 152 Pages: 299-309

    • DOI

      10.1016/j.actaastro.2018.08.009

    • Related Report
      2018 Annual Research Report
    • Peer Reviewed
  • [Presentation] Analysis of Disturbance Anomaly of Interplanetary Micro Spacecraft PROCYON2019

    • Author(s)
      Satoshi Ikari, Takaya Inamori, Takahiro Ito, Ryu Funase
    • Organizer
      29th Space Flight Mechanics Meeting
    • Related Report
      2018 Annual Research Report
    • Int'l Joint Research
  • [Presentation] Precise orbit determination of QZSS satellites with high-fidelity non-gravitational disturbance model2018

    • Author(s)
      Satoshi Ikari, Sinichi Nakasuka, Keiji Nakata, Tomohiko Saito, Yasuyuki Watanabe, Isao Kawano, and Yuki Igarashi
    • Organizer
      IGS Workshop 2018
    • Related Report
      2018 Annual Research Report
    • Int'l Joint Research
  • [Presentation] Optical Property Estimation by Precomputed Tensor Method for High-fidelity SRP Model2017

    • Author(s)
      Satoshi Ikari, Kakeru Tokunaga, Takahiro Ito, Takaya Inamori, Ryu Funase, Shinichi Nakasuka
    • Organizer
      31st ISTS, 26th ISSFD, and 8th NSAT
    • Related Report
      2017 Annual Research Report
    • Int'l Joint Research
  • [Presentation] 事前計算形状テンソルを用いた表面外乱の高精度・高速計算手法2017

    • Author(s)
      五十里 哲, 船曳 敦漠, 海老沼 拓史, 船瀬 龍, 中須賀 真一
    • Organizer
      第61回宇宙科学技術連合講演会
    • Related Report
      2017 Annual Research Report
  • [Presentation] 超小型深宇宙探査機PROCYONの軌道上姿勢外乱解析2017

    • Author(s)
      五十里哲、伊藤琢博、阪上遼、松下周平、稲守孝哉、船瀬龍
    • Organizer
      第14回宇宙環境シンポジウム
    • Related Report
      2017 Annual Research Report
  • [Presentation] Estimation of Shape and Optical Parameters of Spinning Solar Sail Equipped with Reflectivity Control Devices2017

    • Author(s)
      Akihiro Ishikawa, Kenshiro Oguri, Satoshi Ikari, Ryu Funase, Shinichi Nakasuka
    • Organizer
      31st ISTS, 26th ISSFD, and 8th NSAT
    • Related Report
      2017 Annual Research Report
    • Int'l Joint Research
  • [Presentation] Accurate Aerodynamic Model for Membranes in Free-Molecular Flow to be Used for Deorbit Device Design2017

    • Author(s)
      Nobuhiro Funabiki, Satoshi Ikari, Shinichi Nakasuka, Ryu Funase, Akihiro Ishikawa
    • Organizer
      31st ISTS, 26th ISSFD, and 8th NSAT
    • Related Report
      2017 Annual Research Report
    • Int'l Joint Research

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Published: 2017-08-25   Modified: 2020-03-30  

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