Výsledky vyhledávání - "軌道解析"

ミジカナユウグトウノコウガクテキカイセキ (ソノ 2 : バドミントンヨウシャトルコックノダイナミクス)

Publikováno v: 千葉大学教育学部研究紀要 = Bulletin of the Faculty of Education, Chiba University. 61:463-471

バドミントンには,オリンピック正式種目としての「競技」である面と,ラケットとシャトルコックさえあれば小さい子どもからお年寄りまで,誰でも気軽に楽しめる「遊戯」としての一面�

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::d476705e5ab137d261e0ecf369436116
http://opac.ll.chiba-u.jp/da/curator/900116881/

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ミジカナユウグトウノコウガクテキカイセキ (ソノ 2 : バドミントンヨウシャトルコックノダイナミクス)

Publikováno v: 千葉大学教育学部研究紀要 = Bulletin of the Faculty of Education, Chiba University. 61:463-471

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::e02703bf82ce05b2c238bd867f188497
https://opac.ll.chiba-u.jp/da/curator/900116881/

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Influence of the finite duration on a fly-by

Autor: Janssens, Frank

Publikováno v: 第17回アストロダイナミクスシンポジウム講演後刷り集 2007 = Proceedings of 17th Workshop on JAXA Astrodynamics and Flight Mechanics. :69-83

Patched conics is the standard tool for designing fly-by or gravity assist maneuvers performed by a spacecraft about a planet. In this procedure, the trajectory of the spacecraft about the planet is taken as a perfect hyperbola once the spacecraft is

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::9044c2ba965844fdad3a386d0dd9da18
http://id.nii.ac.jp/1696/00007444/

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次期小惑星探査ミッションはやぶさ2のミッション解析

Autor: Kawakatsu, Yasuhiro, Abe, Masanao, Kawaguchi, Junichiro

Publikováno v: 第17回アストロダイナミクスシンポジウム講演後刷り集 2007 = Proceedings of 17th Workshop on JAXA Astrodynamics and Flight Mechanics. :293-298

「はやぶさ(MUSES-C: Asteroid Sample-return Spacecraft)」のITOKAWA接近運用の結果を受け、次の小天体探査ミッションについては、他国に先駆けて、できるだけ早い時期に小天体からのサンプルリタ�

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::9fe4411e4fe2c60e9d63b39487e5ab89
http://id.nii.ac.jp/1696/00007479/

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A study of capture trajectories to the vicinity of L1 and L2 points

Autor: Scheeres, Daniel, Nakamiya, Masaki, Yamakawa, Hiroshi, Yoshikawa, Makoto

Publikováno v: 第17回アストロダイナミクスシンポジウム講演後刷り集 2007 = Proceedings of 17th Workshop on JAXA Astrodynamics and Flight Mechanics. :63-68

We investigate spacecraft capture trajectories to the periodic orbits of the L1 and L2 points in the planar restricted Hill three-body problem are studied. The specific focus is on transfer to these vicinities from interplanetary trajectories. This a

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::e87369b6b71d9eb55cf80045385a5a88
http://id.nii.ac.jp/1696/00007443/

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MUSCAT技術によるビームイオン軌道解析

Autor: Kim, Jongho, Cho, Mengu, Hatta, Shinji, Muranaka, Takanobu, Hosoda, Satoshi

Publikováno v: 宇宙航空研究開発機構特別資料: イオン加速グリッド耐久認定用数値解析JIEDI(JAXA Ion Engine Development Initiatives)ツールの研究開発ワークショップ 2006年度報告書 = JAXA Special Publication: Annual Report of Workshop on Research and Development of JIEDI (JAXA Ion Engine Development Initiatives) Tool for Numerical Evaluation of Ion Engine Grid Lifetime, FY2006. :64-71

Multi-Utility Spacecraft Charging Analysis Tool (MUSCAT) is a software under development by Kyushu Institute of Technology (KIT) jointly with JAXA. Its numerical engine is a plasma simulator based on particle method. It includes both Particle Trackin

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::7778b35b1667a0e363f21033a53bb539
http://id.nii.ac.jp/1696/00005846/

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Technical issues associated with the development of the JIEDI tool and plan for 2007

Autor: Funaki, Ikko, Nakano, Masakatsu, Nakayama, Yoshinori, Kajimura, Yoshihiro

A two-year plan for the development of the first stage of the JIEDI tool (JAXA Ion Engine Development Initiative 1, JIEDI-1) is proposed. In order to circumvent the heavy calculation cost associated with the three-dimensional analysis of multiple hol

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::1c2663636751dd93d3841f16213015c6
http://id.nii.ac.jp/1696/00005847/

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The Real Time Trajectory Estimation Program (RTEP): Overview and experience results

Autor: Ogawa, Mina, Iwana, Yasunori, Taniguchi, Sho, Nakajima, Ken, Hotta, Manabu, Hirota, Masao

Publikováno v: 宇宙航空研究開発機構特別資料: 先進的軌道計測・決定技術に関する研究会論文集 = JAXA Special Publication: Proceedings of Advanced Orbit Measurement and Orbit Calculation Technologies. :59-68

The Real Time Trajectory Estimation Program (RTEP) is JAXA's system for estimating a satellite's trajectory and thrust acceleration based on the Kalman filter during the Apogee Engine Firing (AEF). RTEP has been used during the AEFs of, ETS (Engineer

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::60b368402269bde22b176aa4f8ea54a9
http://id.nii.ac.jp/1696/00005890/

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J2摂動下での、任意の衛星編隊形状維持のための必要最小燃料の導出

Autor: Nagai, Masaki, Nakasuka, Shinichi

Publikováno v: 第16回アストロダイナミクスシンポジウム講演後刷り集 2006 = Proceedings of 16th Workshop on JAXA Astrodynamics and Flight Mechanics. :7-12

衛星の小型化、高性能化が進む中、編隊飛行、母衛星監視飛行といった衛星協調ミッションが注目されている。そこで相対位置制御技術が必要となるが、その燃料消費が衛星重量やコス�

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::ace36d0f62248200dc6d259dd26d7609
http://id.nii.ac.jp/1696/00007497/

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軌道上レーザー源を想定したレーザー推進宇宙機の軌道ダイナミクスについて

Autor: Yamakawa, Hiroshi, Funaki, Ikko

Publikováno v: 第16回アストロダイナミクスシンポジウム講演後刷り集 2006 = Proceedings of 16th Workshop on JAXA Astrodynamics and Flight Mechanics. :28-31

地球周回低軌道上にレーザー源を想定し、そのレーザーを受けることにより加速される宇宙機の軌道ダイナミクスについて考察する。Clohessy-Wiltshire方程式を用いて、積分量としての仮想�

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::fb6309acb2f51a161122df0c29617afe
http://id.nii.ac.jp/1696/00007500/

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