Výsledky vyhledávání - "衛星誘導"

Autor: Morita, Hideo, Shirakawa, Kenichi, Kubota, Takashi, Hashimoto, Tatsuaki, Kawaguchi, Junichiro

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. :173-178

2005年11月、はやぶさ(MUSES-C: Asteroid Sample-return Spacecraft)は小惑星'いとかわ'へ5回の接近誘導を実施した。期待に反し、'いとかわ'表面はごつごつした岩で覆われ、はやぶさが安全にタッチダ

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::6d865681e2a8a4025b830460586df6af
http://id.nii.ac.jp/1696/00007525/

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インターセプタを用いた小天体フライバイのための統合型航法誘導制御

Autor: Mori, Osamu, Tarao, Kota

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. :127-132

ISAS/JAXAでは超小型探査機「インターセプタ」を用いた小天体のフライバイミッションを計画している。本計画は「のぞみ(PLANET-B: Mars Orbiter)」のフライバイと異なり、積極的に近接点を通�

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http://id.nii.ac.jp/1696/00007518/

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はやぶさ探査機の降下着陸フェーズにおける航法誘導制御のフライト結果

Autor: Kubota, Takashi, Hashimoto, Tatsuaki, Tamura, Makoto, Bando, Nobutaka, Uo, Masashi, Shirakawa, Kenichi, Morita, Hideo, Kominato, Takashi, Kawaguchi, Junichiro

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. :139-144

2003年5月9日に打ち上げた小惑星探査機「はやぶさ(MUSES-C: Asteroid Sample-return Spacecraft)」は、2005年9月12日に小惑星イトカワ(1998SF36)に到着し、小惑星の科学観測およびグローバルマッピングの

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http://id.nii.ac.jp/1696/00007520/

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Study on the navigation laser sensor for HTV rendezvous mission

Autor: Oda, Mitsushige, Ishijima, Yoshiyuki, Komatsu, Shigenori, Yamamoto, Toru, Mitani, Shinji

Publikováno v: 宇宙航空研究開発機構特別資料: 平成18年度宇宙航空研究開発機構総合技術研究本部宇宙科学研究本部研究成果報告書 = JAXA Special Publication: Report on Research Achievements for FY2006 Institute of Space and Astronautical Science, Institute of Aerospace Technology, Japan Aerospace Exploration Agency. :341-346

A rendezvous navigation sensor, which measures and estimates relative range and LOS (Line of Sight) angle, is a critical component for on-orbit servicing missions and inter-satellite ranging for formation flying. The medium-range rendezvous laser sen

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http://id.nii.ac.jp/1696/00006051/

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Study on an advanced reaction wheel with high performance: Study on improvement for guidance and control actuators/sensors

Autor: Izawa, Katsuhiko, Ichikawa, Shinichiro

We started developing an advanced reaction wheel based on a study for a reaction wheel with high torque and low disturbance characteristics since FY2001. The advanced reaction wheel is characterized by small and high performance in comparison with a

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::dd0245ea19c9c683d7c357160339e5fc
http://id.nii.ac.jp/1696/00006049/

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複数近接宇宙機の区分線形2次制御

Autor: Umehara, Hiroaki

Publikováno v: 第15回アストロダイナミクスシンポジウム講演後刷り集 2005 = Proceedings of 15th Workshop on JAXA Astrodynamics and Flight Mechanics. :55-60

複数の人工衛星が地球周回軌道の1部を囲む有界領域を航行させるためのニアミス回避・燃費低減・自動制御を満たす軌道誘導則は線形力学であるにもかかわらず未だ構成されていない。

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http://id.nii.ac.jp/1696/00007569/

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Study on an advanced reaction wheel with high performance: Study on improvement for guidance and control actuators/sensors

Autor: Izawa, Katsuhiko, Ichikawa, Shinichiro, Sato, Makoto, Obara, Shingo, Sasaki, Akira

Publikováno v: 宇宙航空研究開発機構特別資料: 平成16年度総合技術研究本部宇宙領域宇宙科学研究本部合同研究成果報告書:人工衛星系基盤技術 = JAXA Special Publication: FY2004 Report of Joint Research Achievements of the Space Division of Institute of Aerospace Technology and Institute of Space and Astronautical Science: Basic Technologies of Satellite Systems. :237-240

We started developing an advanced reaction wheel based on a study for a reaction wheel with high torque and low disturbance characteristics since FY13. The advanced reaction wheel is characterized by small and high performance in comparison with a cu

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::494a802fca735617023f346d5c13667c
http://id.nii.ac.jp/1696/00006298/

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Study on a new generation spaceborne GPS receiver

Autor: Suzuki, Hideto, Ishijima, Yoshiyuki, Yamamoto, Toru, Ito, Toshio

A spaceborne GPS receiver is a very useful component which enhances the autonomy of a next generation spacecraft; consequently the requirements for receivers are getting more advanced. Moreover, because of GPS modernization, new civil signals on L2 a

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http://id.nii.ac.jp/1696/00006299/

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Development strategy of lunar surface exploring technologies and its demonstration plan using a small explorer

Autor: Hashimoto, Tatsuaki, Sawai, Shujiro, Mizuno, Takahide, Kubota, Takashi

Publikováno v: 第5回宇宙科学シンポジウム = Proceedings of the 5th Space Science Symposium. :157-160

資料番号: AA0049122037

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::754ccb6618b915059b68f3d8e7cafdf2
http://id.nii.ac.jp/1696/00011285/

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Consideration about the system of intelligent interceptor

Autor: Mori, Osamu, Tarao, Kota, Kawakatsu, Yasuhiro, Tsuda, Yuichi, Kawaguchi, Junichiro

Publikováno v: 第5回宇宙科学シンポジウム = Proceedings of the 5th Space Science Symposium. :364-367

太陽系の彗星・小惑星などの小天体は軌道が確定しているものだけでも30数万個存在している。太陽系の起源や進化を知るためには、代表的な小天体にランデブして、重点的に調査する�

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::b87344914623f90653636723609e024e
http://id.nii.ac.jp/1696/00011338/

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