@inproceedings{oai:jaxa.repo.nii.ac.jp:00007526,
 author = {久保田, 孝 and 橋本, 樹明 and 田村, 誠 and 坂東, 信尚 and 卯尾, 匡史 and 白川, 健一 and 森田, 秀郎 and 小湊, 隆 and 川口, 淳一郎 and Kubota, Takashi and Hashimoto, Tatsuaki and Tamura, Makoto and Bando, Nobutaka and Uo, Masashi and Shirakawa, Kenichi and Morita, Hideo and Kominato, Takashi and Kawaguchi, Junichiro},
 book = {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},
 month = {Mar},
 note = {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後、11月にサンプル採取のためのタッチダウンを2回遂行した。はやぶさ探査機には、画像処理、自動化自律化機能など、広い意味でさまざまなロボティクス技術が盛り込まれている。本発表では、「はやぶさ」の降下・タッチダウンフェーズにおける航法誘導制御のフライト結果について報告する。, The Japanese asteroid exploration spacecraft Hayabusa (MUSES-C: Asteroid Sample-return Spacecraft) autonomously performed touchdown two times in November 2005. The autonomous guidance and navigation capability is installed aboard the spacecraft. The GNC (Guidance, Navigation and Control) system collects the laser altimeter, laser range finders and navigation cameras information aboard and is designed to estimate where the spacecraft is and to decide the path correction maneuvers. The programmed function includes the image processing designed to detect an artificial target marker location to approach and cancel the relative velocity. A terrain alignment maneuver is also accomplished by both altitude and attitude control. This paper presents how autonomous guidance and navigation was performed in Hayabusa mission., 資料番号: AA0063481025},
 pages = {139--144},
 publisher = {宇宙航空研究開発機構宇宙科学研究本部, Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA/ISAS)},
 title = {Flight results on GNC in final descent phase for Hayabusa touchdown},
 year = {2007}
}