月軟着陸技術の研究:月着陸航法誘導技術の研究

Material type: 文書・図像類

Author: 山本, 昌幸ほか

Publisher: 宇宙航空研究開発機構

Publication date: 2004-10-29

Material Format: Digital

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Note (General)：: In order to realize the science missions at the specific point on the moon, SELENE-B is required highly precise and safe landing. This paper shows the...

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Material Type: 文書・図像類
Title: 月軟着陸技術の研究:月着陸航法誘導技術の研究
Author/Editor: 山本, 昌幸
石島, 義之
濱田, 吉郎
二宮, 哲次郎
松本, 甲太郎
四宮, 康雄
澤井, 秀次郎
橋本, 樹明
神谷, 芳和
Yamamoto, Masayuki
Ishijima, Yoshiyuki
Hamada, Yoshiro
Ninomiya, Tetsujiro
Matsumoto, Kotaro
Shinomiya, Yasuo
Sawai, Shujiro
Hashimoto, Tatsuaki
Kamiya, Yoshikazu
Author Heading: 山本, 昌幸
石島, 義之
濱田, 吉郎
二宮, 哲次郎
松本, 甲太郎
四宮, 康雄
澤井, 秀次郎
橋本, 樹明
神谷, 芳和
Yamamoto, Masayuki
Ishijima, Yoshiyuki
Hamada, Yoshiro
Ninomiya, Tetsujiro
Matsumoto, Kotaro
Shinomiya, Yasuo
Sawai, Shujiro
Hashimoto, Tatsuaki
Kamiya, Yoshikazu
Publication, Distribution, etc.: 宇宙航空研究開発機構
Publication Date: 2004-10-29
Publication Date (W3CDTF): 2004-10-29
Alternative Title: Study on lunar soft landing: Study on guidance and navigation for lunar landing
Periodical title: 宇宙航空研究開発機構研究開発資料: 平成15年度総合技術研究本部宇宙領域研究成果報告書:先行研究等 = JAXA Research and Development Memorandum: FY15 Annual Report of Research & Development on Space Technology in the Institute of Space Technology and Aeronautics: Advanced Technology
No. or year of volume/issue: JAXA-RM-04-011
Volume: JAXA-RM-04-011
Pages: 123-128
ISSN (Periodical Title): ISSN : 1349-1121
Text Language Code: jpn
Subject Heading: SELENE-B
月探査
月面軟着陸
航法誘導
高度計
イメージセンサ
障害物回避
シミュレーション
lunar exploration
lunar soft landing
navigation and guidance
altimeter
image sensor
obstacle avoidance
simulation
Target Audience: 一般
Note (General): In order to realize the science missions at the specific point on the moon, SELENE-B is required highly precise and safe landing. This paper shows the result of the guidance and navigation simulation and estimates the landing accuracy. This simulation is combined the navigation law and guidance law. The navigation law is realized by using the image sensor and the altimeter. The guidance law is restricted using the ON/OFF control thruster.
資料番号: AA0048129025
レポート番号: JAXA-RM-04-011
Access Restrictions: 限定公開
Periodical Title (NCID): AA11983593
https://ci.nii.ac.jp/ncid/AA11983593
Data Provider (Database): 国立情報学研究所 : 学術機関リポジトリデータベース（IRDB）（機関リポジトリ）
https://irdb.nii.ac.jp
Original Data Provider (Database): 宇宙航空研究開発機構 : 宇宙航空研究開発機構リポジトリ