親機子機分離着陸機構を用いた月惑星探査機の2次元応答解析

• 原 進

  名古屋大学大学院工学研究科

• 石川 凌

  名古屋大学大学院工学研究科

• 大槻 真嗣

  宇宙航空研究開発機構宇宙科学研究所

書誌事項

タイトル別名

• Two-dimensional Response Analysis of Lunar/Planetary Spacecraft by Means of Base-extension Separation Landing Mechanism
• シンキコキ ブンリ チャクリク キコウ オ モチイタ ツキ ワクセイ タンサキ ノ 2ジゲン オウトウ カイセキ

抄録

Next-generation lunar/planetary exploration spacecraft need to solve problems of conventional landing methods and mechanisms such as high rebound, impossibility of reuse and high cost. For this purpose, the authors discuss the landing method by means of Base-Extension Separation landing Mechanism (BESM) which uses energy conversion with springs and separable units. In conventional studies, its effectiveness was confirmed for a simple case based on single-axis restriction. However, the investigation of tumble prevention cannot be treated in the simple case. The purpose of this paper is the response analysis with a double-axis case and to discuss the robustness of BESM for more practical landing situations.

収録刊行物

• 計測自動制御学会論文集

  計測自動制御学会論文集 51 (7), 515-517, 2015

  公益社団法人 計測自動制御学会

キーワード

• shock
• energy conversion
• landing
• spacecraft
• tumble prevention

詳細情報

• CRID: 1390001204509863808
• NII論文ID: 130005092298
• NII書誌ID: AN00072392
• DOI: 10.9746/sicetr.51.515
• ISSN: 18838189
• ISSN: 04534654
• NDL書誌ID: 026618411
• Web Site: https://ndlsearch.ndl.go.jp/books/R000000004-I026618411
• Web Site: https://www.jstage.jst.go.jp/article/sicetr/51/7/51_515/_pdf
• 本文言語コード: ja
• データソース種別:
  • JaLC
  • NDL
  • Crossref
  • CiNii Articles
  • KAKEN
• 抄録ライセンスフラグ: 使用不可