Zobrazeno 1 - 10
of 10
pro vyhledávání: '"OOKAMI, Yoshiaki"'
Publikováno v:
航空宇宙技術研究所資料 = Technical Memorandum of National Aerospace Laboratory. 636:15
本資料は剛体の運動方程式におけるクオータニオンによるキネマティックス表現についてまとめたものである。クオータニオンは4つのパラメータで構成され,物体のオリエンテーション
Autor:
Ookami, Yoshiaki, Yoshimura, Shoichi, Kida, Takashi, Yamaguchi, Isao, Tsuchiya, Kazuo, Yamada, Katsuhiko
Publikováno v:
航空宇宙技術研究所特別資料 = Special Publication of National Aerospace Laboratory SP-4. 4:HYS1-91
Formulation of multibody dynamics is one of the key issues in developing a computer simulation program for analysis of orbital and attitude dynamics of complex spacecraft or large flexible structures. This survey study reviews representative research
Publikováno v:
航空宇宙技術研究所資料 = Technical Memorandum of National Aerospace Laboratory. 338:25
資料番号: NALTM0338000
レポート番号: NAL TM-338
レポート番号: NAL TM-338
Publikováno v:
航空宇宙技術研究所報告 = Technical Report of National Aerospace Laboratory TR-633. 633:21
This paper presents the analysis and evaluation of a conical scanning earth sensor which detects the infrared (14-16μm, CO2 absorption bands) radiation of the earth. This type of sensor is widely used as a basic roll/pitch attitude reference for a t
Publikováno v:
航空宇宙技術研究所資料 = Technical Memorandum of National Aerospace Laboratory. 304:23
資料番号: NALTM0304000
レポート番号: NAL TM-304
レポート番号: NAL TM-304
Autor:
YAMAGUCHI, Isao, OOKAMI, Yoshiaki, OKAMOTO, Osamu, KIDA, Takashi, AKIMOTO, Toshio, WAKABAYASHI, Yasushi
Publikováno v:
航空宇宙技術研究所報告 = Technical Report of National Aerospace Laboratory TR-947. 947:104
An Earth sensor utilizing infrared (IR) horizon radiation is one of the fundamental attitude sensors for three-axis attitude stabilized spacecraft. The attitude measurement accuracy of this type of sensor greately depends on the variation of the IR r
Autor:
LSS定式化手法調査チーム, Ookami, Yoshiaki, Yoshimura, Shoichi, Kida, Takashi, Yamaguchi, Isao, Tsuchiya, Kazuo, Yamada, Katsuhiko
Publikováno v:
航空宇宙技術研究所特別資料 = Special Publication of National Aerospace Laboratory SP-4. 4:91
Formulation of multibody dynamics is one of the key issues in developing a computer simulation program for analysis of orbital and attitude dynamics of complex spacecraft or large flexible structures. This survey study reviews representative research
Publikováno v:
航空宇宙技術研究所報告 = Technical Report of National Aerospace Laboratory TR-803. 803:40
This paper presents some results of the vibration analysis for simplified models of a multipurpose geostationary platform. The analysis approach is based on the energy method that has been applied by one of authors using assumed mode functions for th
Publikováno v:
航空宇宙技術研究所資料 = Technical Memorandum of National Aerospace Laboratory. 388:19
資料番号: NALTM0388000
レポート番号: NAL TM-388
レポート番号: NAL TM-388
Autor:
MURAKAMI, Chikara, OOKAMI, Yoshiaki
Publikováno v:
航空宇宙技術研究所資料 = Technical Memorandum of National Aerospace Laboratory. 207:17
資料番号: NALTM0207000
レポート番号: NAL TM-207
レポート番号: NAL TM-207