Zobrazeno 1 - 10
of 37
pro vyhledávání: '"振動試験"'
Publikováno v:
日本建築学会構造系論文集. 80(713):1045-1053
This paper presents a method of evaluating local damage in steel beam-column connections using dynamic strain responses measured under ambient vibrations. In the proposed method, inner-force distribution in steel beam-column connection was estimated
Publikováno v:
都市・建築学研究. 22:57-64
Generally, a transmission tower is designed statically based on Japanese civil standard: Design Standard on Structures for Transmission, JEC127-(1979). However a special tower, e.g. very high tower and a tower under gusty wind, is designed dynamicall
Autor:
Sotozaki, Tokuo, Ueda, Tetsuhiko
Publikováno v:
航空宇宙技術研究所資料 = Technical Memorandum of National Aerospace Laboratory. 732:1-11
動的変位計測装置を用いて経年機(FA-200-180型)の全機地上振動試験を行った。機体は、航空大学校で約12,000時間の飛行訓練に使用されたものである。試験は、2点相関ランダム加振による伝
Publikováno v:
都市・建築学研究. 14:87-94
A hanging jumper beam of a transmission tower is adopted as a countermeasure against a short fault of jumper conductors under strong winds. However it is thought that the hanging jumper beam may cause the vibration of transmission tower members due t
Publikováno v:
都市・建築学研究. 13:33-40
The vibration measurement of a structure requires considerable labor for installing not a few signal cables in the structure, and it is difficult to deal quickly with the unexpected change of circumstances like the change of a typhoon path. It is obv
Autor:
Toshio Kamiya
Publikováno v:
IFAC Proceedings Volumes. 40:509-514
衛星内部に存在する各種の振動擾乱源の中でも擾乱レベルが高く、衛星システム設計の際の擾乱管理対象として注意が必要なステッピングモータ駆動系について、モータ駆動時に発生す
Autor:
Kunimori, Hiroo
Publikováno v:
第7回宇宙科学シンポジウム = Proceedings of the 7th Space Science Symposium. :741-750
資料番号: AA0063354024
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. :27-32
The Space Technology Demonstration Research Center has conducted the research on a next-generation technology for micro-satellite since 2002. As a part of this research, an experimental manufacture, various test and evaluation of small satellites ins
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. :325-329
Pointing Accuracy of sensors and stability of attitude control of spacecraft are influenced by micro-vibration transmitted from components, for example, reaction wheels and coolers, which are regarded as internal disturbance sources. Such micro-vibra
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. :285-290
The Japan Aerospace Exploration Agency (JAXA) is now developing a 20N-class thruster valve for spacecraft propulsion systems. We intend to develop this valve with the high reliability, and a robust and durable design. The suspended armature type was