JAXA Repository / AIREX 未来へ続く、宙(そら)への英知

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title宇宙テザー張力と速度の非接触計測法の検討
Other TitleAn examination contact less measurement method of space tether tension and velocity
Author(jpn)皆川 洋平; 藤井 裕矩; 草谷 大郎; 渡部 武夫; 小島 幸高; 中野 美琴
Author(eng)Minagawa, Yohei; Fujii, Hironori A.; Kusagaya, Tairo; Watanabe, Takeo; Kojima, Yukitaka; Nakano, Mikoto
Author Affiliation(jpn)首都大学東京 大学院; 首都大学東京 大学院; 首都大学東京 大学院; 首都大学東京 大学院; 首都大学東京 大学院; 東京都立科学技術大学
Author Affiliation(eng)Tokyo Metropolitan University Graduate School; Tokyo Metropolitan University Graduate School; Tokyo Metropolitan University Graduate School; Tokyo Metropolitan University Graduate School; Tokyo Metropolitan University Graduate School; Tokyo Metropolitan Institute of Technology
Issue Date2008-05
PublisherInstitute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA/ISAS)
宇宙航空研究開発機構宇宙科学研究本部
Publication title第27回宇宙エネルギーシンポジウム 平成19年度
The Twenty-seventh Space Energy Symposium
Start page102
End page106
Publication date2008-05
Languagejpn
AbstractThere are some tethered-systems. The range of a tension is expected to become micro level in 10(exp -2) N in micro power to control the structure in space. The SSPS (Space Solar Power System) Project is as an example to control the vibration of the structure by using the tether technology. This is a system that generates electricity, converts the electric power into the microwave in space, and transmits it to the earth from space, and tether is used to control the vibration of the solar panel. The tether moves in accordance with the panel vibration and the speed resulting in the tether. A contact less measurement device is expected in order to measure the micro order tether tension and speed from the point of the observation. The method of measuring the tether tension and the speed without touching tether is studied in this paper as a contact less measurement method. The tether tension can be measured without any disturbance in this method. This paper examines experimentally the method to measure the tether tension and speed without contact by employing a laser displacement sensor.
Keywordssolar power satellite; tethered satellite; structural vibration; microwave power beaming; tensile strength; vibration damping; nonintrusive measurement; mechanical measurement; satellite attitude control; self induced vibration; 太陽発電衛星; テザー衛星; 構造振動; マイクロ波パワービーミング; 引張強度; 振動減衰; 非接触計測; 機械的測定; 衛星姿勢制御; 自励振動
Document TypeConference Paper
JAXA Categoryシンポジウム・研究会
SHI-NOAA0063965021
URIhttps://repository.exst.jaxa.jp/dspace/handle/a-is/56570


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