Zobrazeno 1 - 10
of 492
pro vyhledávání: '"飛行船"'
Autor:
Gaku, IWAI
Publikováno v:
甲南大學紀要.文学編 = The Journal of Konan University. Faculty of Letters. 173:41-51
Publikováno v:
平成15年度アストロダイナミクスシンポジウム:講演後刷り集 = ISAS Proceedings of 13th Workshop on Astrodynamics and Flight Mechanics 2003: A Collection of Technical Papers. :216-226
本研究では惑星探査ミッション用のプラットフォームとしての遠隔操縦飛行船を検討する。惑星大気圏から、長時間観測できる航空機プラットフォームとして、飛行船が考えられる。惑
Publikováno v:
日本バーチャルリアリティ学会論文誌. 16(2):127-138
This paper proposes an augmented telepresence system which generates large-scale omnidirectional AR scenes in outdoor environments using recorded omnidirectional videos captured from an unmanned airship. The proposed system realizes geometric registr
Autor:
Fujii, Hironori A.
Publikováno v:
大気球シンポジウム: 平成18年度 = Balloon Symposium: 2006. :45-48
大気球シンポジウム 平成18年度(2007年1月15-16日. 宇宙航空研究開発機構宇宙科学研究本部 (JAXA)(ISAS)), 相模原市, 神奈川県)
Balloon Symposium 2006 (January 15-16, 2007. Institute of Space and Astronautic
Balloon Symposium 2006 (January 15-16, 2007. Institute of Space and Astronautic
Autor:
Shing-Lang Wang, 王歆嵐
94
The main theme of the thesis is to design an autonomous vision-based small-scale blimp which can search and approach the desired target without human’s operation. The blimp uses wireless camera to capture images and sends the image data to
The main theme of the thesis is to design an autonomous vision-based small-scale blimp which can search and approach the desired target without human’s operation. The blimp uses wireless camera to capture images and sends the image data to
Externí odkaz:
http://ndltd.ncl.edu.tw/handle/82629546170562441881
Autor:
Yuan-Kuan Yang, 楊元坤
90
In this research, we develop an unmanned airship system. In addition to the traditional Remote Control system, a PC-based flight control system was developed to improve flight stability and maneuverability. The system includes two parts: the
In this research, we develop an unmanned airship system. In addition to the traditional Remote Control system, a PC-based flight control system was developed to improve flight stability and maneuverability. The system includes two parts: the
Externí odkaz:
http://ndltd.ncl.edu.tw/handle/749p67