Zobrazeno 1 - 10
of 12
pro vyhledávání: '"NAMERA, TAKAKAZU"'
Autor:
Yamaguchi, Kazuhiro, Nagahashi, Takaharu, Akiyama, Takuya, Matsue, Hideaki, Uekado, Kunio, Namera, Takakazu, Fukui, Hiroshi, Nanamatsu, Satoshi
Publikováno v:
2015 International Conference on Information Networking (ICOIN); 2015, p242-247, 6p
Autor:
Yamaguchi, Kazuhiro, Nagahashi, Takaharu, Akiyama, Takuya, Yamaguchi, Takahiro, Matsue, Hideaki, Hasui, Akio, Namera, Takakazu, Fukui, Hiroshi, Nanamatsu, Satoshi
Publikováno v:
2014 International Conference on Information & Communication Technology Convergence (ICTC); 2014, p253-258, 6p
Autor:
Yamaguchi, Kazuhiro, Nagahashi, Takaharu, Akiyama, Takuya, Matsue, Hideaki, Uekado, Kunio, Namera, Takakazu, Fukui, Hiroshi, Nanamatsu, Satoshi
Publikováno v:
Scientific World Journal; 9/2/2015, Vol. 2015, p1-10, 10p
Autor:
Ota, Kenko, Matsue, Hideaki, Miyazawa, Satoru, Nanamatsu, Satoshi, Hirata, Yukihiro, Hasui, Akio, Yamazaki, Masahiro, Namera, Takakazu, Fukui, Hiroshi, Harvey, Matthew, Miyajima, Hajime, Yazawa, Yoshiaki, Kainuma, Yoshihiro, Yui, Takuma
Publikováno v:
2011 IEEE Global Telecommunications Conference (GLOBECOM 2011); 2011, p1-5, 5p
Autor:
Namera, Takakazu, Stubberud, Allen
Publikováno v:
22nd IEEE Conference on Decision & Control; 1983, Issue 22, p84-87, 4p
Autor:
NAMERA, TAKAKAZU, STUBBERUD, ALLEN R.
Publikováno v:
International Journal of Control; Nov1983, Vol. 38 Issue 5, p1047-1053, 7p
Autor:
HINADA, Motoki, NAKATANI, Ichiro, NINOMIYA, Keiken, MURANAKA, Noboru, NAMERA, Takakazu, UO, Masahi, OGURA, Naoto
Publikováno v:
The Institute of Space and Astronautical Science report. S.P. : The Proceedings of the Symposium on Mechanics for Space Flight 1987. 6:137-147
Analysis is given for the dynamics of a spinning satellite with four radial wire antennas. In this analysis, generalized model is used, in which, mass properties of wire antennas are not equal and antennas' attachment points on the satellite have som
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=jairo_______::227c3483eb5e1879f416fc08d99ba66a
http://id.nii.ac.jp/1696/00031322/
http://id.nii.ac.jp/1696/00031322/
Autor:
NINOMIYA, Keiken, UESUGI, Kuninori, KAWAGUCHI, Junichiro, YOKOTA, Hiroki, MURANAKA, Noboru, NAMERA, Takakazu, KITADE, Kenji, OGASAWARA, Masahiro, KIMURA, Masahumi, DOBASHI, Masayuki
Publikováno v:
宇宙科学研究所報告. 33:1-45
To support the operation of onboard AOCS (Attitude and Orbit Control System) of "SAKIGAKE" and "SUISEI", ground support software for attitude control and orbit correction was developed. The software, named POPS (PLANET-A AOCS Operation Software), has
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=jairo_______::133825995e7bce254712a4a7eb15175e
http://id.nii.ac.jp/1696/00032673/
http://id.nii.ac.jp/1696/00032673/
Autor:
NINOMIYA, Keiken, UESUGI, Kuninori, MURANAKA, Noboru, KATOH, Akio, KITADE, Kenji, NAMERA, Takakazu, UO, Masashi
Publikováno v:
宇宙科学研究所報告. 37:1-62
"SAKIGAKE", Japan's first interplanetary spacecraft was successfully launched on January 8,1985.Its mission was to verify the launch capability of the then newly developed Mu-3SIIvehicle and the technology applied to "SUISEI", Japan's Halley's comet
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=jairo_______::4f42c67c27cfc6ddd9e37e4939a1bcd5
http://id.nii.ac.jp/1696/00032677/
http://id.nii.ac.jp/1696/00032677/
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