Zobrazeno 1 - 10
of 67
pro vyhledávání: '"Keiken Ninomiya"'
Autor:
Keiken Ninomiya, Kenji Minesugi, Saku Tsuneta, Takeo Kosugi, Sadanori Shimada, Kiyoshi Ichimoto, Osamu Takahara, Norimasa Yoshida, Tatsuaki Hashimoto
Publikováno v:
IFAC Proceedings Volumes. 37:101-106
The systematic approach adopted in SOLAR-B in order to achieve its fine pointing requirement is presented. The approach consists of : (1)unique pointing requirement analysis in frequency domain that provides a framework of satellite system design, (2
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::04168f9e54a16f53d3b72d7df447caa3
https://doi.org/10.1016/s1474-6670(17)32157-2
https://doi.org/10.1016/s1474-6670(17)32157-2
Autor:
Keiken Ninomiya
Publikováno v:
IFAC Proceedings Volumes. 37:191-196
The status of control technology for Japanese scientific spacecraft is reviewed by referring to the recent and near-term interplanetary, lunar and astronomy robotic missions.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::760717ad18f223ac1085578ea866618b
https://doi.org/10.1016/s1474-6670(17)32172-9
https://doi.org/10.1016/s1474-6670(17)32172-9
Autor:
Shujiro Sawai, Jun'ichiro Kawaguchi, Takashi Kubota, Keiken Ninomiya, Tatsuaki Hashimoto, Mashashi Uo, Kenichi Baba
Publikováno v:
Acta Astronautica. 52(2-6):125-131
ISAS plans to launch an asteroid sample and return spacecraft MUSES-C in 2002 and the spacecraft arrives at near earth asteroid 1989ML in 2003. To approach, rendezvous with, and land on the asteroid safely, the spacecraft has an autonomous navigation
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::ca44062d12f3a4a0a626a9df7afcbc02
http://id.nii.ac.jp/1696/00026562/
http://id.nii.ac.jp/1696/00026562/
Publikováno v:
Acta Astronautica. 51:797-806
The Space Flyer Unit (SFU) system and mission chronology are briefly introduced. Lessons learned from the SFU mission are categorized as programmatic and engineering lessons. In the programmatic category are dealt with both international and domestic
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::fc9c4b643917dbecfa113e4b8d141e2c
https://doi.org/10.1016/s0094-5765(02)00026-7
https://doi.org/10.1016/s0094-5765(02)00026-7
Publikováno v:
Acta Astronautica. 50(2):95-101
This paper proposes a procedure for editing the “IAA Multilingual Space Dictionary”. The dictionary is constructed through international cooperation. Therefore, assignment of the work to each country and international information exchange methods
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::30fcb090701e7bcf4efa12ce6e0143bb
http://id.nii.ac.jp/1696/00026561/
http://id.nii.ac.jp/1696/00026561/
Publikováno v:
IFAC Proceedings Volumes. 34:53-60
A rapid and stable rest-to-rest manoeuvre-scheme is developed for a spacecraft which needs a quick attitude reorientation. By using this scheme, a minimum-time manoeuvre is realized under the limit of sensor's and actuator's capability. In this schem
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::31bd338d497ece946739f1647d84021e
https://doi.org/10.1016/s1474-6670(17)40704-x
https://doi.org/10.1016/s1474-6670(17)40704-x
Actively Controlled Mgnetic Bearing Momentum Wheel and Its Application to Satellite Attitude Control
Publikováno v:
The Institute of Space and Astronautical Science report. 680:1-51
For the high-accuracy attitude control of spacecraft, Magnetic Bearing MomentumWheel (MBMW) has been being investigated as an actuator because of its merits of low disturbancecharacteristics and "gimballability" when a suitable active controller is u
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=jairo_______::71137c06aa2f86108716bba124a0be25
http://id.nii.ac.jp/1696/00036642/
http://id.nii.ac.jp/1696/00036642/
Publikováno v:
Transactions of The Japan Society for Aeronautical and Space Sciences. 44(145):133-141
This paper presents an attitude control law for astronomy or earth-observation satellites, which require highly stable attitude-pointing for observation and large-angle attitude maneuverability between successive observations. In the control law, mag
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::e88c6ce7b18c6831745d1714fc4964a4
http://id.nii.ac.jp/1696/00026569/
http://id.nii.ac.jp/1696/00026569/
Publikováno v:
Systems and Computers in Japan. 31:65-77
A method of recognition and extraction of geographical features from a grayscale image of the surface of a celestial body is proposed. The scheme is based on direct recognition from the image taken by a camera on a spacecraft without shape reconstruc
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::6de41042d8b5ecc6753c92b2100b685f
https://doi.org/10.1002/1520-684x(200009)31:10<65::aid-scj7>3.0.co
https://doi.org/10.1002/1520-684x(200009)31:10<65::aid-scj7>3.0.co
Publikováno v:
Transactions of The Japan Society for Aeronautical and Space Sciences. 43(142):182-189
As pointing requirements of astronomy satellites become more demanding, a conventional momentum-exchange scheme for attitude-pointing control is sometimes not enough to satisfy stringent stability requirements. This paper presents a new attitude cont
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::d6d190dc856e305e262acbc77e72b179
http://id.nii.ac.jp/1696/00026568/
http://id.nii.ac.jp/1696/00026568/