Zobrazeno 1 - 10
of 36
pro vyhledávání: '"Nobutada Sako"'
Autor:
Nobutada Sako, Norihide Miyamura
Publikováno v:
TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES, AEROSPACE TECHNOLOGY JAPAN. 16:47-52
Publikováno v:
Journal of Aerospace Engineering. 32
This study considers the attitude disturbance torque caused by the magnetic shape anisotropy of onboard magnetic substances in low Earth orbit (LEO) satellites. The gravity gradient, solar ...
Publikováno v:
Acta Astronautica. 112:192-199
We propose a magnetic plasma deorbit (MPD) system using magnetic torquers (MTQs) for inducing the deorbit of nano- and micro-satellites. Currently, orbital space debris from these satellites is a matter of increasing concern to all satellites; howeve
Autor:
Phongsatorn Saisutjarit, Shinichi Nakasuka, Takayuki Hosonuma, Nobutada Sako, Satoshi Ikari, Takaya Inamori
Publikováno v:
Advances in Space Research. 55:1199-1210
Recently, small satellites have been employed in various satellite missions such as astronomical observation and remote sensing. During these missions, the attitudes of small satellites should be stabilized to a higher accuracy to obtain accurate sci
Publikováno v:
JOURNAL OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES. 63:119-128
Autor:
Phongsatorn Saisutjarit, Ryuhei Hamaguchi, Shinichi Nakasuka, Takaya Inamori, Nobutada Sako, Kouhei Ozawa
Publikováno v:
Journal of Aerospace Engineering. 29
Magnetic sensors are reliable, lightweight, and low power consumption sensors that are utilized in almost all nanosatellites and microsatellites for a magnetic attitude control system using magnetic torquers (MTQs). In some nanosatellites and microsa
Publikováno v:
Advances in Space Research. 48:432-440
Theses days, many nano- and micro-satellites are applied to several astronomy and remote sensing missions. In order to achieve mission requirements, these satellites must control the attitude precisely. A magnetic disturbance is one of the dominant s
Publikováno v:
Aircraft Engineering and Aerospace Technology. 83:221-228
PurposeThis paper aims to present an attitude determination and control system for a nano‐astrometry satellite which requires precise angular rate control. Focus of the research is methods to achieve the requirement.Design/methodology/approachIn or
Publikováno v:
Acta Astronautica. 68:2038-2046
Nano-satellites provide space access to broader range of satellite developers and attract interests as an application of the space developments. These days several new nano-satellite missions are proposed with sophisticated objectives such as remote-
Autor:
Yuya Nakamura, Takashi Eishima, Mitsuhito Komatsu, Nobutada Sako, Hironori Sahara, Shinichi Nakasuka
Publikováno v:
Acta Astronautica. 66:1099-1105
The paper overviews recent nano-satellite development activities of University of Tokyo, Intelligent Space Systems Laboratory (ISSL). Development of real satellites and actually launching them provides excellent materials for space engineering educat