Výsledky vyhledávání - "Ryo SUZUMOTO"

Akademický článek

μm-class Control of Relative Position and Attitude for a Formation Flying Synthetic Aperture Telescope with Micro-satellites.

Autor: Ryo SUZUMOTO¹ suzumoto@space.t.u-tokyo.ac.jp, Satoshi IKARI¹, Norihide MIYAMURA², Shinichi NAKASUKA¹, Maddock, Christie

Publikováno v: Transactions of the Japan Society of Aeronautical & Space Science. 2021, Vol. 64 Issue 2, p101-111. 11p.

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Mission to Earth–Moon Lagrange Point by a 6U CubeSat: EQUULEUS

Autor: Hiroyuki Koizumi, Ryo Suzumoto, Reina Hikida, Ichiro Yoshikawa, Yusuke Murata, Yosuke Masuda, Kazuo Yoshioka, Kento Tomita, Tatsuaki Hashimoto, Keidai Iiyama, Haruki Nakano, Kosei Kikuchi, Jun Asakawa, Hiroki Aohama, Masaki Kuwabara, Toshinori Ikenaga, Shuhei Matsushita, Kanta Yanagida, Toshihiro Shibukawa, Hajime Yano, Kota Miyoshi, Ryohei Takahashi, Yuji Saito, Daiko Mori, Keita Nishii, Shintaro Nakajima, Eigo Ishioka, Kazuyoshi Arai, Akihiro Hattori, Yosuke Kawabata, Shunichiro Nomura, Satoshi Ikari, Atsushi Tomiki, Shogo Arao, Wataru Mikuriya, Akihiro Ishikawa, Kota Kakihara, Sho Ishiwata, Naoya Ozaki, Masahisa Yanagisawa, Hirotaka Kondo, Shinsuke Abe, Ryota Fuse, Nobuhiro Funabiki, Ryu Funase, Takayuki Hirai, Yuta Kobayashi, Wataru Torii, Stefano Campagnola, Hiroto Seki, Ritsuko Jitsukawa, Taichi Ito, Masahiro Fujiwara, Nicola Baresi

Publikováno v: IEEE Aerospace and Electronic Systems Magazine. 35:30-44

EQUULEUS (EQUilibriUm Lunar-Earth point 6U Spacecraft) will be the world's smallest spacecraft to explore the Earth-Moon Lagrange point. It is being jointly developed by JAXA (Japan Aerospace Exploration Agency) and the University of Tokyo, and will

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_________::1316990cbd3aeac7278034673ad1833a
https://doi.org/10.1109/maes.2019.2955577

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Conceptual Optical Design of a Synthetic Aperture Telescope by Small Satellite Formation Flying for GEO Remote Sensing

Autor: Norihide Miyamura, Shinichi Nakasuka, Satoshi Ikari, Ryo Suzumoto

Publikováno v: TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES, AEROSPACE TECHNOLOGY JAPAN. 18:101-107

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_________::4267697a1438a0d438f458059e9f2fe0
https://doi.org/10.2322/tastj.18.101

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Experimental Study for μ-class Control of Relative Position and Attitude for Synthetic Aperture Telescope Using Formation Flying Micro-satellites

Autor: Shinichi Nakasuka, Ryo Suzumoto, Norihide Miyamura, Satoshi Ikari

Publikováno v: IFAC-PapersOnLine. 53:5701-5708

Earth remote sensing from geostationary orbit (GEO) realizes high time resolution that is essential for disaster monitoring; however, the spatial resolution is commonly worse than observation from low Earth orbit (LEO). In order to achieve high-resol

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_________::d79a2b471a9ad5ad7b6f5cb8a8f7c65a
https://doi.org/10.1016/j.ifacol.2020.12.1597

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Image processing for a formation flying synthetic aperture telescope

Autor: Norihide Miyamura, Shinichi Nakasuka, Ryo Suzumoto, Satoshi Ikari

Publikováno v: International Conference on Space Optics — ICSO 2020.

Small satellites have been used for remote sensing with a spatial resolution of several meters from LEO in recent years. However, it is difficult to increase temporal resolution for LEO remote sensing due to the short orbital period. Therefore, GEO r

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_________::63e2b908f4ec837bae91026be4c74f59
https://doi.org/10.1117/12.2599818

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Modeling of piezoelectric actuator's hysteresis and its effect on the control accuracy of a LEO-to-GEO laser-communication for a small satellite

Autor: Shinichi Nakasuka, Takayuki Hosonuma, Alberto Carrasco-Casado, Phong Xuan Do, Florian Moll, Ryo Suzumoto, Morio Toyoshima

Compared to conventional large satellites in the past, small satellite classes (less than 150 kg) show their advantages for mass production, such as short time and low cost for development and launch, to cope with the demand for emerging missions tha

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_dedup___::033ba6d9ae053b9fdc0ecb80c5cd6ab1
https://elib.dlr.de/187056/

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Comparison of Performance by different operation method of a Water Resistojet Propulsion System : AQUARIUS Installed on 6U CubeSat : EQUULEUS

Autor: Hiroyuki Koizumi, Kosei Kikuchi, Masaya Murohara, Ryo Suzumoto, Kanta Yanagida, Akihiro Hattori, Jun Asakawa, Mariko Akiyama, Yasuho Ataka, Keita Nishii, Qihang Wang, Kimiya Komurasaki, Kota Kakihara, Ryu Funase

Publikováno v: AIAA Propulsion and Energy 2019 Forum.

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_________::d18311660c49a5a16a85a043ce1c7cdd
https://doi.org/10.2514/6.2019-3955

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Proposal of Mechanism to Reduce Nonlinearity of Dynamic Vibration Absorber Using Pendulum

Autor: Keisuke Yamada, Ryo Suzumoto

Publikováno v: The Proceedings of the Dynamics & Design Conference. 2019:214

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_________::4bf15fa1ba1de5213dff56d2ec4a73b7
https://doi.org/10.1299/jsmedmc.2019.214

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