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Archive | 2010

Development of Spaceborne Small Hyperspectral sensor HSC-III for Micro Satellite

Yoshihide Aoyanagi; Shin Satori; Tsuyoshi Totani; Toshihiko Yasunaka; Akihiro Nakamura; Yusuke Takeuchi

The earth observation micro-satellite “TAIKI” is 50 kg satellite which has low-cost and small bus-subsystem. TAIKI is characterized by a low-cost spaceborne small hyperspectral sensor “HSC-III”. HSC-III is targeted at the performances of 30 m ground sampling distance, visible and near infrared wavelength range, 10 nm spectral resolutions, 61 spectral bands and 10 kg weight. HSC-III consists of the telescope, the imaging spectrometer, the electrical system, the on-orbital calibration equipment. The telescope has a pupil diameter of 0.2 m, and has two mirror configuration of Ritchey-Chretien type. The spectrometer has the transmitting grating with the slit and relay lens unit, and array sensor using back-illumination type CMOS image sensor. As a SNR model of HSC-III, we did some calculations and concluded that SNR is approximately 340. Last year, we succeeded to develop the breadboard model of HSC-III optics instrument, and we obtained result of more requirement specification. Also, we have developed the on-orbit spectral calibration equipment. It achieved 0.02 nm of spectral calibration accuracy.


Transactions of The Japan Society for Aeronautical and Space Sciences, Space Technology Japan | 2016

Cluster Launch of Hodoyoshi-3 and -4 Satellites from Yasny by Dnepr Launch Vehicle

Seiji Yoshimoto; Shinichi Nakasuka; Yoshihiro Tsuruda; Yoshihide Aoyanagi; Toshiki Tanaka; Hironori Sahara; Takehiro Ohira; Yuta Araki; Miki Ito; Vladimir Kainov; Andrey Karandaev; Olexij Silkin


Transactions of The Japan Society for Aeronautical and Space Sciences, Space Technology Japan | 2015

Demonstration of Innovative System Design for Twin Micro-Satellite: Hodoyoshi-3 and -4

Yoshihiro Tsuruda; Yoshihide Aoyanagi; Toshiki Tanaka; Takeshi Matsumoto; Shinichi Nakasuka; Seiko Shirasaka; Masayasu Matsui; Ichiro Mase


Transactions of The Japan Society for Aeronautical and Space Sciences, Space Technology Japan | 2010

Breadboard Model of On-orbit Calibration Equipment for Small Hyperspectral Sensor

Yoshihide Aoyanagi; Shin Satori; Yusuke Takeuchi


Archive | 2010

Distance measuring apparatus and distance measuring method

Shinya Kawamata; Ryuji Funayama; Shin Satori; Yoshihide Aoyanagi; Tadayoshi Komatsuda


Archive | 2018

On-Orbit Demonstrations of Robust Autonomous Operations on Cubesat

Toshihiro Obata; Shinichi Nakasuka; Yoshihide Aoyanagi; Takeshi Matsumoto; Seiko Shirasaka


Acta Astronautica | 2018

Discussions on attitude determination and control system for micro/nano/pico-satellites considering survivability based on Hodoyoshi-3 and 4 experiences

Shinichi Nakasuka; Kikuko Miyata; Yoshihiro Tsuruda; Yoshihide Aoyanagi; Takeshi Matsumoto


Archive | 2017

On-orbit Demonstration of Satellite Software Architecture With a Flexible Reconfiguration Capability

Shintaro Nakajima; Ryu Funase; Shinichi Nakasuka; Satoshi Ikari; Masashi Tomooka; Yoshihide Aoyanagi


Transactions of The Japan Society for Aeronautical and Space Sciences, Space Technology Japan | 2016

Results of Hodoyoshi-3 and -4 Earth Observation Missions

Yoshihide Aoyanagi; Akira Iwasaki; Shinichi Nakasuka; Takuji Ebinuma; Shinichi Kimura; Tomohiro Narumi


Transactions of The Japan Society for Aeronautical and Space Sciences, Space Technology Japan | 2016

Development of Store and Forward System for Hodoyoshi-3&4 Microsatellites

Takeshi Matsumoto; Masayasu Matsui; Shinichi Nakasuka; Tomoya Fukami; Yoshihide Aoyanagi; Takaya Inamori; Ayumu Tokaji; Yoshihiro Tsuruda; Toshiki Tanaka; Koji Yamaguchi; Yuzo Shibayama

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Shin Satori

Hokkaido University of Science

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Ryuichi Mitsuhashi

Hokkaido University of Science

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Kosei Ishimura

Japan Aerospace Exploration Agency

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