Attitude Determination and Control System for the PROCYON Micro-Spacecraft-Reference-Cited by-同舟云学术

Attitude Determination and Control System for the PROCYON Micro-Spacecraft

Published:2017 Issue:3 Volume:60 Page:181-191
ISSN:0549-3811
Container-title:TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES
language:en
Short-container-title:Trans. Japan Soc. Aero. S Sci.

Author:

IKARI Satoshi¹,INAMORI Takaya²,ITO Takahiro³,ARIU Kaito¹,OGURI Kenshiro¹,FUJIMOTO Masataka¹,SAKAI Shinichiro³,KAWAKATSU Yasuhiro³,FUNASE Ryu¹

Affiliation:

1. Department of Aeronautics and Astronautics, The University of Tokyo

2. Department of Aerospace Engineering, Nagoya University

3. Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency

Publisher

Japan Society for Aeronautical and Space Sciences

Subject

Space and Planetary Science,Aerospace Engineering

Link

https://www.jstage.jst.go.jp/article/tjsass/60/3/60_T-16-4/_pdf

Reference14 articles.

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2. 2) Saito, H.: Small Satellite REIMEI for Auroa Observation–Five Years on Orbit, IEICE Technical Report, 2010, pp. 161–172.

3. 3) Inamori, T., Hosonuma, T., Ikari, S., Saisutjarit, P., Sako, N., and Nakasuka, S.: Precise Attitude Rate Estimation Using Star Images Obtained by Mission Telescope for Satellite Missions, Adv. Space Res., 55, 4 (2015), pp. 1199–1210.

4. 4) Nakasuka, S.: UNITEC-1 and Onboard Survival Competition in Interplanetary Environment, 27th ISTS, Tsukuba, 2009.

5. 5) Funase, R., Koizumi, H., and Nakasuka, S.: 50kg-class Deep Space Exploration Technology Demonstration Micro-spacecraft PROCYON, 28th Annual AIAA/USU Conference on Small Satellite, Utah, 2014.

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