Development of the attitude control system for Tohoku University SPRITE-SAT using a new-model deployable mast

Yuji Sakamoto; Kazuya Yoshida; Yukihiro Takahashi; Takeshi Sakanoi; Kei Takiuchi; Tomoki Sawakami; Yasuhiro Nakazayo; Satoshi Kondo

Development of the attitude control system for Tohoku University SPRITE-SAT using a new-model deployable mast

Yuji Sakamoto, Kazuya Yoshida, Yukihiro Takahashi, Takeshi Sakanoi, Kei Takiuchi, Tomoki Sawakami, Yasuhiro Nakazayo, Satoshi Kondo

Research output: Chapter in Book/Report/Conference proceeding › Conference contribution

Abstract

Tohoku University is now developing the 50-kg micro satellite named SPRITE-SAT. The SPRITE-SAT has the deployable mast, which length is 86 cm and the tip-mass weight is 3.68 kg. The deployable mast was newly developed for SPRITE-SAT. In this paper, the hardware mechanism and evaluation method are described. In addition, the control algorithm of magnetic torquers and the numerical simulation in typical control sequence were explained. As results, the validation of hardware and software of attitude control system for SPRITE-SAT was confirmed.

Original language	English
Title of host publication	International Astronautical Federation - 59th International Astronautical Congress 2008, IAC 2008
Pages	5223-5230
Number of pages	8
Publication status	Published - 2008 Dec 1
Event	59th International Astronautical Congress 2008, IAC 2008 - Glasgow, United Kingdom Duration: 2008 Sep 29 → 2008 Oct 3

Publication series

Name	International Astronautical Federation - 59th International Astronautical Congress 2008, IAC 2008
Volume	8

Other

Other	59th International Astronautical Congress 2008, IAC 2008
Country	United Kingdom
City	Glasgow
Period	08/9/29 → 08/10/3

ASJC Scopus subject areas

Space and Planetary Science
Aerospace Engineering
Astronomy and Astrophysics

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Sakamoto, Y., Yoshida, K., Takahashi, Y., Sakanoi, T., Takiuchi, K., Sawakami, T., Nakazayo, Y., & Kondo, S. (2008). Development of the attitude control system for Tohoku University SPRITE-SAT using a new-model deployable mast. In International Astronautical Federation - 59th International Astronautical Congress 2008, IAC 2008 (pp. 5223-5230). (International Astronautical Federation - 59th International Astronautical Congress 2008, IAC 2008; Vol. 8).

Development of the attitude control system for Tohoku University SPRITE-SAT using a new-model deployable mast. / Sakamoto, Yuji ; Yoshida, Kazuya; Takahashi, Yukihiro; Sakanoi, Takeshi; Takiuchi, Kei; Sawakami, Tomoki; Nakazayo, Yasuhiro; Kondo, Satoshi.

International Astronautical Federation - 59th International Astronautical Congress 2008, IAC 2008. 2008. p. 5223-5230 (International Astronautical Federation - 59th International Astronautical Congress 2008, IAC 2008; Vol. 8).

Research output: Chapter in Book/Report/Conference proceeding › Conference contribution

Sakamoto, Y , Yoshida, K, Takahashi, Y, Sakanoi, T, Takiuchi, K, Sawakami, T, Nakazayo, Y & Kondo, S 2008, Development of the attitude control system for Tohoku University SPRITE-SAT using a new-model deployable mast. in International Astronautical Federation - 59th International Astronautical Congress 2008, IAC 2008. International Astronautical Federation - 59th International Astronautical Congress 2008, IAC 2008, vol. 8, pp. 5223-5230, 59th International Astronautical Congress 2008, IAC 2008, Glasgow, United Kingdom, 08/9/29.

Sakamoto Y , Yoshida K, Takahashi Y, Sakanoi T, Takiuchi K, Sawakami T et al. Development of the attitude control system for Tohoku University SPRITE-SAT using a new-model deployable mast. In International Astronautical Federation - 59th International Astronautical Congress 2008, IAC 2008. 2008. p. 5223-5230. (International Astronautical Federation - 59th International Astronautical Congress 2008, IAC 2008).

Sakamoto, Yuji ; Yoshida, Kazuya ; Takahashi, Yukihiro ; Sakanoi, Takeshi ; Takiuchi, Kei ; Sawakami, Tomoki ; Nakazayo, Yasuhiro ; Kondo, Satoshi. / Development of the attitude control system for Tohoku University SPRITE-SAT using a new-model deployable mast. International Astronautical Federation - 59th International Astronautical Congress 2008, IAC 2008. 2008. pp. 5223-5230 (International Astronautical Federation - 59th International Astronautical Congress 2008, IAC 2008).

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abstract = "Tohoku University is now developing the 50-kg micro satellite named SPRITE-SAT. The SPRITE-SAT has the deployable mast, which length is 86 cm and the tip-mass weight is 3.68 kg. The deployable mast was newly developed for SPRITE-SAT. In this paper, the hardware mechanism and evaluation method are described. In addition, the control algorithm of magnetic torquers and the numerical simulation in typical control sequence were explained. As results, the validation of hardware and software of attitude control system for SPRITE-SAT was confirmed.",

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AU - Sakamoto, Yuji

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AU - Sakanoi, Takeshi

AU - Takiuchi, Kei

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AU - Nakazayo, Yasuhiro

AU - Kondo, Satoshi

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AB - Tohoku University is now developing the 50-kg micro satellite named SPRITE-SAT. The SPRITE-SAT has the deployable mast, which length is 86 cm and the tip-mass weight is 3.68 kg. The deployable mast was newly developed for SPRITE-SAT. In this paper, the hardware mechanism and evaluation method are described. In addition, the control algorithm of magnetic torquers and the numerical simulation in typical control sequence were explained. As results, the validation of hardware and software of attitude control system for SPRITE-SAT was confirmed.

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