Flight Model Development of Tokyo Tech Nano-Satellite Cute-1.7 + APD II

Ashida, Hiroki; Nishida, Jun‐ichi; Omagari, Kuniyuki; Fujiwara, Ken; Konda, Yasumi; Yamanaka, Tateo; Tanaka, Yohei; Maeno, Masaki; Fujihashi, Kota; Inagawa, Shinichi; Miura, Yoshio; Matunaga, Saburo

doi:10.2322/tstj.7.tf_37

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“…The Laboratory for Space Systems at the Tokyo Institute of Technology (LSS) has developed and launched three nanosatellites named CUTE-I 1) , Cute-1.7 + APD 2) and Cute-1.7 + APD II 3,4) , as shown in Fig. 1.…”

Section: Introductionmentioning

confidence: 99%

High-Speed Attitude Control System for Small Satellite with Micro-CMGs

Akiyama

Fujihashi

Matunaga

2010

AEROSPACE TECHNOLOGY JAPAN

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The problem of high-speed maneuver with CMGs (Control Moment Gyros) is considered. In general, CMGs are mostly mounted on large spacecraft, such as ISS (International Space Station) or MIR space station because it is large in size and requires a substantial amount of power. The objective of this paper is to introduce the Micro-CMG, which has been jointly-developed by LSS and TAMAGAWA SEIKI Co., Ltd. This CMG is used to achieve the mission that the small satellite named TSUBAME observes the emission of gamma-ray burst. Furthermore, a time-optimal control problem is solved numerically using the gradient method to obtain the time-optimal input to the pyramid array of four CMGs. The solution gives some indication of the feasibility of the mission of TSUBAME.

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Section: Introductionmentioning

confidence: 99%