ETS-VI On-Orbit System Identification Experiments

Isao Yamaguchi, Takashi Kida, Keiji Komatsu, Masaaki Sano, Takeshi Sekiguchi, Shin Ichi Ishikawa, Shin Ichiro Ichikawa, Katsuhiko Yamada, Yuichi Chida, Shuichi Adachi

研究成果: Article

13 引用 (Scopus)

抜粋

System identification and attitude control experiments have been performed as part of a series of bus experiments on the Engineering Test Satellite-VI, which was launched by an H-II rocket in August 1994. The aims of the experiments were to establish a pre-launch system dynamics modeling method, to evaluate typical on-orbit modal parameter identification methods and to develop robust and precise attitude controller design technology for future large flexible spacecraft and large space structures. In the on-orbit identification experiments, the central body of the satellite was excited by gas jet thrusters and the measured attitude and paddle accelerometer signals were downlinked by telemetry. In this paper, the identified parameters are compared with those of the pre-launch modeling and the accuracy of the pre-launch model is evaluated.

元の言語English
ページ(範囲)623-629
ページ数7
ジャーナルJSME International Journal, Series C: Mechanical Systems, Machine Elements and Manufacturing
40
発行部数4
出版物ステータスPublished - 1997 12
外部発表Yes

    フィンガープリント

ASJC Scopus subject areas

  • Industrial and Manufacturing Engineering
  • Mechanical Engineering
  • Engineering(all)

これを引用

Yamaguchi, I., Kida, T., Komatsu, K., Sano, M., Sekiguchi, T., Ishikawa, S. I., ... Adachi, S. (1997). ETS-VI On-Orbit System Identification Experiments. JSME International Journal, Series C: Mechanical Systems, Machine Elements and Manufacturing, 40(4), 623-629.