On-orbit attitude control experiments for ETS-VI. I-PD and two-degree-of-freedom ℋ_∞ control

Author

Chida, Y. ; Yamaguchi, Yoshio ; Soga, H. ; Kida, T. ; Yamaguchi, I. ; Sekiguchi, T.

Author_Institution

Res. & Dev. Center, Toshiba Corp., Kawasaki, Japan

Volume

1

fYear

1996

fDate

11-13 Dec 1996

Firstpage

486

Abstract

Engineering Test Satellite VI (ETS-VI) is a three-axis-stabilized satellite launched by National Space Development Agency of Japan in 1994. Identification and attitude control experiments on orbit were planned as one of the ETS-VI experimental programs and were carried out in 1995. These experiments were the first tests fulfilled by Japan for a real on-orbit satellite. In this paper, we present certain results of the attitude control experiments using I-PD control and two degree-of-freedom control based on ℋ_∞ control. Experimental results showed that these controllers provide the expected control performance and that these design methods are effective for satellite control

Keywords

H^∞ control; artificial satellites; attitude control; three-term control; 2-DOF ℋ_∞ control; ETS-VI; Engineering Test Satellite VI; I-PD control; identification; in-orbit attitude control; on-orbit attitude control experiments; three-axis-stabilized satellite; Aerospace control; Aerospace engineering; Aerospace testing; Attitude control; Control systems; Research and development; Satellites; Silicon carbide; Torque control; Transfer functions;

fLanguage

English

Publisher

ieee

Conference_Titel

Decision and Control, 1996., Proceedings of the 35th IEEE Conference on

Conference_Location

Kobe

ISSN

0191-2216

Print_ISBN

0-7803-3590-2

Type

conf

DOI

10.1109/CDC.1996.574361

Filename

574361

On-orbit attitude control experiments for ETS-VI. I-PD and two-degree-of-freedom ℋ∞ control

Chida, Y. ; Yamaguchi, Yoshio ; Soga, H. ; Kida, T. ; Yamaguchi, I. ; Sekiguchi, T.

conf

On-orbit attitude control experiments for ETS-VI. I-PD and two-degree-of-freedom ℋ_∞ control