| Article ID | Journal | Published Year | Pages | File Type |
|---|---|---|---|---|
| 8055762 | Acta Astronautica | 2018 | 8 Pages |
Abstract
This paper presents the results of line-of-sight (LOS) attitude control using control moment gyros under a micro-gravity environment generated by parabolic flight. The W-Z parameters are used to describe the spacecraft attitude. In order to stabilize the current LOS to the target LOS, backstepping-based feedback control is considered using the W-Z parameters. Numerical simulations and experiments under a micro-gravity environment are carried out, and their results are compared in order to validate the proposed control methods.
Related Topics
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Aerospace Engineering
Authors
Hirohisa Kojima, Kana Hiraiwa, Yasuhiro Yoshimura,