抄録
This study proposes a feedback control law for orbital parameters of a coplanar rigid satellite system. The governing equations are denoted as ‘Symmetrical Affine System’ with three variables and two control inputs, which is guaranteed to be locally controllable. However, because of time-variant parameters included in the governing equations, previously proposed feedback control laws cannot be directly applied. Therefore, in this paper, a novel feedback control law to simultaneously control plural orbital parameters is proposed. Finally the effectiveness of the proposed control law is validated through numerical simulations.
| 寄稿の翻訳タイトル | Feedback Control of Orbital Parameters for a Rigid Satellite under Nonholonomic Constraint |
|---|---|
| 本文言語 | 日本語 |
| ページ（範囲） | 1-7 |
| ページ数 | 7 |
| ジャーナル | 日本航空宇宙学会論文集 = Journal of the Japan Society for Aeronautical and Space Sciences |
| 巻 | 56 |
| 号 | 648 |
| DOI | |
| 出版ステータス | 出版済み - 1月 5 2008 |