| Project/Area Number |
15560689
|
|---|
| Research Category |
Grant-in-Aid for Scientific Research (C)
|
| Allocation Type | Single-year Grants |
|---|
| Section | 一般 |
|---|
| Research Field |
Aerospace engineering
|
|---|
| Research Institution | Japan Aerospace Exploration Agency |
|---|
Principal Investigator |
MORITA Yasuhiro ISAS, Space Transportation Engineering, Professor, 宇宙科学研究本部・宇宙輸送工学研究系, 教授 (80230134)
|
|---|
| Project Period (FY) |
2003 – 2004
|
| Project Status |
Completed (Fiscal Year 2004)
|
| Budget Amount *help |
¥3,000,000 (Direct Cost: ¥3,000,000)
Fiscal Year 2004: ¥1,300,000 (Direct Cost: ¥1,300,000)
Fiscal Year 2003: ¥1,700,000 (Direct Cost: ¥1,700,000)
|
|---|
| Keywords | Localized Control / Space Systems / Flexible Structures / 有限要素モデル / 偏微分方程式 / 数値シュミレーション / 数値シミュレーション |
|---|
| Research Abstract |
The research deals with a demonstration of a novel control concept-the localized control, which can be considered one of the most prosperous future algorithms to control complicated large space structures. The theoretical aspect of the study has given the detailed formulation and the proof of its theoretical effectiveness. Beyond this, the study introduces a methodology for practical design of a controller, which involves placement of actuators ; tuning of regulator and interface force controller, and robustness enhancement coupled with observation algorithm design. The simulation technique is utilized to establish the methodology and gives its endorsement to the practical effectiveness of the concept.
|
