東京都立科学技術大学
東京都立科学技術大学
東京都立科学技術大学
Georgia Institute of Technology
著者所属（英）
Tokyo Metropolitan Institute of Technology
Tokyo Metropolitan Institute of Technology
Tokyo Metropolitan Institute of Technology
Georgia Institute of Technology
出版者
宇宙航空研究開発機構宇宙科学研究本部
出版者（英）
Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA/ISAS)
雑誌名
平成15年度アストロダイナミクスシンポジウム:講演後刷り集
雑誌名(英)
ISAS Proceedings of 13th Workshop on Astrodynamics and Flight Mechanics 2003: A Collection of Technical Papers
The Deflection-Limiting Input Shaping for the rest-to-rest maneuver of flexible space structures is demonstrated experimentally. The deflection-limiting input shaping is the method for slewing flexible space structures with both suppression of deflection during the slew and elimination of residual oscillations. The method minimizes the maneuver time subject to constraints on residual vibration magnitude, rest-to-rest distance, and the transient deflection amplitude. A model employed in the experiment is a rigid body equipped with a flexible appendage. Results of the experiment show satisfactory performance.
Application of input shaping control to slew maneuver problem of a flexible space structure
