Empirical Model Reduction of Spinning Solar Sail
スポンサーリンク
概要
- 論文の詳細を見る
The Spinning solar sail is expected to be a future space exploration system. Considering the dynamic deformation of the sail membrane is an indispensable factor in designing the spacecraft. But the mathematical model of the sail membrane is complex. Computational analysis is difficult and time consuming. Therefore this has a negative impact on simulation, design and control problems. The model reduction technique is required to shorten the design period. It is a necessary step in order to put the gossamer structure to practical use. In this presentation, the dynamic property of the square type spinning solar sail is revealed, and the requirements for constructing a reduction model are revealed. Then, empirical model reduction techniques are applied to gossamer structures, and the issue of constructing a low-order model is summarized.
- THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCESの論文
THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES | 論文
- Study on Ignition and Electron Emission Characteristics of Inductively Coupled Plasma Cathode
- Research and Development of a Debris Removal Method Using Interaction between Space and Electrode with Applied Voltage
- Disaster Monitoring Using ALOS/PALSAR Data
- Design and Experimental Validation of Inter-Satellite Link System for Formation Flight SCOPE Mission
- Magnetic Inflation of Magnetic Plasma Sail by One Component Plasma Simulation