| Trajectory Analysis of Spacecraft Propelled by Photonic Laser Propulsion System | |
|---|---|
| 學年 | 99 |
| 學期 | 2 |
| 發表日期 | 2011-02-13 |
| 作品名稱 | Trajectory Analysis of Spacecraft Propelled by Photonic Laser Propulsion System |
| 作品名稱（其他語言） | |
| 著者 | T. H. Wang, C. C. Lee, P. J. Yang, H. J. Wei, B. Y. Tsai and F. Y. Hsiao |
| 作品所屬單位 | 淡江大學航空太空工程學系 |
| 出版者 | Univelt, Inc. |
| 會議名稱 | 2011 Space Flight Mechanics Meeting |
| 會議地點 | New Orleans, USA |
| 摘要 | This paper studies the application of photonic laser propulsion (PLP) system to the trajectory analysis in a space mission. The PLP system is an innovative technology proposed by Dr. Bae. With repeated reflections of laser beam, it can generate continuous and tremendous power by consuming very small energy. When applying to the trajectory analysis in space flight, we model the problem as a circular restricted three-body problem, and the corresponded Jacobi integral is found. A contour of zero-velocity lines is presented. Equilibrium points under this system are also discussed and found. Numerical simulations are presented to show the validity of our derivations. The results obtained in this paper are directly applicable to the usage of the PLP thrust in the future, and potentially helpful to various space missions, including interplanetary traveling. |
| 關鍵字 | |
| 語言 | en_US |
| 收錄於 | EI |
| 會議性質 | 國際 |
| 校內研討會地點 | |
| 研討會時間 | 20110213~20110217 |
| 通訊作者 | 蕭富元 |
| 國別 | USA |
| 公開徵稿 | Y |
| 出版型式 | 電子版 |
| 出處 | Advances in the Astronautical Sciences 140, AAS 11 – 269 |
| 相關連結 |
機構典藏連結 ( http://tkuir.lib.tku.edu.tw:8080/dspace/handle/987654321/98868 ) |
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