| Trajectory of spacecraft with photonic laser propulsion in the two-body problem | |
|---|---|
| 學年 | 101 |
| 學期 | 2 |
| 出版（發表）日期 | 2013-03-01 |
| 作品名稱 | Trajectory of spacecraft with photonic laser propulsion in the two-body problem |
| 作品名稱（其他語言） | |
| 著者 | Hsiao, Fu-Yuen; Wang, Tai-Hang; Lee, Chi-Cheng; Yang, Pin-Chu; Wei, Hung-Chu; Tsai, Ping-Yen |
| 單位 | 淡江大學航空太空工程學系 |
| 出版者 | Kidlington: Pergamon |
| 著錄名稱、卷期、頁數 | Acta Astronautica 84, pp.215-226 |
| 摘要 | The photonic laser propulsion (PLP) system can produce continuous and constant thrust. This paper reviews its basics and then studies its application in the two-body interplanetary trajectory. This study also derives the equations of motion (EOM) for a spacecraft in an inertial frame and rotational frame for the two-body problem, and uses the Jacobi integral to investigate the spatial restrictions on trajectory. This study proposes a constraint on the smallest thrust at the launching stage, and finds the in-plane and out-of-plane equilibria. Numerical simulations confirm the validity of the derivations. The results of this paper are directly applicable to future PLP thrust missions, and particularly interplanetary travel. |
| 關鍵字 | Photonic laser propulsion;Spacecraft trajectory;Two-body problem;Jacobi integral;Missions to Mars;Jacobi integral; Missions to Mars |
| 語言 | en |
| ISSN | 0094-5765 |
| 期刊性質 | 國外 |
| 收錄於 | SCI |
| 產學合作 | |
| 通訊作者 | Hsiao, Fu-Yuen |
| 審稿制度 | |
| 國別 | GBR |
| 公開徵稿 | |
| 出版型式 | 紙本 |
| 相關連結 |
機構典藏連結 ( http://tkuir.lib.tku.edu.tw:8080/dspace/handle/987654321/83721 ) |
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