Trajectory Characteristics of Spacecraft Propelled by Planet/Asteroid-Based Photonic Laser Propulsion | |
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學年 | 104 |
學期 | 2 |
發表日期 | 2016-02-14 |
作品名稱 | Trajectory Characteristics of Spacecraft Propelled by Planet/Asteroid-Based Photonic Laser Propulsion |
作品名稱(其他語言) | |
著者 | Fu-Yuen Hsiao |
作品所屬單位 | |
出版者 | |
會議名稱 | 2016 AAS/AIAA Space Flight Mechanics Meeting |
會議地點 | Napa, CA, USA |
摘要 | This paper studies the trajectory characteristics of the spacecraft propelled by a ground-based photonic laser propulsion (PLP) system. An spaceborne PLP system was studied in the past years, but a ground-based PLP system may also helpful in space missions. In this paper, a PLP sytem is assumed to be installed in the surface of a celestial body. The equations of motion of the spacecraft in the body-fixed frame is derived,and the corresponded Jocobi integral is found. Contours of zero-velocity lines are presented and trajectories of example missions will be provided as potential applications in the final paper. |
關鍵字 | |
語言 | en_US |
收錄於 | |
會議性質 | 國際 |
校內研討會地點 | 無 |
研討會時間 | 20160214~20160218 |
通訊作者 | |
國別 | USA |
公開徵稿 | |
出版型式 | |
出處 | Astronautical Sciences Spaceflight Mechanics 2016, Volume 158. |
相關連結 |
機構典藏連結 ( http://tkuir.lib.tku.edu.tw:8080/dspace/handle/987654321/109957 ) |