會議論文

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
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