Trajectory Analysis of Spacecraft Propelled by Photonic Laser Propulsion System

淡江大學機構典藏 > 工學院 > 航空太空工程學系暨研究所 > 會議論文 > Item 987654321/98868

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題名:	Trajectory Analysis of Spacecraft Propelled by Photonic Laser Propulsion System
作者:	T. H. Wang, C. C. Lee, P. J. Yang, H. J. Wei, B. Y. Tsai and F. Y. Hsiao
貢獻者:	淡江大學航空太空工程學系
日期:	2011-02
上傳時間:	2014-09-24 11:53:39 (UTC+8)
出版者:	Univelt, Inc.
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.
關聯:	Advances in the Astronautical Sciences 140, AAS 11 – 269
顯示於類別:	[航空太空工程學系暨研究所] 會議論文

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