Trajectory Evolution Under Laser Photonic Propulsion in The Two-Body Problem
學年 101
學期 1
發表日期 2013-01-26
作品名稱 Trajectory Evolution Under Laser Photonic Propulsion in The Two-Body Problem
作品名稱（其他語言）
著者 蕭富元
作品所屬單位 淡江大學航空太空工程學系
出版者
會議名稱 24th AAS/AIAA Space Flight Mechanics Meeting
會議地點 Santa Fe, USA
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 for the two-body problem, and variation of orbit elements. This study introduces the Gauss’ Equations to evaluate the evolution of orbit elements, and normalizes the Gauss’ Equations with parameters of mother ship. The evolution of orbit elements also confirms the constraint on the smallest thrust at the launching stage. Numerical simulations are provided in this paper. The results of this paper are directly applicable to future PLP thrust missions, and particularly interplanetary travel.
關鍵字
語言 en
收錄於
會議性質 國際
校內研討會地點
研討會時間 20130126~20130130
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 148, AAS 13 – 377
相關連結

機構典藏連結 ( http://tkuir.lib.tku.edu.tw:8080/dspace/handle/987654321/98870 )

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