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    jsp.display-item.identifier=請使用永久網址來引用或連結此文件: http://tkuir.lib.tku.edu.tw:8080/dspace/handle/987654321/109957

    题名: Trajectory Characteristics of Spacecraft Propelled by Planet/Asteroid-Based Photonic Laser Propulsion
    作者: Hsiao, Fu-Yuen
    日期: 2016/03/04
    上传时间: 2017-03-15 02:10:59 (UTC+8)
    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.
    關聯: Astronautical Sciences Spaceflight Mechanics 2016, Volume 158.
    显示于类别:[航空太空工程學系暨研究所] 會議論文


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