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    Please use this identifier to cite or link to this item: https://tkuir.lib.tku.edu.tw/dspace/handle/987654321/109957

    Title: Trajectory Characteristics of Spacecraft Propelled by Planet/Asteroid-Based Photonic Laser Propulsion
    Authors: Hsiao, Fu-Yuen
    Date: 2016-02-14
    Issue Date: 2017-03-15 02:10:59 (UTC+8)
    Abstract: 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.
    Relation: Astronautical Sciences Spaceflight Mechanics 2016, Volume 158.
    Appears in Collections:[Graduate Institute & Department of Aerospace Engineering] Proceeding

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