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    Please use this identifier to cite or link to this item: https://tkuir.lib.tku.edu.tw/dspace/handle/987654321/83721

    Title: Trajectory of spacecraft with photonic laser propulsion in the two-body problem
    Authors: Hsiao, Fu-Yuen;Wang, Tai-Hang;Lee, Chi-Cheng;Yang, Pin-Chu;Wei, Hung-Chu;Tsai, Ping-Yen
    Contributors: 淡江大學航空太空工程學系
    Keywords: Photonic laser propulsion;Spacecraft trajectory;Two-body problem;Jacobi integral;Missions to Mars;Jacobi integral;Missions to Mars
    Date: 2013-03
    Issue Date: 2013-03-20 16:56:41 (UTC+8)
    Publisher: Kidlington: Pergamon
    Abstract: 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 and rotational frame for the two-body problem, and uses the Jacobi integral to investigate the spatial restrictions on trajectory. This study proposes a constraint on the smallest thrust at the launching stage, and finds the in-plane and out-of-plane equilibria. Numerical simulations confirm the validity of the derivations. The results of this paper are directly applicable to future PLP thrust missions, and particularly interplanetary travel.
    Relation: Acta Astronautica 84, pp.215-226
    DOI: 10.1016/j.actaastro.2012.11.006
    Appears in Collections:[Graduate Institute & Department of Aerospace Engineering] Journal Article

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