Volume 41 Issue 2
Mar.  2021
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ZHANG Jiawen, ZHENG Jianhua, WANG Youliang, LI Mingtao. Trajectory Design for Solar Approaching Detection Mission Using Multiple Resonant Gravity Assists of the Venus[J]. Journal of Space Science, 2021, 41(2): 310-319. doi: 10.11728/cjss2021.02.310
Citation: ZHANG Jiawen, ZHENG Jianhua, WANG Youliang, LI Mingtao. Trajectory Design for Solar Approaching Detection Mission Using Multiple Resonant Gravity Assists of the Venus[J]. Journal of Space Science, 2021, 41(2): 310-319. doi: 10.11728/cjss2021.02.310

Trajectory Design for Solar Approaching Detection Mission Using Multiple Resonant Gravity Assists of the Venus

doi: 10.11728/cjss2021.02.310
  • Received Date: 2019-11-27
  • Rev Recd Date: 2020-09-13
  • Publish Date: 2021-03-15
  • To approach close to the Sun, direct launch from the Earth costs a lot of energy, which can be effectively reduced by the gravity assist of the Venus. In this paper, interplanetary transfer trajectories with multiple resonant gravity assists of the Venus are designed for a solar approaching detection mission. And design models for the trajectories with continuous resonant gravity assists, as well as resonant and non-resonant gravity assists combined are built. A mission launched between 2025 and 2028 is studied. The study shows that, compared with trajectory with continuous resonant gravity assists, trajectory with resonant and non-resonant gravity assists combined is useful for reducing transfer time of solar approaching detection mission. And its impact on the energy cost is not universal, which is related to the resonance ratio in the trajectory.

     

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  • [1]
    GALEEV A A, VAISBERG O L, ZAKHAROV A V, et al. Project Ziolkovsky-Solar Probe mission concept[J]. Adv. Space Res., 1996, 17(3):13-20
    [2]
    TSURUTANI B T, VAISBERG O L. The Solar Probe mission and comments on plasma wave observations[C]//AIP Conference Proceeding. New York:AIP Press, 1996:255
    [3]
    GUO Y. Trajectory design of Solar Probe+ using multiple Venus gravity assists[C]//AIAA/AAS Astrodynamics Specialist Conference and Exhibit. Honolulu, Hawaii:American Institute of Aeronautics and Astronautics, 2008:3029-3039
    [4]
    SUKHANOV A A. Close approach to Sun using gravity assists of the inner planets[J]. Acta Astron., 1999, 45:177-185
    [5]
    QIAO Dong. Study of Transfer Trajectory Design Method for Deep Space Exploration and Application to Small Body Exploration[D]. Harbin:Harbin Institute of Technology, 2007 (乔栋. 深空探测转移轨道设计方法研究及 在小天体探测中的应用[D]. 哈尔滨:哈尔滨工业大学, 2007)
    [6]
    LI Junfeng, BAOYIN Hexi, JIANG Fanghua. Dynamics and Control of Interplanetary Flight[M]. Beijing:Tsinghua University Press, 2014:110-127 (李俊峰, 宝音贺西,蒋方华. 深空探测动力学与控制[M]. 北京:清华大学出版社, 2014:110-127)
    [7]
    YUAN Jianping, ZHAO Yushan, TANG Geshi, et al. Spacecraft Deep Space Flight Trajectory Design[M]. Beijing:China Astronautic Publishing House, 2014:59-76 (袁建平, 赵育善, 唐歌实, 等. 航天器深空飞 行轨道设计[M]. 北京:中国宇航出版社, 2014:59-76)
    [8]
    HU Zhongbo. The Study of Differential Evolution Algorithm for the Function Optimization[D]. Wuhan:Wuhan University of Technology, 2006 (胡中波. 差分演化算法及其在函数优化中的应用研究[D]. 武汉:武汉理工大学, 2006)
    [9]
    Differential evolution (DE) for continuous function optimization (an algorithm by Kenneth Price and Rainer Storn)[OL].[2019-10-10] http://www1.icsi.berkeley.edu/~storn/code.html#tevc
    [10]
    LI Xiaoyu. Design and Optimization of Deep Space Trajectory on the Initial Design Stage[D]. Beijing:University of Chinese Academy of Sciences, 2012 (李小玉. 深空探测轨道的初始方案设计与优化[D]. 北京:中国科 学院大学, 2012)
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