Chinese Space Science and Technology ›› 2013, Vol. 33 ›› Issue (2): 61-66.doi: 10.3780/j.issn.1000-758X.2013.02.010

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Design of Multiple Gravity Assist Trajectories with Deep Space Maneuver

ZHANG  Ying1, YUE  Xiao-Kui1, HE  Liang2   

  1. (1 School of Astronautics, Northwestern Polytechnical University, Xi′an 710072)(2 Shanghai Institute of Space Flight Control Technology, Shanghai 200233)
  • Received:2012-05-31 Revised:2012-10-23 Published:2013-04-25 Online:2013-04-25

Abstract: Planetary swing-by is an effective way to reduce the launch energy for interplanetary exploration missions. However, the traditional swing-by model is difficult to match the relative velocity vector before and after the swing-by. Therefore, the swing-by model was established, and the hyperbolic velocity vector after the swing-by was also derived. Because of the strong coupling of the trajectory design parameters, a global-local hybrid search algorithm was proposed for designing Earth-Venus-Earth-Mars-Jupiter transfer trajectories. All these results certify the effectivity of the proposed model.

Key words: Planetary swing-by, Deep space maneuver, Hybrid search method, Interplanetary exploration