Volume 43 Issue 5
Nov.  2023
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DONG Bowen, YU Xizheng, LI Mingtao, WANG Kaiduo, WANG Youliang. Orbit Design Optimization Method for an Asteroid Flyby Mission from DRO (in Chinese). Chinese Journal of Space Science, 2023, 43(5): 864-874 doi: 10.11728/cjss2023.05.2023-0011
Citation: DONG Bowen, YU Xizheng, LI Mingtao, WANG Kaiduo, WANG Youliang. Orbit Design Optimization Method for an Asteroid Flyby Mission from DRO (in Chinese). Chinese Journal of Space Science, 2023, 43(5): 864-874 doi: 10.11728/cjss2023.05.2023-0011
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Orbit Design Optimization Method for an Asteroid Flyby Mission from DRO

doi: 10.11728/cjss2023.05.2023-0011 cstr: 32142.14.cjss2023.05.2023-0011
  • 1.

    National Space Science Center, Chinese Academy of Sciences, Beijing 100190

  • 2.

    University of Chinese Academy of Sciences, Beijing 100049

  • Received Date: 2023-01-20
  • Rev Recd Date: 2023-04-18
    • Available Online: 2023-07-26
    Abstract
  • Distant Retrograde Orbit (DRO) is a kind of stable periodic orbit in Earth-Moon system. In this paper, a design method of distant retrograde orbit for spacecraft to fly by and explore near-Earth asteroids by means of the moon and Earth’s gravity assistance starting from DRO orbital station is studied. By means of earth-moon gravity assistance and mid-course lever maneuver, the velocity increment required for adjusting the inclination angle is reduced, and the reachable range of the asteroid flying by exploration under the same velocity increment constraint is expanded. At the same time, the calculation complexity of the problem is reduced by introducing DRO phasing, with reducing the phase constraints of escape and capture in DRO, and decoupling the phase of the transfer track from the DRO orbital station. The simulation results show that under the velocity increment of 2 km·s–1, the method can realize the orbit design of flyby exploration of near-Earth asteroids from DRO orbital station and return.

     

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