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Author:

Zhang, G. (Zhang, G..) | Pang, B. (Pang, B..) | Sun, Y. (Sun, Y..) | Zhou, X. (Zhou, X..) | Shang, Y. (Shang, Y..) | Chen, C. (Chen, C..) | Lu, M. (Lu, M..) | Zhang, Y. (Zhang, Y..) | Jin, Z. (Jin, Z..) | Qiao, P. (Qiao, P..) | Liu, Y. (Liu, Y..) | Zhu, Z. (Zhu, Z..) | Qian, Y. (Qian, Y..) | Wen, C. (Wen, C..)

Indexed by:

EI Scopus SCIE

Abstract:

In the 2016 International Astronautical Congress, SpaceX's Mars immigration plan was first formally proposed alongside a fully-reusable transportation infrastructure. In the 12th edition of the China Trajectory Optimization Competition (CTOC-12) held in 2022, a Mars transportation trajectory design problem using reusable transporters from a parking distant retrograde orbit (DRO) in the Earth–Moon system was released. It is expected to transport as many immigrants as possible using a maximum of 50 transporters within a total of 20 years. The BIT-DFH-BJUT team reported a solution that can deliver 9080 immigrants to Mars, which ranked first in the competition. In this paper, the methods and results from the winning team are presented, primarily including an overall analysis, underlying round-trip trajectory design, and top-level scheduling. Specifically, a round-trip is divided into four phases, leaving the DRO to man-boarding at the perigee, Earth–Mars interplanetary transfer, Mars's return to the Earth, and return to the DRO. An overall optimization framework is constructed by synthesizing techniques such as data set creation and patching, differential evolution, nonlinear programming, greedy algorithm, and mixed-integer programming. Finally, we outline the final solution of our team and compare the results with those from the top five teams. This competition demonstrates that a large-scale Mars immigration plan is possible by using reusable transporters from the Earth–Moon system. © 2023 IAA

Keyword:

Mars immigration Distant retrograde orbit China trajectory optimization competition Reusable transporters

Author Community:

  • [ 1 ] [Zhang G.]Beijing Institute of Technology, Beijing, 100081, China
  • [ 2 ] [Pang B.]Beijing Institute of Technology, Beijing, 100081, China
  • [ 3 ] [Sun Y.]Beijing Institute of Technology, Beijing, 100081, China
  • [ 4 ] [Zhou X.]Beijing Institute of Technology, Beijing, 100081, China
  • [ 5 ] [Shang Y.]Beijing Institute of Technology, Beijing, 100081, China
  • [ 6 ] [Chen C.]Beijing Institute of Technology, Beijing, 100081, China
  • [ 7 ] [Lu M.]DFH Satellite Company, Beijing, 100094, China
  • [ 8 ] [Zhang Y.]Beijing University of Technology, Beijing, 100124, China
  • [ 9 ] [Jin Z.]Beijing Institute of Technology, Beijing, 100081, China
  • [ 10 ] [Zhang Y.]Beijing Institute of Technology, Beijing, 100081, China
  • [ 11 ] [Qiao P.]Beijing University of Technology, Beijing, 100124, China
  • [ 12 ] [Liu Y.]DFH Satellite Company, Beijing, 100094, China
  • [ 13 ] [Zhu Z.]DFH Satellite Company, Beijing, 100094, China
  • [ 14 ] [Qian Y.]Beijing University of Technology, Beijing, 100124, China
  • [ 15 ] [Wen C.]Beijing Institute of Technology, Beijing, 100081, China

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Source :

Acta Astronautica

ISSN: 0094-5765

Year: 2023

Volume: 207

Page: 129-152

3 . 5 0 0

JCR@2022

ESI Discipline: ENGINEERING;

ESI HC Threshold:19

Cited Count:

WoS CC Cited Count: 0

SCOPUS Cited Count: 4

ESI Highly Cited Papers on the List: 0 Unfold All

WanFang Cited Count:

Chinese Cited Count:

30 Days PV: 0

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