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The problem of optimizing the lunar transfers of low-thrust spacecraft with the optimal value of the right ascension of the ascending node and the argument of the perigee of the initial Earth’s and the final Moon’s orbits is considered. The goal of optimization is to minimize a thrust value of the electric propulsion systems. The obtained trajectories with minimum thrust for partially free and fixed boundary conditions are compared.

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Optimization of Minimum Thrust Trajectories with Free Boundary Conditions Between Earth and Lunar Orbit

  • 会议论文

  • 发表日期：

    2026年

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  • Sung Wook Yoon,
  • Viacheslav G. Petukhov

摘要

The problem of optimizing the lunar transfers of low-thrust spacecraft with the optimal value of the right ascension of the ascending node and the argument of the perigee of the initial Earth’s and the final Moon’s orbits is considered. The goal of optimization is to minimize a thrust value of the electric propulsion systems. The obtained trajectories with minimum thrust for partially free and fixed boundary conditions are compared.