Family of 2:1 resonant quasi-periodic distant retrograde orbits in cislunar space

Given the current enthusiasm for lunar exploration, the 2:1 resonant distant retrograde orbit (DRO) in Earth-Moon space is of interest. To gain an in-depth understanding of the complex dynamic environment in cislunar space and provide more options for parking orbits, this paper investigates the existence of quasi-periodic orbits near the 2:1 resonant DRO in the circular restricted three-body problem (CR3BP). Firstly, the numerical computation approach, continuation strategy, and stability analysis method of quasi-periodic orbits are introduced. Then, addressing the primary challenges in the continuation progress, we have developed an adaptive continuation algorithm with automatic adjustment of the step size and the number of discrete points that characterize the invariant torus. Finally, two types of 2D quasi-DROs and their linear stability properties are explored. Using Poincaré sections, we investigated the boundaries of the maximum extent attainable by both 2D quasi-DRO families in the CR3BP at a specific Jacobi energy, confirming that both types of quasi-periodic families have reached their respective boundaries. The algorithm described in this paper is beneficial for facilitating the computation of quasi-periodic families and aids in discovering additional potential dynamical structures.

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Publication Details

Journal
Frontiers in Astronomy and Space Sciences
Published
2024-09-02
DOI
https://doi.org/10.3389/fspas.2024.1352489
Citations
1
Primary Topic
Spacecraft Dynamics and Control
Type
article
Field-Weighted Citation Impact
1.30
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article

Family of 2:1 resonant quasi-periodic distant retrograde orbits in cislunar space

Yang Sun, Ming Wang, Chihang Yang, Hao Zhang
1 citations
Frontiers in Astronomy and Space Sciences
Spacecraft Dynamics and Control
1.30
article

Family of 2:1 resonant quasi-periodic distant retrograde orbits in cislunar space

Yang Sun, Ming Wang, Chihang Yang, Hao Zhang
article en
1 citations

Abstract

Given the current enthusiasm for lunar exploration, the 2:1 resonant distant retrograde orbit (DRO) in Earth-Moon space is of interest. To gain an in-depth understanding of the complex dynamic environment in cislunar space and provide more options for parking orbits, this paper investigates the existence of quasi-periodic orbits near the 2:1 resonant DRO in the circular restricted three-body problem (CR3BP). Firstly, the numerical computation approach, continuation strategy, and stability analysis method of quasi-periodic orbits are introduced. Then, addressing the primary challenges in the continuation progress, we have developed an adaptive continuation algorithm with automatic adjustment of the step size and the number of discrete points that characterize the invariant torus. Finally, two types of 2D quasi-DROs and their linear stability properties are explored. Using Poincaré sections, we investigated the boundaries of the maximum extent attainable by both 2D quasi-DRO families in the CR3BP at a specific Jacobi energy, confirming that both types of quasi-periodic families have reached their respective boundaries. The algorithm described in this paper is beneficial for facilitating the computation of quasi-periodic families and aids in discovering additional potential dynamical structures.

Frontiers in Astronomy and Space SciencesVol. 11
Chinese Academy of Sciences (CN), Technology and Engineering Center for Space Utilization (CN), University of Chinese Academy of Sciences (CN)
Openalex Percentile: Top 13%
Spacecraft Dynamics and Control
1.30
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