Design and application of low energy transfer orbit based on Lissajous staging post
Lissajous orbit is a kind of quasi-periodic orbit, which has rich shape choices, more mission flexibility and less fuel consumption required for orbit maintenance. Therefore, it can be used as a staging post orbit for the future construction of the cislunar space Airline-flight-mode transportation n...
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EDP Sciences
2025-04-01
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| Series: | Xibei Gongye Daxue Xuebao |
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| Online Access: | https://www.jnwpu.org/articles/jnwpu/full_html/2025/02/jnwpu2025432p212/jnwpu2025432p212.html |
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| author | YU Huichang DAI Honghua ZHANG Jiye WANG Yamin YUE Xiaokui ZHANG Yonghe |
| author_facet | YU Huichang DAI Honghua ZHANG Jiye WANG Yamin YUE Xiaokui ZHANG Yonghe |
| author_sort | YU Huichang |
| collection | DOAJ |
| description | Lissajous orbit is a kind of quasi-periodic orbit, which has rich shape choices, more mission flexibility and less fuel consumption required for orbit maintenance. Therefore, it can be used as a staging post orbit for the future construction of the cislunar space Airline-flight-mode transportation network. Low-energy transfer orbits from low Earth orbit to the Lissajous staging post will be the basis of building an economic and sustainable transportation system. However, the characteristics of low energy transfer orbits based on Lissajous staging post are currently unclear, and for the staging post orbits whose invariant manifolds are far from the moon, the maneuvering insertion strategy adopted in the traditional three-maneuver design method cannot fully utilize its advantages in reducing fuel consumption. In view of the above issues, a design method of three-maneuver low-energy transfer combining patched manifold and lunar flyby is proposed. The dimension of the optimization problem is reduced by piecewise solution, and the optimal solution is obtained by bi-level optimization. The results show that the above design method can reduce transfer fuel consumption by about 18-400 m/s for some orbit insertion points, effectively increasing the range of optional insertion points, and is also applicable to large amplitude Lissajous staging post orbits. Finally, the variation characteristics of flyby azimuth, flyby height, orbital insertion position, and other celestial gravity effects are emphatically analyzed. The results have important reference value for the selection of staging post orbits, launch windows, and orbital insertion points in future cislunar space Airline-flight-mode transportation networks. |
| format | Article |
| id | doaj-art-89c74bc4cc4846048a41b30e7ef86a77 |
| institution | Kabale University |
| issn | 1000-2758 2609-7125 |
| language | zho |
| publishDate | 2025-04-01 |
| publisher | EDP Sciences |
| record_format | Article |
| series | Xibei Gongye Daxue Xuebao |
| spelling | doaj-art-89c74bc4cc4846048a41b30e7ef86a772025-08-20T03:25:56ZzhoEDP SciencesXibei Gongye Daxue Xuebao1000-27582609-71252025-04-0143221222110.1051/jnwpu/20254320212jnwpu2025432p212Design and application of low energy transfer orbit based on Lissajous staging postYU Huichang0DAI Honghua1ZHANG Jiye2WANG Yamin3YUE Xiaokui4ZHANG Yonghe5School of Astronautics, Northwestern Polytechnical UniversitySchool of Astronautics, Northwestern Polytechnical UniversitySchool of Astronautics, Northwestern Polytechnical UniversityInnovation Academy for Microsatellites of Chinese Academy of SciencesSchool of Astronautics, Northwestern Polytechnical UniversityInnovation Academy for Microsatellites of Chinese Academy of SciencesLissajous orbit is a kind of quasi-periodic orbit, which has rich shape choices, more mission flexibility and less fuel consumption required for orbit maintenance. Therefore, it can be used as a staging post orbit for the future construction of the cislunar space Airline-flight-mode transportation network. Low-energy transfer orbits from low Earth orbit to the Lissajous staging post will be the basis of building an economic and sustainable transportation system. However, the characteristics of low energy transfer orbits based on Lissajous staging post are currently unclear, and for the staging post orbits whose invariant manifolds are far from the moon, the maneuvering insertion strategy adopted in the traditional three-maneuver design method cannot fully utilize its advantages in reducing fuel consumption. In view of the above issues, a design method of three-maneuver low-energy transfer combining patched manifold and lunar flyby is proposed. The dimension of the optimization problem is reduced by piecewise solution, and the optimal solution is obtained by bi-level optimization. The results show that the above design method can reduce transfer fuel consumption by about 18-400 m/s for some orbit insertion points, effectively increasing the range of optional insertion points, and is also applicable to large amplitude Lissajous staging post orbits. Finally, the variation characteristics of flyby azimuth, flyby height, orbital insertion position, and other celestial gravity effects are emphatically analyzed. The results have important reference value for the selection of staging post orbits, launch windows, and orbital insertion points in future cislunar space Airline-flight-mode transportation networks.https://www.jnwpu.org/articles/jnwpu/full_html/2025/02/jnwpu2025432p212/jnwpu2025432p212.html航班化lissajous轨道不变流形轨道优化轨道特性 |
| spellingShingle | YU Huichang DAI Honghua ZHANG Jiye WANG Yamin YUE Xiaokui ZHANG Yonghe Design and application of low energy transfer orbit based on Lissajous staging post Xibei Gongye Daxue Xuebao 航班化 lissajous轨道 不变流形 轨道优化 轨道特性 |
| title | Design and application of low energy transfer orbit based on Lissajous staging post |
| title_full | Design and application of low energy transfer orbit based on Lissajous staging post |
| title_fullStr | Design and application of low energy transfer orbit based on Lissajous staging post |
| title_full_unstemmed | Design and application of low energy transfer orbit based on Lissajous staging post |
| title_short | Design and application of low energy transfer orbit based on Lissajous staging post |
| title_sort | design and application of low energy transfer orbit based on lissajous staging post |
| topic | 航班化 lissajous轨道 不变流形 轨道优化 轨道特性 |
| url | https://www.jnwpu.org/articles/jnwpu/full_html/2025/02/jnwpu2025432p212/jnwpu2025432p212.html |
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