September 24, 2025Open Access

Geometry-Preserving Libration Point Orbit Design in High-Fidelity Ephemeris Model via Sequential Convex Programming

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Authors

KHKoki HoWest Virginia University YSYuri ShimaneGeorgia Institute of Technology

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Implication

Nonlinear programming generates fuel-optimal libration point orbits in high-fidelity ephemeris model, indicating significant advancements for space missions.

Key Points

The approach effectively creates fuel-optimal libration point orbits while ensuring geometric preservation.
Demonstrations include constructing 9:2 resonant L2 near rectilinear halo orbits, showing practical application.
The method utilizes sequential convex programming to guarantee convergence to a local optimum efficiently.
This may enable more sustainable mission designs in proximity to critical libration points for various space applications.

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Ho et al. (2025) studied this question.

synapsesocial.com/papers/68d6e1248b2b6861e4c3f93f https://doi.org/10.21203/rs.3.rs-6172452/v1

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Implication

Nonlinear programming generates fuel-optimal libration point orbits in high-fidelity ephemeris model, indicating significant advancements for space missions.

Geometry-Preserving Libration Point Orbit Design in High-Fidelity Ephemeris Model via Sequential Convex Programming

Discussion

Member takes

Implication

Key Points

Cite This Study

Geometry-Preserving Libration Point Orbit Design in High-Fidelity Ephemeris Model via Sequential Convex Programming

Discussion

Member takes

Implication

Key Points

Cite This Study

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