Multi-Vehicle Guidance for Formation Flight on Libration Point Orbits
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arXiv
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| Main Authors: | , , |
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| Format: | Preprint |
| Published: |
2025
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| _version_ | 1866912591618506752 |
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| author | Shimane, Yuri Elango, Purnanand Weiss, Avishai |
| author_facet | Shimane, Yuri Elango, Purnanand Weiss, Avishai |
| contents | The multiple spacecraft guidance problem for proximity flight in libration point orbit is considered. A nonlinear optimal control problem with continuous-time path constraints enforcing minimum separation between each spacecraft is formulated. The path constraints are enforced via an isoperimetric reformulation, and the problem is solved via a sequential convex programming. The proposed approach does not necessitate specific dynamic system structures to provide continuous-time guarantees for minimum separation within a fuel-optimal solution. The optimal control problem is deployed within a model predictive control scheme and demonstrated in the ephemeris model dynamics. |
| format | Preprint |
| id |
arxiv_https___arxiv_org_abs_2509_14730 |
| institution | arXiv |
| publishDate | 2025 |
| record_format | arxiv |
| spellingShingle | Multi-Vehicle Guidance for Formation Flight on Libration Point Orbits Shimane, Yuri Elango, Purnanand Weiss, Avishai Optimization and Control The multiple spacecraft guidance problem for proximity flight in libration point orbit is considered. A nonlinear optimal control problem with continuous-time path constraints enforcing minimum separation between each spacecraft is formulated. The path constraints are enforced via an isoperimetric reformulation, and the problem is solved via a sequential convex programming. The proposed approach does not necessitate specific dynamic system structures to provide continuous-time guarantees for minimum separation within a fuel-optimal solution. The optimal control problem is deployed within a model predictive control scheme and demonstrated in the ephemeris model dynamics. |
| title | Multi-Vehicle Guidance for Formation Flight on Libration Point Orbits |
| topic | Optimization and Control |
| url | https://arxiv.org/abs/2509.14730 |