Orbital Depot Location Optimization for Satellite Constellation Servicing with Low-Thrust Transfers
This paper addresses the critical problem of co-optimizing the optimal locations for orbital depots and the sequence of in-space servicing for a satellite constellation. While most traditional studies used network optimization for this problem, assuming a fixed set of discretized nodes in the network (i.e., a limited number of depot location candidates), this work is unique in that it develops a method to optimize the depot location in continuous space. The problem is formulated as mixed-integer nonlinear programming, and we propose a solution methodology that iteratively solves two decoupled problems: one using mixed-integer linear programming and the other using nonlinear programming with an analytic transfer solution. To demonstrate the effectiveness of our approach, we apply this methodology to a case study involving a GPS satellite constellation. Numerical experiments confirm the stability of our proposed solutions.
Authors
- Koki Ho (ORCID: https://orcid.org/0000-0002-3809-2954)
- Euihyeon Choi (ORCID: https://orcid.org/0000-0003-3048-2971)
Institutions
- Georgia Institute of Technology (US)
Publication Details
- Journal
- Journal of Spacecraft and Rockets
- Published
- 2025-06-30
- DOI
- https://doi.org/10.2514/1.a36386
- Citations
- 3
- Primary Topic
- Satellite Communication Systems
- Type
- article
- Field-Weighted Citation Impact
- 14.98
Funders
- Air Force Office of Scientific Research