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.

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Institutions

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

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article

Orbital Depot Location Optimization for Satellite Constellation Servicing with Low-Thrust Transfers

Koki Ho, Euihyeon Choi
3 citations
Journal of Spacecraft and Rockets
Satellite Communication Systems
14.98
article

Orbital Depot Location Optimization for Satellite Constellation Servicing with Low-Thrust Transfers

Koki Ho, Euihyeon Choi
article en
3 citations

Abstract

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.

Journal of Spacecraft and RocketsVol. 63(1)
Georgia Institute of Technology (US)
Air Force Office of Scientific Research
Openalex Percentile: Top 2%
Satellite Communication Systems
14.98
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