Global optimization of space mission concept of operations and systems design via mixed-integer nonlinear programming
Simultaneously optimizing space mission Concepts of Operations (ConOps) and spacecraft systems design involves discrete choices and nonconvex systems design models. This paper formulates the problem as a mixed-integer nonlinear program (MINLP) and presents both a heuristic approach based on augmented Lagrangian decomposition and a global optimization scheme that exploits concave structures commonly found in space systems. Specifically, we consider a crewed Mars mission case study developed in collaboration with NASA’s Advanced Concepts Office. To efficiently find feasible solutions to this MINLP, a decomposition framework from our prior work is modified and applied, where a series of convex mixed-integer quadratic programs and nonconvex nonlinear programs are iteratively solved. To identify globally optimal solutions, the proposed scheme incorporates the decomposition method as an upper bounding heuristic, constructs tight relaxations via piecewise linear underestimators, and applies variable domain reduction to close the optimality gap. The case study results demonstrate high computational efficiency and robust convergence behavior for both approaches. In particular, the proposed global optimization scheme converges to the same solution found by a state-of-the-art MINLP solver with substantially reduced computational cost, often by a few orders of magnitude. These results indicate the potential of the proposed framework as a practical and scalable alternative for solving nonconvex MINLPs in space mission and ConOps optimization coupled with systems design. • Space mission ConOps and systems design are co-optimized as a MINLP. • A decomposition method is used to efficiently generate high-quality feasible solutions. • A global optimization scheme is proposed for MINLPs involving concave functions. • Global optimality is achieved with significantly reduced computational cost. • Mars mission case study shows strong coupling between ConOps and systems.
Authors
- Nick Gollins (ORCID: https://orcid.org/0000-0002-6152-6765)
- Koki Ho (ORCID: https://orcid.org/0000-0002-3809-2954)
- Masafumi Isaji (ORCID: https://orcid.org/0000-0003-1050-8855)
Institutions
- Georgia Institute of Technology (US)
Publication Details
- Journal
- Acta Astronautica
- Published
- 2025-11-20
- DOI
- https://doi.org/10.1016/j.actaastro.2025.11.043
- Primary Topic
- Spacecraft Dynamics and Control
- Type
- article
- Field-Weighted Citation Impact
- 0.00