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Iowa State University - Thesis & Dissertation

Machine learning-aided trajectory optimization and tour design

Abstract

dc:description.abstract

This dissertation investigates machine learning (ML)-aided methods for preliminary space mission design, with a focus on trajectory optimization and tour design for interplanetary missions involving multiple gravity assists. In early-stage trajectory analysis, the repeated solution of Lambert’s problem often becomes a major computational bottleneck. Meanwhile, the number of possible flyby sequences grows combinatorially as the number of flybys increases, and each sequence is associated with a distinct cost function topology, making optimization and trade-space exploration especially challenging. To address these issues, this dissertation develops and evaluates several ML-aided frameworks for rapid transfer approximation, flyby-sequence optimization, and reinforcement-learning-based trajectory optimization. First, a neural-network-based Lambert approximator is developed to provide rapid estimates of transfer legs needed for large-scale trajectory searches while maintaining sufficient accuracy for preliminary mission design. Second, the neural network model for Lambert’s problem is integrated into the dynamic-size multiple-populations genetic algorithm (DSMPGA), and a vectorized implementation is adopted to enhance computational speed. This approach handles variable-length gravity-assist trajectories and generates both optimal and suboptimal mission candidates. Third, reinforcement learning is investigated as a sequential decision-making framework for multiple-gravity-assist trajectory optimization. In addition, deep learning is investigated for the placement of deep-space maneuvers, and the Extreme Theory of Functional Connections (X-TFC) is applied to orbital transfer problems under non-Keplerian dynamics, including J2-perturbed two-body motion and the circular restricted three-body problem. Overall, the results demonstrate that ML can accelerate preliminary trajectory design, improve the exploration of large and complex search spaces, and provide a promising foundation for future ML-aided mission design frameworks in space exploration.

Degree

thesis:*
Name thesis:degree_name
Doctor of Philosophy
Level thesis:degree_level
dissertation
Discipline thesis:degree_discipline
Aerospace engineering
Grantor
Iowa State University - Thesis & Dissertation
Year dc:date.issued
2026

Author and committee

dc:creator, dc:contributor.*
Author dc:creator
  • Choi, Sungmoon
Advisor dc:contributor.advisor
  • Abdelkhalik, Ossama

Subjects

dc:subject × 1

Rights

Language dc:language.iso
en_US

Identifiers

dc:identifier.*
Repository record dc:identifier.uri
https://dr.lib.iastate.edu/handle/20.500.12876/106702
OAI identifier oai:identifier
oai:dr.lib.iastate.edu:20.500.12876/106702

Chain of custody

source
Harvested from
Iowa State University
Base URL
dr.lib.iastate.edu/server/oai/request
Last updated
2026-07-24
Source record
OAI-PMH GetRecord
citation

Choi, Sungmoon. Machine learning-aided trajectory optimization and tour design. dissertation thesis, Iowa State University - Thesis & Dissertation, 2026. https://dr.lib.iastate.edu/handle/20.500.12876/106702