Trajectory Optimization for Orbit Transfers: Principles, Advances, Case Studies, and Outlook

This review presents an in-depth exploration of trajectory optimization techniques for various orbit transfer applications, focusing on principles, methodologies, and practical case studies. The emphasis is placed on indirect, direct, and data-driven trajectory optimization methods powered by numerical, deterministic, and gradient-based optimization algorithms, and an overview on the basic fundamentals of each method is provided. Applications cover numerous orbit transfer problems, from geocentric and interplanetary transfers to other orbital maneuvers that are applicable to the orbit transfer problem, highlighting critical advancements of trajectory optimization techniques in enabling more efficient and feasible space missions. A minimum-fuel transfer from Earth to Mars is considered as a case study and solved using the indirect, direct, and data-driven methods, respectively, demonstrating an effective primer on the implementation of each method. Finally, we identify open challenges and issues, discuss potential opportunities, and make suggestions for future research directions. By synthesizing current methods and emerging trends, this review provides a comprehensive toolkit for addressing complex challenges in orbit transfers.

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Publication Details

Journal
Aerospace
Published
2025-12-06
DOI
https://doi.org/10.3390/aerospace12121087
Citations
1
Primary Topic
Spacecraft Dynamics and Control
Type
article
Field-Weighted Citation Impact
4.99
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Trajectory Optimization for Orbit Transfers: Principles, Advances, Case Studies, and Outlook

Daniel DeLaurentis, Kshitij Mall, Zhenbo Wang, Katherine Vasiloff et al.
1 citations
Aerospace
Spacecraft Dynamics and Control
4.99
article

Trajectory Optimization for Orbit Transfers: Principles, Advances, Case Studies, and Outlook

Daniel DeLaurentis, Kshitij Mall, Zhenbo Wang, Katherine Vasiloff, Israel Adesina
article en
1 citations

Abstract

This review presents an in-depth exploration of trajectory optimization techniques for various orbit transfer applications, focusing on principles, methodologies, and practical case studies. The emphasis is placed on indirect, direct, and data-driven trajectory optimization methods powered by numerical, deterministic, and gradient-based optimization algorithms, and an overview on the basic fundamentals of each method is provided. Applications cover numerous orbit transfer problems, from geocentric and interplanetary transfers to other orbital maneuvers that are applicable to the orbit transfer problem, highlighting critical advancements of trajectory optimization techniques in enabling more efficient and feasible space missions. A minimum-fuel transfer from Earth to Mars is considered as a case study and solved using the indirect, direct, and data-driven methods, respectively, demonstrating an effective primer on the implementation of each method. Finally, we identify open challenges and issues, discuss potential opportunities, and make suggestions for future research directions. By synthesizing current methods and emerging trends, this review provides a comprehensive toolkit for addressing complex challenges in orbit transfers.

AerospaceVol. 12(12)
Purdue University West Lafayette (US), Knoxville College (US), University of Tennessee at Knoxville (US), University of South Alabama (US)
Openalex Percentile: Top 4%
Spacecraft Dynamics and Control
4.99
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Trajectory Optimization for Orbit Transfers: Principles, Advances, Case Studies, and Outlook — Daniel DeLaurentis, Kshitij Mall, et al. · Aerospace (2025) | TGRS Research Map | TGRS