Agile Tradespace Exploration for Space Rendezvous Mission Design via Transformers
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Abstract (arXiv)
Spacecraft rendezvous enables on-orbit servicing, debris removal, and crewed docking, forming the foundation for a scalable space economy. Designing such missions requires rapid exploration of the tradespace between control cost and flight time across multiple candidate targets. However, multi-objective optimization in this setting is challenging, as the underlying constraints are often nonconvex, and mission designers must balance accuracy (e.g., solving the full problem) with efficiency (e.g., convex relaxations), slowing iteration and limiting design agility. To address these challenges, this paper proposes an AI-powered framework that enables agile and generalized rendezvous mission design. Given the orbital information of the target spacecraft, boundary conditions of the servicer, and a range of flight times, a transformer model generates a set of near-Pareto optimal trajectories across varying flight times in a single parallelized inference step, thereby enabling rapid mission trade studies. The model is further extended to accommodate variable flight times and perturbed orbital dynamics, supporting realistic multi-objective trade-offs. Validation on chance-constrained rendezvous problems in Earth orbits with passive safety constraints demonstrates that the model generalizes across both flight times and dynamics, consistently providing high-quality initial guesses that converge to superior solutions in fewer iterations. Moreover, the framework efficiently approximates the Pareto front, achieving runtimes comparable to convex relaxation by exploiting parallelized inference. Together, these results position the proposed framework as a practical surrogate for nonconvex trajectory generation and mark an important step toward AI-driven trajectory design for accelerating preliminary mission planning in real-world rendezvous applications.
Key facts. Cited by 4 papers in the map (data through 7 Oct 2026). Builds on 24 of its 70 references that are in the map. First posted on arXiv 3 Oct 2025.
Builds on
24 of 70 references.
References · 24
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- 2025Global Search for Optimal Low Thrust Spacecraft Trajectories using Diffusion Models and the Indirect Methodcited by 7
- 2023Constraint-Informed Learning for Warm Starting Trajectory Optimizationcited by 6
- 2024Generalizable Spacecraft Trajectory Generation via Multimodal Learning with Transformerscited by 6
12 more
- 2022Passively-Safe and Robust Multi-Agent Optimal Control with Application to Distributed Space Systemscited by 5
- 2023Autonomous Guidance Navigation and Control of the VISORS Formation-Flying Missioncited by 5
- 2021Fast Homotopy for Spacecraft Rendezvous Trajectory Optimization with Discrete Logiccited by 4
- 2024Chance-Constrained, Drift-Safe Guidance for Spacecraft Rendezvouscited by 3
- 2025Safe and Optimal N-Spacecraft Swarm Reconfiguration in Non-Keplerian Cislunar Orbitscited by 3
- 2025Deep Learning Warm Starts for Trajectory Optimization on the International Space Stationcited by 3
- 2022Neural-Rendezvous: Provably Robust Guidance and Control to Encounter Interstellar Objectscited by 2
- 2024Filtering-Linearization: A First-Order Method for Nonconvex Trajectory Optimization with Filter-Based Warm-Startingcited by 2
- 2022Robust Constrained Multi-objective Evolutionary Algorithm based on Polynomial Chaos Expansion for Trajectory Optimizationcited by 1
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- 2024Compositional Diffusion Models for Powered Descent Trajectory Generation with Flexible Constraintscited by 1
- 2025Initial Guess Generation for Low-Thrust Trajectory Design with Robustness to Missed-Thrust-Eventscited by 1
Built on by
Citing papers per year: 2025: 1; 2026: 3.
4 papers.
- 2025Language-Conditioned Safe Trajectory Generation for Spacecraft Rendezvouscited by 3
- 2026Intent-aligned Autonomous Spacecraft Guidance via Reasoning Modelscited by 1
- 2026Transformer-Based Warm-Starting for Feasible and Optimal Terminal Approach to Tumbling Objects with Space Manipulatorscited by 1
- 2026Transformer-Informed Trajectory Optimization for Relative Motion in Cislunar Orbitscited by 0
- 2026Transformer-Informed Trajectory Optimization for Relative Motion in Cislunar Orbits21 Sep 2026
- 2026Transformer-Based Warm-Starting for Feasible and Optimal Terminal Approach to Tumbling Objects with Space Manipulators15 Jun 2026
- 2026Intent-aligned Autonomous Spacecraft Guidance via Reasoning Models19 Apr 2026
- 2025Language-Conditioned Safe Trajectory Generation for Spacecraft Rendezvous9 Dec 2025